QUICK REFERENCE HANDBOOK 01DEC2014 GROUND QRH - DO NOT USE IN FLIGHT The content of this document is the property of Airbus. It is supplied in confidence and commercial security on its contents must be maintained. It must not be used for any purpose other than that for which it is supplied, nor may information contained in it be disclosed to unauthorized persons. It must not be reproduced in whole or in part without permission in writing from the owners of the copyright. © AIRBUS 2005. All rights reserved. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE Intentionally left blank A330 TRANSMITTAL LETTER QUICK REFERENCE HANDBOOK 1/2 01 DEC 14 Issue date: 01 DEC 14 This is the first issue of the QUICK REFERENCE HANDBOOK dated 01 DEC 14 for the A330 QRH PAGE GEN.02A PROVIDES ADDITIONAL GUIDANCE TO MANAGE THE QRH UPDATES. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 TRANSMITTAL LETTER QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 01 DEC 14 A330 FILING INSTRUCTIONS QUICK REFERENCE HANDBOOK Please note that the entire manual is delivered. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 1/2 01 DEC 14 A330 FILING INSTRUCTIONS QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 01 DEC 14 A330 QUICK REFERENCE HANDBOOK (1) M Localization PLP-LESS PLP-LETDU GEN ABN-22 ABN-24 ABN-25 ABN-26 ABN-27 ABN-28 ABN-29 ABN-30 ABN-31 ABN-32 ABN-34 ABN-36 ABN-70 ABN-80 NP-NP NP-NCL PER-A PER-B PER-C PER-D PER-24 PER-27 PER-27A PER-28 PER-29 PER-30 PER-32 PER-34 PER-36 PER-70 PER-E PER-G PER-H PER-I OPS OEBPROC-PLP-LEOEB PRELIMINARY PAGES LIST OF EFFECTIVE SECTIONS/SUBSECTIONS Subsection Title LIST OF EFFECTIVE SECTIONS/SUBSECTIONS LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS General Auto-Flight Electrical Equipment Fire Protection Flight Controls Fuel Hydraulic Ice and Rain Protection Indicating / Recording Systems Landing Gear Navigation Pneumatic Engines Miscellaneous Normal Procedures Normal Checklist Speeds Fuel Penalty Factors Landing Performance Assessment Landing Distance without Failure Landing Distance with Electrical System Failure Landing Distance with Flight Controls System Failure Landing Distance with Slats and Flaps System Failure Landing Distance with Fuel System Failure Landing Distance with Hydraulic System Failure Landing Distance with Anti Ice System Failure Landing Distance with Brake System Failure Landing Distance with Navigation System Failure Landing Distance with Bleed System Failure Landing Distance with Engine System Failure One Engine Inoperative All Engines Operative Flight Without Cabin Pressurization Miscellaneous Operational Data LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN (1) Evolution code : N=New, R=Revised, E=Effectivity, M=Moved TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 1/2 01 DEC 14 Rev. Date 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 01 DEC 14 A330 QUICK REFERENCE HANDBOOK PRELIMINARY PAGES LIST OF EFFECTIVE SECTIONS/SUBSECTIONS Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 01 DEC 14 A330 QUICK REFERENCE HANDBOOK M (1) PRELIMINARY PAGES LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS Localization DU Title DU identification 1/2 01 DEC 14 DU date ABN-80 Computer Reset Table FG00763 ABN-80 Computer Reset Table - 32 - Landing Gear 00015048.0001001 07 OCT 13 Criteria: LR Applicable to: ALL Impacted DU: 00010654 Computer Reset Table - 32 - Landing Gear Reason for issue: The BSCU reset procedure for WHEEL N/W STRG FAULT is amended with a temporary procedure, in order to better address the spurious alerts that are currently encountered in-service. Under the very specific conditions defined in the procedure, the flight crews can continue the flight without troubleshooting after a successful BSCU reset. (1) Evolution code : N=New, R=Revised, E=Effectivity TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK PRELIMINARY PAGES LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 01 DEC 14 A330 QUICK REFERENCE HANDBOOK PRELIMINARY PAGES AIRCRAFT ALLOCATION TABLE 1/2 01 DEC 14 This table gives, for each delivered aircraft, the cross reference between: - The Manufacturing Serial Number (MSN). The Fleet Serial Number (FSN) of the aircraft as known by AIRBUS S.A.S. The registration number of the aircraft as known by AIRBUS S.A.S. The aircraft model. (1) M MSN FSN Registration Number Model 0232 PT-MVA 330-223 0238 PT-MVB 330-223 0247 PT-MVC 330-223 0259 PT-MVD 330-223 0361 PT-MVE 330-223 0466 PT-MVF 330-203 0472 PT-MVG 330-203 0700 PT-MVL 330-203 0968 PT-MVQ 330-223 1112 PT-MVS 330-223 1118 PT-MVT 330-223 (1) Evolution code : N=New, R=Revised TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK PRELIMINARY PAGES AIRCRAFT ALLOCATION TABLE Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 01 DEC 14 A330 QUICK REFERENCE HANDBOOK (1) M MODIFICATION D17250 1/4 PRELIMINARY PAGES LIST OF MODIFICATIONS Linked SB Incorp. Date 01 DEC 14 Title 30 AUG 10 Applicable to: ALL D19426 AIR CONDITIONING-DEFINE VENTILATION OF FORWARD CARGO COMPARTMENT 30 AUG 10 Applicable to: MSN 0232-0361 D40487 COMMUNICATIONS-GENERAL-INSTALL AUTOMATIC PORTABLE ELT WITH ANTENNA AND CONTROL PANEL CEIS A06 30 AUG 10 Applicable to: ALL D41528 FUEL - APU FUEL PUMP SYSTEM - PREVENT AN ELECTRICAL ESS NETWORK "OVERLOAD" (A330) 30 AUG 10 Applicable to: MSN 0232-0361 D42829 COMMUNICATIONS - GENERAL - ADAPT AUTOMATIC PORTABLE ELT WITH ANTENNA AND CONTROL PANEL CEIS A06 30 AUG 10 Applicable to: MSN 0700-1118 D43619 COMMUNICATIONS - GENERAL - BASIC PROVISIONS FOR IN FLIGHT ENTERTAINMENT SYSTEM A330/A340-200/300 30 AUG 10 EQUIPMENT/FURNISHINGS-COCKPIT- INSTALL ELT REMOTE CONTROL PANEL IN COCKPIT -SEXTANT- 30 AUG 10 EQUIPMENT/FURNISHINGS - COCKPIT - INSTALL AN ARMOURED COCKPIT DOOR 30 AUG 10 Applicable to: MSN 0700-1118 D44532 25-3215 03 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT - INSTALL NOISE REDUCED COCKPIT DOOR LOCK SYSTEM 30 AUG 10 Applicable to: MSN 0232-0472 D44690 EQUIPMENT/FURNISHINGS - CURTAINS AND PARTITIONS -MODIFY CDLS STRIKE TOLERANCE 30 AUG 10 Applicable to: MSN 0700-1118 D45352 25-5150 00 EQUIPMENT/FURNISHINGS - CURTAINS AND PARTITIONS - INSTALL A MAXIMUM NOISE REDUCED COCKPIT DOOR LOCK SYSTEM (CDLS) 30 AUG 10 Applicable to: MSN 0968-1118 H13232 EQUIPMENT/FURNISHINGS-MIS. EMER. EQPT.- INSTALL HONEYWELL ELT WITH REMOTE CONTROL PANEL IN THE COCKPIT 30 AUG 10 Applicable to: ALL H13701 LANDING GEAR - WHEELS - DEFINE AND FIT ALLIED SIGNAL BRAKES FOR GROWTH A/C 30 AUG 10 Applicable to: ALL H13959 FUEL - JETTISON SYSTEM - INSTALL JETTISON SYSTEM ON A330-200 30 AUG 10 ICE AND RAIN PROTECTION - WING ICE PROTECTION RELOCATE OUTBOARD VALVE TO INBOARD POSITION 25 NOV 11 FUEL - FCMS - INSTALL FCMC STAGE 9.0 30 MAY 12 Applicable to: MSN 0700-1118 S12358 GENERAL-DESIGN WEIGHTS-CERTIFY A330-200 WV050 MTOW 230T, MLW 180T, MZFW 168T WITH REVISED A/C DESIGN SERVICE GOAL 30 AUG 10 Applicable to: ALL S12968 FLIGHT CONTROLS - CHANGE WIRING OF FCPC1 AND FCSC1 FAULT INDICATOR LIGHTS 30 AUG 10 Applicable to: ALL S13133 NAVIGATION - WEATHER RADAR SYSTEM - ACTIVATE DUAL PREDICTIVE WINDSHEAR RADAR SYSTEM, COLLINS 30 AUG 10 Applicable to: ALL S13208 ICE AND RAIN PROTECTION - WINDSHIELD RAIN PROTECTION - DEACTIVATE RAIN REPELLENT SYSTEM 30 AUG 10 ENGINE FUEL AND CONTROL-GENERAL-PROVIDE DERATED TAKE-OFF FACILITY FOR PRATT AND WHITNEY Applicable to: MSN 0466-0700 D44099 25-3161 03 25-3194 00 Applicable to: ALL D44341 Applicable to: ALL H14027 Applicable to: ALL H15264 28-3067 01 Applicable to: MSN 0232-0361, 0968-1118 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK (1) M 2/4 PRELIMINARY PAGES LIST OF MODIFICATIONS 01 DEC 14 Continued from the previous page MODIFICATION S13217 Linked SB Incorp. Date Title 30 AUG 10 Applicable to: ALL S13313 FUEL - DISTRIBUTION - INSTALL STRUCTURE AND SYSTEM PROVISIONS FOR ACTIVATION OF CENTER TANK (A330-200) 30 AUG 10 Applicable to: ALL S13433 FLIGHT CONTROLS - GENERAL - ADAPT FLIGHT CONTROLS FOR ST7 30 AUG 10 Applicable to: MSN 0466-0700 S13661 ENGINE FUEL AND CONTROL - GENERAL - PROVIDE DERATED TAKE-OFF FACILITIES FOR G.E. ENGINES 30 AUG 10 Applicable to: ALL S13893 NAVIGATION - MMR - INSTALL COLLINS MULTI-MODE RECEIVERS PROVIDING ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION 30 AUG 10 Applicable to: ALL S13916 OXYGEN - CREW OXYGEN - INSTALL A 115 CU.FT COMPOSITE OXYGEN CYLINDER 30 AUG 10 Applicable to: ALL S14135 ICE AND RAIN PROTECTION - WINDSHIELD RAIN PROTECTION - REACTIVATE THE RAIN REPELLENT SYSTEM 30 AUG 10 INDICATING/RECORDING SYSTEMS - EIS - DISPLAY MANAGEMENT COMPUTER - INSTALL NEW DMC SOFTWARE V510X 30 AUG 10 NAVIGATION - GPWS - ACTIVATE ENHANCED GPWS 30 AUG 10 AUTO FLIGHT - FMGEC - INSTALL FMGEC P1-B7 FOR GE ENGINES 30 AUG 10 AUTO FLIGHT - FMGEC - INSTALL FMGEC P1-CD7 FOR RR OR PW ENGINES Applicable to: ALL S14218 Applicable to: ALL S14273 34-3077 05 Applicable to: MSN 0466-0700 S14275 22-3026 03 Applicable to: MSN 0232-0361, 0968-1118 S14327 30 AUG 10 INDICATING/RECORDING SYSTEMS-CENTRAL WARNING SYSTEMS-PROVIDE NEW AUTO CALL-OUT CALLED "V1" Applicable to: MSN 0700-1118 S14521 30 AUG 10 Applicable to: MSN 0968-1118 S14562 22-3022 01 NAVIGATION-TCAS-INSTALL ALLIED SIGNAL CHANGE 7 P/N 066-50000-2220 30 AUG 10 AUTO FLIGHT - FMGEC - INSTALL A NEW STANDARD FMGEC L9CD6 Applicable to: MSN 0232-0361, 0968-1118 S14591 30 AUG 10 NAVIGATION-TCAS-INSTALL COLLINS TCAS TTR921 - P/N 822-1293-321 Applicable to: MSN 0466-0700 S14649 34-3073 01 30 AUG 10 Applicable to: ALL S14736 NAVIGATION - MMR - INSTALL COLLINS MULTI-MODE RECEIVERS P/N 822-1152-121 30 AUG 10 Applicable to: MSN 0466-0700 S14739 34-3098 03 AUTO FLIGHT - FMGEC - INSTALL A NEW STANDARD FMGEC L9B6 FOR GE ENGINE 30 AUG 10 Applicable to: MSN 0232-0700 S14786 NAVIGATION-TCAS-INSTALL TCAS 2 COLLINS CHANGE 7 COMPUTER P/N 622-8971-322 30 AUG 10 Applicable to: MSN 0700-1118 S14859 NAVIGATION-STANDBY NAVIGATION SYSTEMS- INSTALL SEXTANT AVIONICS INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) 30 AUG 10 Applicable to: MSN 0700-1118 S15891 INDICATING/RECORDING SYSTEMS-ELECTRONIC INSTRUMENT SYSTEM - INSTALL NEW DISPLAY SYSTEM (EIS2) EQTS (DMC/DU/DISKETTES) 30 AUG 10 NAVIGATION - EGPWS - USE LATERAL GPS POSITION WITH AUTOMATIC DESELECTION Applicable to: MSN 0968-1118 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK (1) M 3/4 PRELIMINARY PAGES LIST OF MODIFICATIONS 01 DEC 14 Continued from the previous page MODIFICATION S16107 Linked SB 46-3006 04 Incorp. Date Title 07 APR 11 INFORMATION SYSTEMS - GENERAL - CERTIFY FANS A CONFIGURATIONS 30 AUG 10 NAVIGATION - EGPWS - ACTIVATE OBSTACLE FUNCTION 30 AUG 10 Applicable to: MSN 0700-1118 S16286 FLIGHT CONTROLS - ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS) - INSTALL RUDDER FLY-BY WIRE ON A330/A340 30 AUG 10 Applicable to: MSN 0700-1118 S16318 INDICATING/RECORDING SYSTEMS - FWC - INSTALL NEW STANDARD K7 30 AUG 10 Applicable to: MSN 0700-1118 S16354 31-3048 00 ELECTICAL POWER - GENERAL - INSTALL EMERGENCY POWER CENTER 743 VU IN SECT 11/12 30 AUG 10 Applicable to: ALL S16606 INDICATING/RECORDING SYSTEMS - FWC - REPLACE THE EXISTING STANDARD FWC BY A NEW STD K6 FOR A330 FAR 121-344 30 AUG 10 Applicable to: MSN 0700-1118 S16646 INDICATING/RECORDING SYSTEMS - EIS - INTALL NEW EIS2 STANDARD L4 ON A330/A340 ENHANCED 07 APR 11 Applicable to: MSN 0968-1118 S16983 NAVIGATION - WEATHER RADAR SYSTEM - INSTALL COLLINS DUAL CONTROL PANEL CAPABLE OF MULTISCAN FUNCTION 07 APR 11 Applicable to: MSN 0700-1118 S16985 INFORMATION SYSTEMS - GENERAL - CERTIFY FANS A+ CONFIGURATIONS (OVERALL MODIFICATION) 30 AUG 10 Applicable to: MSN 0968-1118 S17494 GENERAL-TECHNICAL INFO ,WEIGHT AND GC - INCREASE MAXIMUM OPERATING ALTITUDE FROM 41100 TO 41450 FEET 30 AUG 10 Applicable to: MSN 0700-1118 S17828 36-3030 01 INDICATING/RECORDING SYSTEM - EIS - INSTALL NEW EIS2 STANDARD L3-1 (DMC, DU AND DISKS) 30 AUG 10 Applicable to: ALL S17830 PNEUMATIC - LEAK DETECTION - INSTALL BMC "M4" STANDARD ON A330 A/C 30 AUG 10 Applicable to: MSN 0700-1118 S18094 INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER - INSTALL NEW FWC STANDARD K8 ON A330 30 AUG 10 FLIGHT CONTROL - FLIGHT CONTROL PRIMARY COMPUTER (FCPC) - INTRODUCE TRIM SETTING AUTOMATIC FUNCTION 30 AUG 10 NAVIGATION-ADIRS-INTRODUCE AIR DATA MONITORING FUNCTION 30 AUG 10 AUTO-FLIGHT - MCDU - INSTALL 3 LCD MCDU HONEYWELL 30 AUG 10 Applicable to: MSN 0968-1118 S18568 31-3104 02 NAVIGATION - SWITCHING AND INDICATING - REMOVE DDRMI INDICATORS 30 MAY 12 Applicable to: MSN 0232-0472 S18711 INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER - INSTALL FWC STANDARD K9-486 ON A330 30 AUG 10 Applicable to: MSN 0968-1118 S18882 AUTO-FLIGHT - MCDU - INSTALL NEW MCDU LCD HONEYWELL (REBOND STANDARD) 30 AUG 10 Applicable to: MSN 0968-1118 S19212 NAVIGATION - DME - RELOCATE DME1 POWER SUPPLY TO PROVIDE POWER IN EMERGENCY FOR A330 30 AUG 10 NAVIGATION - RADIO MAGNETIC INFORMATION SWITCHING AND INDICATING - RE-INSTALL DDRMI P/N 63534-253-4 Applicable to: ALL S16262 Applicable to: MSN 0968-1118 S16279 Applicable to: MSN 1112-1118 S18144 34-3213 04 34-5060 03 Applicable to: MSN 0700-1118 S18168 Applicable to: MSN 0968-1118 S18222 Applicable to: MSN 0968-1118 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK (1) M 4/4 PRELIMINARY PAGES LIST OF MODIFICATIONS 01 DEC 14 Continued from the previous page MODIFICATION S19417 Applicable to: ALL S30132 Linked SB 31-3125 01 31-5038 01 Incorp. Date Applicable to: MSN 1112-1118 S30498 72-3020 01 Title 30 AUG 10 INDICATING / RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) - INSTALL FWC STANDARD T2-0. 30 MAY 12 ENGINE - GENERAL -INTRODUCE NEW PW4170 "ADVANTAGE 70" ENGINE ON A330 A/C 30 MAY 12 ENGINE-GENERAL-INTRODUCE NEW PW4168A-ID "ADVANTAGE 70" ENGINE ON A330 A/C PRODUCTION SOLUTION - CNF PW33-0138 Applicable to: MSN 1112-1118 S30672 31-3146 02 31-5043 01 Applicable to: MSN 0700-1118 S30734 07 APR 11 INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC STANDARD T3-0 ON LR A/C 30 MAY 12 Applicable to: MSN 1112-1118 S31353 31-3154 00 ENGINE FUEL AND CONTROL - FADEC - INTRODUCE NEW FADEC SOFTWARE STANDARD SCN10A ON PW4000 ENGINES 07 APR 11 Applicable to: MSN 0700-1118 31-3096 01 INDICATING RECORDING SYSTEMS - FWC - ACTIVATE MONITORING OF ATC/XPDR FAULTS 05 MAR 14 Applicable to: MSN 0232-0472 31-3105 00 INDICATING/RECORDING SYSTEM - DMC ACQUISITION/INTERFACE - INSTALL NEW DMC S/W V512X STD ON A330. 30 AUG 10 Applicable to: MSN 0232-0472 34-3165 01 INDICATING/RECORDING SYSTEM - FWC - INSTALL NEW FWC K8-1 WITH 386 BASED CPU BOARD ON A330. 05 MAR 14 NAVIGATION - ADIRS - INSTALL NEW HONEYWELL ADIRU STANDARD - AE22. Applicable to: MSN 0238-0259, 0466-0472 (1) Evolution code : N=New, R=Revised, E=Effectivity TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK GENERAL TABLE OF CONTENTS GEN 1/2 01 DEC 14 Important.........................................................................................GEN.01A General Information........................................................................GEN.02A TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK GENERAL TABLE OF CONTENTS Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE GEN 2/2 01 DEC 14 A330 GENERAL QUICK REFERENCE HANDBOOK GEN.01A 01 DEC 14 IMPORTANT Ident.: GEN-A-00010448.0001001 / 17 AUG 10 Applicable to: ALL SCOPE The QRH contains some specific procedures which are not displayed on the ECAM. As a general rule, procedures displayed on the ECAM are not provided in the QRH (Refer to FCOM PRO/ABN). Ident.: GEN-A-00010465.0001001 / 01 DEC 14 Applicable to: ALL TASK SHARING FOR ABN/EMER PROC For all abnormal/emergency procedures, the tasksharing is as follows: PF : Pilot flying - Responsible for the: ‐ Thrust levers ‐ Flight path and airspeed control ‐ Aircraft configuration (Request configuration change) ‐ Navigation ‐ Communications PM : Pilot monitoring - Responsible for: ‐ Monitoring and reading aloud the ECAM and checklists ‐ Performing required actions or actions requested by the PF, if applicable ‐ Using engine master switches, reset buttons, IR and guarded switches with PF's confirmation (except on ground). Ident.: GEN-A-00010466.0001001 / 17 AUG 10 Applicable to: ALL ECAM CLEAR DO NOT CLEAR ECAM WITHOUT CROSS-CONFIRMATION OF BOTH PILOTS. Ident.: GEN-A-00010467.0001001 / 21 MAR 11 Applicable to: ALL ABN/EMER PROC INITIATION Procedures are initiated on pilot flying command. No action will be taken (apart from audio warning cancel through MASTER WARN light) until: ‐ The appropriate flight path is established and, ‐ The aircraft is at least 400 ft above the runway, if a failure occurs during takeoff, approach, or go around. (In some emergency cases, provided the appropriate flight path is established, the pilot flying may initiate actions before the height). Ident.: GEN-A-00010468.0001001 / 01 DEC 14 Applicable to: ALL NORMAL CHECKLIST Normal C/L are initiated by the PF and read by the PM. The PF shall respond after having checked the existing configuration. When both pilots have to respond, "BOTH" is indicated. Ident.: GEN-A-00014735.0001001 / 08 FEB 13 Applicable to: ALL DEFINITIONS OF WARNINGS, CAUTIONS AND NOTES The following are the official definitions of warnings, cautions and notes taken directly from the JAR25/CS-25 and applicable to Airbus flight operation documentation: WARNING An operating procedure, technique, etc. that may result in personal injury or loss of life if not followed. CAUTION An operating procedure, technique, etc. that may result in damage to equipment if not followed. NOTE An operating procedure, technique, etc. considered essential to emphasize. Information contained in notes may also be safety related. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE GENERAL A330 QUICK REFERENCE HANDBOOK GEN.02A 01 DEC 14 GENERAL INFORMATION Ident.: GEN-B-00015231.0001001 / 24 FEB 14 Applicable to: ALL QRH REVISION DATE The update of the FCOM does not necessarily result in the update of the QRH. Therefore, the revision dates of the QRH and of the FCOM may differ. Ident.: GEN-B-00013895.0001001 / 23 MAR 11 Applicable to: ALL EFFECTIVITY As QRH is published at aircraft level, each paper page has only one effectivity. Ident.: GEN-B-00013879.0001001 / 28 FEB 14 Applicable to: ALL PAGE NUMBERING The page numbering follows the following rules: 01A, 02A, 02B,.. : Numbering and Index (A, B, ...) for GEN, ABN, OPS, OEB PROC sections Note: For these sections, the procedures start with the index A and for long procedures (more than one page), the index continues with B, C... 1/10, 3/5, ... C1, C2 C3 "BLANK" : : : : Numbering for NP-NP, PER Back cover page interior Back cover page exterior Index of an intentionally left blank paper page created to ensure the correct format of the next chapter (begins on recto page) Ident.: GEN-B-00013894.0001001 / 01 DEC 14 Applicable to: ALL PRELIMINARY PAGES WITHIN THE QRH BINDER It is essential for Airlines to correctly manage the updates of the QRH. For this purpose, Airbus publishes Preliminary Pages (PLP) with each QRH revision. These PLP are used as reference documents for Airlines to manage the QRH updates, e.g. easily insert the revisions, identify the modifications that impact the QRH, get a synthesis of changes introduced with each revision. However, when the QRH revisions have been incorporated in accordance with the information given in the PLP, these pages do not bring operational added value and therefore are no longer useful in the QRH binder for any operational purposes. Therefore, to minimize the size of the QRH binder on board the aircraft and to optimize the operational use of the QRH, Airbus has no objection that the Airlines remove the PLP from the QRH after the revisions have been incorporated in the QRH and all checks performed to confirm the revisions have been correctly incorporated. You will find below the list of PLP that may be removed from the QRH binder : ‐ The transmittal letter ‐ The List of Effective Preliminary Pages (LEPP) ‐ The Filing Instructions (FI) ‐ The List of Effective Documentary Units (the LESS is the reference) ‐ The List Of Modifications (LOM) ‐ The Summary Of Highlights (SOH) ‐ The front pages of all QRH sections ‐ The Table Of Contents (TOC) of the General section. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS ABN 1/4 01 DEC 14 Auto-Flight ABN-22 Loss of FMS Data In Descent/Approach (Severe Reset)...................22.01A MCDU 1(2)(3) Failure.........................................................................22.02A Electrical ABN-24 ELEC EMER CONFIG Sys-Remaining.............................................. 24.01A ELEC EMER CONFIG Summary..................................................... 24.02A Equipment ABN-25 Cockpit Door Fault............................................................................. 25.01A Fire Protection ABN-26 SMOKE/FUMES/AVNCS SMOKE.....................................................26.01A REMOVAL OF SMOKE/FUMES....................................................... 26.02A SMOKE/FIRE FROM LITHIUM BATTERY........................................ 26.03A Flight Controls ABN-27 LANDING WITH SLATS OR FLAPS JAMMED................................. 27.01A No Flaps no Slats Landing................................................................ 27.03A Sidestick / Rudder Pedals Stiff.......................................................... 27.04A Rudder Jam/Rudder Pedal Jam.........................................................27.05A Rudder Trim Runaway....................................................................... 27.06A Fuel ABN-28 FUEL IMBALANCE............................................................................ 28.01A FUEL LEAK........................................................................................28.02A FUEL LOSS REDUCTION................................................................. 28.03A FUEL JETTISON................................................................................28.04A GRVTY FUEL FEEDING....................................................................28.05A TRIM TANK FUEL UNUSABLE......................................................... 28.06A Hydraulic ABN-29 HYD B+Y SYS LO PR Summary..................................................... 29.01A HYD G+B SYS LO PR Summary.....................................................29.02A HYD G+Y SYS LO PR Summary.....................................................29.03A Ice and Rain Protection ABN-30 Double AOA Heat Failure.................................................................. 30.01A TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS ABN 2/4 01 DEC 14 Continued from the previous page Indicating / Recording Systems ABN-31 Display Unit Failure............................................................................31.01A ECAM Single Display.........................................................................31.02A EIS DISPLAY DISCREPANCY.......................................................... 31.03A Landing Gear ABN-32 Loss of Braking................................................................................32.01A L/G Gravity Extension .......................................................................32.03A Landing with Abnormal L/G................................................................32.04A Navigation ABN-34 Abnormal V Alpha Prot...................................................................... 34.01A ADR CHECK PROC.......................................................................... 34.02A Unreliable Speed Indication............................................................... 34.02A ALL ADR OFF...................................................................................34.03A ADR 1 + 2 + 3 FAULT.......................................................................34.04A NAV FM / GPS POS DISAGREE...................................................... 34.05A IR Alignment in ATT Mode................................................................ 34.06A EGPWS Alerts...................................................................................34.07A TCAS Warnings................................................................................ 34.08A Pneumatic ABN-36 AIR ENG 1+2 BLEED FAULT............................................................36.01A Engines ABN-70 ENG ALL ENG FLAMEOUT - FUEL REMAINING........................... 70.01A ENG ALL ENG FLAMEOUT - NO FUEL REMAINING.....................70.02A ENG RELIGHT (IN FLIGHT)..............................................................70.03A ENG 1(2) STALL................................................................................70.04A ENG Tailpipe Fire.............................................................................. 70.05A HIGH ENGINE VIBRATION............................................................... 70.06A Suspected ENG Fuel Sys Contamination.......................................... 70.07A ENG Fuel Sys Contamination............................................................ 70.07B Miscellaneous ABN-80 Circling Approach with One Engine Inoperative................................ 80.01A Bomb on Board.................................................................................. 80.02A Ditching............................................................................................. 80.03A Forced Landing................................................................................ 80.04A EMER DESCENT...............................................................................80.05A TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS ABN 3/4 01 DEC 14 Continued from the previous page Overspeed Recovery..........................................................................80.06A Overweight Landing........................................................................... 80.07A Stall Recovery.................................................................................. 80.08A Stall Warning at Liftoff.................................................................... 80.08A Tailstrike............................................................................................. 80.09A Volcanic Ash Encounter.....................................................................80.10A Windshear......................................................................................... 80.11A Windshear Ahead.............................................................................80.12A Cockpit Windshield / Window Arcing................................................. 80.13A Cockpit Windshield / Window Cracked.............................................. 80.14A ECAM Advisory Conditions................................................................ 80.15A Tripped C/B Re - Engagement.......................................................... 80.16A Computer Reset - General.................................................................80.17A Computer Reset Table.......................................................................80.18A Emergency Evacuation...........................................................................C2 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABN 4/4 01 DEC 14 A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 22.01A 01 DEC 14 LOSS OF FMS DATA IN DESCENT/APPROACH (SEVERE RESET) Ident.: ABN-22-00010477.0001001 / 08 FEB 13 Applicable to: ALL AP/FD lateral and vertical selected modes, and A/THR, are available immediately after the reset. If necessary, the pilot may perform the FCU selections for short-term navigation. When the FMS has automatically recovered: ‐ The database cycle may have changed ‐ The FMGES does not autotune the ILS and ADF ‐ The FMS position bias is lost ‐ Lateral and vertical managed modes cannot re-engage ‐ The ″CAB PR LDG ELEV FAULT″ message is displayed on the ECAM ‐ The ″REENTER WEIGHT/CG″ MCDU message is displayed. Depending on the flight phase, apply the following procedure(s) as appropriate: INITIAL APPROACH OR CLOSE TO ILS INTERCEPTION When the system has recovered: Access the RAD NAV page, and manually tune the ILS (preferably using Ident). Enter the ILS course, if a frequency has been entered. Fly in selected speed. Note: ‐ LOC and G/S guidance modes are available ‐ VLS speed is still available and displayed on the PFD ‐ Missed approach trajectory is not available. DESCENT (IF TIME PERMITS): When the system has recovered: Select the initial database cycle. Perform DIR TO a downpath waypoint. Select heading, if required. Perform a LAT REV at the downpath waypoint, and redefine the DESTINATION in the NEW DEST field. Redefine the arrival and/or the approach procedure. Select the FUEL PRED page, and enter the GW and CG values read on the ECAM fuel page. Activate the APPROACH phase. Enter the destination data on the PERF APPR page, as required. Managed speed is available. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 22.02A 01 DEC 14 MCDU 1(2)(3) FAILURE Ident.: ABN-22-00010479.0001001 / 08 FEB 13 Applicable to: MSN 0232-0700 BRT KNOB (on affected MCDU)...........................................................................OFF MCDU 3 automatically replaces MCDU 1 or 2. MCDU 1(2)(3) FAILURE Ident.: ABN-22-00010479.0002001 / 08 FEB 13 Applicable to: MSN 0968-1118 DIM KEY (on affected MCDU)......................................................................... PRESS Press the DIM key for a few seconds until the MCDU turns off. MCDU 3 automatically replaces MCDU 1 or 2. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK 24.01A ABNORMAL AND EMERGENCY PROCEDURES 01 DEC 14 ELEC EMER CONFIG SYS-REMAINING Applicable to: MSN 0232-0472 ELEC EMER CONFIG SYS REMAINING EMER GEN RUNNING BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) PRESS AUTO SYS 1 Norm Norm Norm Norm MAN PRESS CTL inop inop inop Norm Norm Norm Norm Norm Ident.: ABN-24-SYN-00010481.0001001 / 17 NOV 14 AIR COND RAM AIR PRESS PACK VALVE VENT Norm Norm Norm Norm AVIONIC VENT OVBD only OVBD only OVBD only OVBD only CARGO VENT ISOL valve only inop inop inop FMGC 1 only inop inop inop AUTO FLT MCDU 1 only inop inop 3 only 1 only 1 only 1 only 1 only VHF 1 Norm Norm Norm Norm HF 1 Norm (a) inop inop inop RMP 1 Norm Norm Norm Norm ACP (CAPT., F/O) Norm Norm Norm Norm CIDS Norm Norm Norm Norm INTERPHONE Norm Norm Norm Norm CVR Norm inop inop inop LOUDSPEAKER 1 + 2 Norm Norm Norm Norm ENG LOOPS A only A only A only A only APU LOOP A only A only A only Norm CARGO SMOKE DET 1 only inop inop inop ENG FIRE EXT. Squib A Squib A Squib A Squib A APU FIRE EXT. Squib A Squib A Squib A Squib A CARGO FIRE EXT. Squib A Squib A Squib A Squib A APU AUTO EXT. - - - Norm PRIM 1 Norm Norm Norm Norm SEC 2 Norm Norm Norm Norm SEC 1 Norm Norm Norm Norm FCDC 1 Norm inop inop inop SFCC SLATS 1 only (b) 1 only (b) 1 only 1 only SFCC FLAPS 1 only (b) inop inop inop PITCH TRIM 1 only inop inop inop RUDD TRIM Norm (c) inop inop inop RUDD TRAVEL Norm Norm Norm Norm Ident.: ABN-24-SYN-00010488.0001001 / 17 NOV 14 FCU Ident.: ABN-24-SYN-00010489.0001001 / 17 NOV 14 COM Ident.: ABN-24-SYN-00010491.0002001 / 17 NOV 14 FIRE Ident.: ABN-24-SYN-00010492.0004001 / 01 DEC 14 FLT CTL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01B ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 01 DEC 14 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) FCMC 1 only inop inop 2 only PUMPS L PUMP 2 (d) L PUMP 2 (d) inop inop X FEED Mot 1 only Mot 1 only Mot 1 only Mot 1 only LP VALVES Mot 1 only Mot 1 only Mot 1 only Mot 1 only XFR, ISOL VALVES Norm Norm Norm Norm AFT APU PUMPS Norm (a) Norm (a) Norm (a) Norm (a) APU LP VALVE Norm Norm Norm Norm JETTISON inop inop inop inop FIRE SOV Norm Norm Norm Norm RAT CTL Norm Norm Norm Norm ENG A. ICE Open Open Open Open WING A. ICE Norm inop inop inop CAPT PITOT Norm Norm Norm Norm Norm (e) inop inop inop CAPT AOA Norm inop inop inop STBY AOA/PITOT Norm (f) inop inop inop RAIN REPEL Capt Capt Capt Capt PFD 1 Norm Norm Norm Norm ND 1 Norm inop inop inop ECAM upper DU Norm Norm Norm Norm DMC 1 or 3 Norm Norm Norm Norm SDAC1, FWC1, ECP, CLOCK Norm Norm Norm Norm 1 only (e) 1 only (e) 1 only 1 only GRVTY EXT Norm Norm Norm Norm IND. PANEL Norm Norm Norm Norm Inop / Norm (e) inop inop inop Norm Norm Norm Norm Norm (e) inop inop inop Ident.: ABN-24-SYN-00010493.0004001 / 17 NOV 14 FUEL Ident.: ABN-24-SYN-00010494.0001001 / 17 NOV 14 HYD Ident.: ABN-24-SYN-00010495.0001001 / 17 NOV 14 ICE & RAIN WHC 1 Ident.: ABN-24-SYN-00010496.0001001 / 17 NOV 14 EIS Ident.: ABN-24-SYN-00010497.0001001 / 01 DEC 14 LGCIU L/G AUTO BRK/ANTI SKID PARK BRK Ident.: ABN-24-SYN-00010498.0001001 / 17 NOV 14 LIGHTS L LDG LT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01C ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 01 DEC 14 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) Norm Norm Norm Norm Ident.: ABN-24-SYN-00010499.0004001 / 17 NOV 14 IR 1 and 3 NAV IR 2 5 min 5 min 5 min 5 min ADR 1 Norm Norm Norm Norm ADR 3 Norm (h) inop inop inop VOR or ADF (g) 1 only 1 only 1 only 1 only DME 1 only inop inop inop MMR 1 only 1 only 1 only 1 only DDRMI Norm Norm Norm Norm ATC 1 only inop inop inop RADAR 1 only inop inop inop STBY HOR/COMPASS Norm Norm Norm Norm STBY ASI (not de-iced) Norm Norm Norm Norm STBY ALTI (VIB) Norm inop inop inop Crew OXY valve CTL Norm inop inop inop PAX OXY Norm Norm Norm Norm ENG BLEED BMC 2 inop BMC 2 inop BMC 2 inop BMC 2 inop X BLEED man only man only man only man only Norm Norm Norm Norm Norm Norm Norm Norm FADEC's, IGNITION A only A only A only A only REV inop inop inop Norm HP VALVE closure Norm Norm Norm Norm Ident.: ABN-24-SYN-00010500.0001001 / 17 NOV 14 OXYGEN Ident.: ABN-24-SYN-00010501.0001001 / 17 NOV 14 PNEU Ident.: ABN-24-SYN-00010502.0001001 / 17 NOV 14 APU Ident.: ABN-24-SYN-00010503.0001001 / 17 NOV 14 DOORS SLIDES ARM WARN Ident.: ABN-24-SYN-00010504.0001001 / 17 NOV 14 PWR PLT (a) Shed when LAND RECOVERY ON. (b) Operative when LAND RECOVERY pb is ON. However the FLAPS remain lost, if ENG 2 is failed and IDG 1 is lost. (c) RUDDER TRIM is operative, but position indicator is lost on center pedestal. (d) Crossfeed valve automatically opens. ‐ If L PUMP 2 is inoperative, R PUMP 2 takes over. ‐ Remaining pump is lost when the LAND RECOVERY pb is ON. When supplied by the RAT only, the remaining pump is lost when speed is below 260 kt. (e) Operative when LAND RECOVERY pb is ON. (f) Shed when the LAND RECOVERY pb is ON, unless the AIR DATA selector is switched ”to CAPT ON 3”. (g) Only VOR1 or ADF1 (as selected on the DDRMI) is available at a time. If the DDRMI is deactivated, only VOR 1 is available on the ND (ADF 1 will not be available independently of the selection performed on the DDRMI). (h) Shed when the LAND RECOVERY pb is ON, unless the AIR DATA selector is switched ”to CAPT ON 3”. (This leads to loss of the autopilot). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK 24.01D ABNORMAL AND EMERGENCY PROCEDURES 01 DEC 14 ELEC EMER CONFIG SYS-REMAINING Applicable to: MSN 0700 ELEC EMER CONFIG SYS REMAINING EMER GEN RUNNING BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) PRESS AUTO SYS 1 Norm Norm Norm Norm MAN PRESS CTL inop inop inop Norm Norm Norm Norm Norm Ident.: ABN-24-SYN-00010481.0001001 / 17 NOV 14 AIR COND RAM AIR PRESS PACK VALVE VENT Norm Norm Norm Norm AVIONIC VENT OVBD only OVBD only OVBD only OVBD only CARGO VENT ISOL valve only inop inop inop FMGC 1 only inop inop inop AUTO FLT MCDU 1 only inop inop 3 only 1 only 1 only 1 only 1 only VHF 1 Norm Norm Norm Norm HF 1 Norm (a) inop inop inop RMP 1 Norm Norm Norm Norm ACP (CAPT., F/O) Norm Norm Norm Norm CIDS Norm Norm Norm Norm INTERPHONE Norm Norm Norm Norm CVR Norm inop inop inop LOUDSPEAKER 1 + 2 Norm Norm Norm Norm ENG LOOPS A only A only A only A only APU LOOP A only A only A only Norm CARGO SMOKE DET 1 only inop inop inop ENG FIRE EXT. Squib A Squib A Squib A Squib A APU FIRE EXT. Squib A Squib A Squib A Squib A CARGO FIRE EXT. Squib A Squib A Squib A Squib A APU AUTO EXT. - - - Norm PRIM 1 Norm Norm Norm Norm SEC 2 Norm Norm Norm Norm SEC 1 Norm Norm Norm Norm FCDC 1 Norm inop inop inop SFCC SLATS 1 only (b) 1 only (b) 1 only 1 only SFCC FLAPS 1 only (b) inop inop inop PITCH TRIM 1 only inop inop inop RUDD TRIM Norm (c) inop inop inop RUDD TRAVEL Norm Norm Norm Norm Ident.: ABN-24-SYN-00010488.0001001 / 17 NOV 14 FCU Ident.: ABN-24-SYN-00010489.0001001 / 17 NOV 14 COM Ident.: ABN-24-SYN-00010491.0002001 / 17 NOV 14 FIRE Ident.: ABN-24-SYN-00010492.0004001 / 01 DEC 14 FLT CTL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01E ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 01 DEC 14 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) FCMC 1 only inop inop 2 only PUMPS L PUMP 2 (d) L PUMP 2 (d) inop inop X FEED Mot 1 only Mot 1 only Mot 1 only Mot 1 only LP VALVES Mot 1 only Mot 1 only Mot 1 only Mot 1 only XFR, ISOL VALVES Norm Norm Norm Norm AFT APU PUMPS Norm (a) Norm (a) Norm (a) Norm (a) APU LP VALVE Norm Norm Norm Norm JETTISON inop inop inop inop FIRE SOV Norm Norm Norm Norm RAT CTL Norm Norm Norm Norm ENG A. ICE Open Open Open Open WING A. ICE Norm inop inop inop CAPT PITOT Norm Norm Norm Norm Norm (e) inop inop inop CAPT AOA Norm inop inop inop STBY AOA/PITOT Norm (f) inop inop inop RAIN REPEL Capt Capt Capt Capt PFD 1 Norm Norm Norm Norm ND 1 Norm inop inop inop ECAM upper DU Norm Norm Norm Norm DMC 1 or 3 Norm Norm Norm Norm SDAC1, FWC1, ECP, CLOCK Norm Norm Norm Norm 1 only (e) 1 only (e) 1 only 1 only GRVTY EXT Norm Norm Norm Norm IND. PANEL Norm Norm Norm Norm Inop / Norm (e) inop inop inop Norm Norm Norm Norm Norm (e) inop inop inop Ident.: ABN-24-SYN-00010493.0004001 / 17 NOV 14 FUEL Ident.: ABN-24-SYN-00010494.0001001 / 17 NOV 14 HYD Ident.: ABN-24-SYN-00010495.0001001 / 17 NOV 14 ICE & RAIN WHC 1 Ident.: ABN-24-SYN-00010496.0001001 / 17 NOV 14 EIS Ident.: ABN-24-SYN-00010497.0001001 / 01 DEC 14 LGCIU L/G AUTO BRK/ANTI SKID PARK BRK Ident.: ABN-24-SYN-00010498.0001001 / 17 NOV 14 LIGHTS L LDG LT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01F ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 01 DEC 14 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) Norm Norm Norm Norm Ident.: ABN-24-SYN-00010499.0008001 / 17 NOV 14 IR 1 and 3 NAV IR 2 5 min 5 min 5 min 5 min ADR 1 Norm Norm Norm Norm ADR 3 Norm (h) inop inop inop VOR or ADF (g) 1 only 1 only 1 only 1 only DME 1 only inop inop inop MMR 1 only 1 only 1 only 1 only DDRMI Norm Norm Norm Norm ATC 1 only inop inop inop RADAR 1 only inop inop inop ISIS Norm Norm Norm Norm Crew OXY valve CTL Norm inop inop inop PAX OXY Norm Norm Norm Norm ENG BLEED BMC 2 inop BMC 2 inop BMC 2 inop BMC 2 inop X BLEED man only man only man only man only Norm Norm Norm Norm Norm Norm Norm Norm A only A only A only A only Ident.: ABN-24-SYN-00010500.0001001 / 17 NOV 14 OXYGEN Ident.: ABN-24-SYN-00010501.0001001 / 17 NOV 14 PNEU Ident.: ABN-24-SYN-00010502.0001001 / 17 NOV 14 APU Ident.: ABN-24-SYN-00010503.0001001 / 17 NOV 14 DOORS SLIDES ARM WARN Ident.: ABN-24-SYN-00010504.0001001 / 17 NOV 14 FADEC's, IGNITION PWR PLT REV inop inop inop Norm HP VALVE closure Norm Norm Norm Norm (a) Shed when LAND RECOVERY ON. (b) Operative when LAND RECOVERY pb is ON. However the FLAPS remain lost, if ENG 2 is failed and IDG 1 is lost. (c) RUDDER TRIM is operative, but position indicator is lost on center pedestal. (d) Crossfeed valve automatically opens. ‐ If L PUMP 2 is inoperative, R PUMP 2 takes over. ‐ Remaining pump is lost when the LAND RECOVERY pb is ON. When supplied by the RAT only, the remaining pump is lost when speed is below 260 kt. (e) Operative when LAND RECOVERY pb is ON. (f) Shed when the LAND RECOVERY pb is ON, unless the AIR DATA selector is switched ”to CAPT ON 3”. (g) Only VOR1 or ADF1 (as selected on the DDRMI) is available at a time. If the DDRMI is deactivated, only VOR 1 is available on the ND (ADF 1 will not be available independently of the selection performed on the DDRMI). (h) Shed when the LAND RECOVERY pb is ON, unless the AIR DATA selector is switched ”to CAPT ON 3”. (This leads to loss of the autopilot). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK 24.01G ABNORMAL AND EMERGENCY PROCEDURES 01 DEC 14 ELEC EMER CONFIG SYS-REMAINING Applicable to: MSN 0968-1118 ELEC EMER CONFIG SYS REMAINING EMER GEN RUNNING BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) PRESS AUTO SYS 1 Norm Norm Norm Norm MAN PRESS CTL inop inop inop Norm Norm Norm Norm Norm Ident.: ABN-24-SYN-00010481.0001001 / 17 NOV 14 AIR COND RAM AIR PRESS PACK VALVE VENT Norm Norm Norm Norm AVIONIC VENT OVBD only OVBD only OVBD only OVBD only CARGO VENT ISOL valve only inop inop inop FMGC 1 only inop inop inop AUTO FLT MCDU 1 only inop inop 3 only 1 only 1 only 1 only 1 only VHF 1 Norm Norm Norm Norm HF 1 Norm (a) inop inop inop RMP 1 Norm Norm Norm Norm ACP (CAPT., F/O) Norm Norm Norm Norm CIDS Norm Norm Norm Norm INTERPHONE Norm Norm Norm Norm CVR Norm inop inop inop LOUDSPEAKER 1 + 2 Norm Norm Norm Norm ENG LOOPS A only A only A only A only APU LOOP A only A only A only Norm CARGO SMOKE DET 1 only inop inop inop ENG FIRE EXT. Squib A Squib A Squib A Squib A APU FIRE EXT. Squib A Squib A Squib A Squib A CARGO FIRE EXT. Squib A Squib A Squib A Squib A APU AUTO EXT. - - - Norm PRIM 1 Norm Norm Norm Norm SEC 2 Norm Norm Norm Norm SEC 1 Norm Norm Norm Norm FCDC 1 Norm inop inop inop SFCC SLATS 1 only (b) 1 only (b) 1 only 1 only SFCC FLAPS 1 only (b) inop inop inop PITCH TRIM 1 only inop inop inop RUDD TRIM Norm (c) inop inop inop RUDD TRAVEL Norm Norm Norm Norm Ident.: ABN-24-SYN-00010488.0001001 / 17 NOV 14 FCU Ident.: ABN-24-SYN-00010489.0001001 / 17 NOV 14 COM Ident.: ABN-24-SYN-00010491.0002001 / 17 NOV 14 FIRE Ident.: ABN-24-SYN-00010492.0004001 / 01 DEC 14 FLT CTL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01H ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 01 DEC 14 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) FCMC 1 only inop inop 2 only PUMPS L PUMP 2 (d) L PUMP 2 (d) inop inop X FEED Mot 1 only Mot 1 only Mot 1 only Mot 1 only LP VALVES Mot 1 only Mot 1 only Mot 1 only Mot 1 only XFR, ISOL VALVES Norm Norm Norm Norm AFT APU PUMPS Norm (a) Norm (a) Norm (a) Norm (a) APU LP VALVE Norm Norm Norm Norm JETTISON inop inop inop inop FIRE SOV Norm Norm Norm Norm RAT CTL Norm Norm Norm Norm ENG A. ICE Open Open Open Open WING A. ICE Norm inop inop inop CAPT PITOT Norm Norm Norm Norm Norm (e) inop inop inop CAPT AOA Norm inop inop inop STBY AOA/PITOT Norm (f) inop inop inop RAIN REPEL Capt Capt Capt Capt PFD 1 Norm Norm Norm Norm ND 1 Norm inop inop inop ECAM upper DU Norm Norm Norm Norm DMC 1 or 3 Norm Norm Norm Norm SDAC1, FWC1, ECP, CLOCK Norm Norm Norm Norm 1 only (e) 1 only (e) 1 only 1 only GRVTY EXT Norm Norm Norm Norm IND. PANEL Norm Norm Norm Norm Inop / Norm (e) inop inop inop Norm Norm Norm Norm Norm (e) inop inop inop Ident.: ABN-24-SYN-00010493.0004001 / 17 NOV 14 FUEL Ident.: ABN-24-SYN-00010494.0001001 / 17 NOV 14 HYD Ident.: ABN-24-SYN-00010495.0001001 / 17 NOV 14 ICE & RAIN WHC 1 Ident.: ABN-24-SYN-00010496.0001001 / 17 NOV 14 EIS Ident.: ABN-24-SYN-00010497.0001001 / 01 DEC 14 LGCIU L/G AUTO BRK/ANTI SKID PARK BRK Ident.: ABN-24-SYN-00010498.0001001 / 17 NOV 14 LIGHTS L LDG LT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01I ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 01 DEC 14 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) Norm Norm Norm Norm Ident.: ABN-24-SYN-00010499.0017001 / 17 NOV 14 IR 1 and 3 NAV IR 2 5 min 5 min 5 min 5 min ADR 1 Norm Norm Norm Norm ADR 3 Norm (h) inop inop inop VOR or ADF (g) 1 only 1 only 1 only 1 only DME 1 only 1 only 1 only 1 only MMR 1 only 1 only 1 only 1 only DDRMI Norm Norm Norm Norm ATC 1 only inop inop inop RADAR 1 only inop inop inop ISIS Norm Norm Norm Norm Crew OXY valve CTL Norm inop inop inop PAX OXY Norm Norm Norm Norm ENG BLEED BMC 2 inop BMC 2 inop BMC 2 inop BMC 2 inop X BLEED man only man only man only man only Norm Norm Norm Norm Norm Norm Norm Norm A only A only A only A only Ident.: ABN-24-SYN-00010500.0001001 / 17 NOV 14 OXYGEN Ident.: ABN-24-SYN-00010501.0001001 / 17 NOV 14 PNEU Ident.: ABN-24-SYN-00010502.0001001 / 17 NOV 14 APU Ident.: ABN-24-SYN-00010503.0001001 / 17 NOV 14 DOORS SLIDES ARM WARN Ident.: ABN-24-SYN-00010504.0001001 / 17 NOV 14 FADEC's, IGNITION PWR PLT REV inop inop inop Norm HP VALVE closure Norm Norm Norm Norm (a) Shed when LAND RECOVERY ON. (b) Operative when LAND RECOVERY pb is ON. However the FLAPS remain lost, if ENG 2 is failed and IDG 1 is lost. (c) RUDDER TRIM is operative, but position indicator is lost on center pedestal. (d) Crossfeed valve automatically opens. ‐ If L PUMP 2 is inoperative, R PUMP 2 takes over. ‐ Remaining pump is lost when the LAND RECOVERY pb is ON. When supplied by the RAT only, the remaining pump is lost when speed is below 260 kt. (e) Operative when LAND RECOVERY pb is ON. (f) Shed when the LAND RECOVERY pb is ON, unless the AIR DATA selector is switched ”to CAPT ON 3”. (g) Only VOR1 or ADF1 (as selected on the DDRMI) is available at a time. If the DDRMI is deactivated, only VOR 1 is available on the ND (ADF 1 will not be available independently of the selection performed on the DDRMI). (h) Shed when the LAND RECOVERY pb is ON, unless the AIR DATA selector is switched ”to CAPT ON 3”. (This leads to loss of the autopilot). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 24.02A 01 DEC 14 ELEC EMER CONFIG SUMMARY Applicable to: MSN 0232-0700 Ident.: ABN-24-SUM-00010480.0014001 / 28 APR 14 CRUISE SPD BRK...................................................................................................................................DO NOT USE MAX SPD............................................................................................................................................. 330/.82 ALTN LAW : PROT LOST ONLY CAPT PITOT AND AOA PROBES HEATED FUEL: Center tank: 15 t (33 000 lb) unusable AUTOFLIGHT: AP1 only NAV: ILS1, GLS1 , VOR1, GPS1 only COM: HF1, VHF1, ATC1, RMP1 only For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-24-SUM-00010483.0006001 / 17 NOV 14 APPROACH CAT 2 INOP FOR LANDING............................................................................................................................USE FLAP 3 SLATS FLAPS SLOW For slats extension: RAT MAN............................................................................................................................................. ON MINIMUM RAT SPEED 140 kt LAND RECOVERY...............................................................................................................................ON FUEL: 2 t unusable in each Inner Tank. L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN USE MAN PITCH TRIM Ident.: ABN-24-SUM-00010484.0001001 / 17 AUG 10 LANDING FLARE: Only 3 spoilers per wing. Direct law. SPOILERS: Only 3 per wing NO REVERSER BRAKING: NORMAL NO NOSEWHEEL STEERING Ident.: ABN-24-SUM-00010485.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION FUEL: Increased fuel consumption (Refer to QRH PER-B) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 24.02B 01 DEC 14 ELEC EMER CONFIG SUMMARY Applicable to: MSN 0968-1118 Ident.: ABN-24-SUM-00010480.0015001 / 28 APR 14 CRUISE SPD BRK...................................................................................................................................DO NOT USE MAX SPD............................................................................................................................................. 330/.82 ALTN LAW : PROT LOST ONLY CAPT PITOT AND AOA PROBES HEATED FUEL: Center tank: 15 t (33 000 lb) unusable AUTOFLIGHT: AP1 only NAV: ILS1, GLS1 , DME1, VOR1, GPS1 only COM: HF1, VHF1, ATC1, RMP1 only For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-24-SUM-00010483.0006001 / 17 NOV 14 APPROACH CAT 2 INOP FOR LANDING............................................................................................................................USE FLAP 3 SLATS FLAPS SLOW For slats extension: RAT MAN............................................................................................................................................. ON MINIMUM RAT SPEED 140 kt LAND RECOVERY...............................................................................................................................ON FUEL: 2 t unusable in each Inner Tank. L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN USE MAN PITCH TRIM Ident.: ABN-24-SUM-00010484.0001001 / 17 AUG 10 LANDING FLARE: Only 3 spoilers per wing. Direct law. SPOILERS: Only 3 per wing NO REVERSER BRAKING: NORMAL NO NOSEWHEEL STEERING Ident.: ABN-24-SUM-00010485.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION FUEL: Increased fuel consumption (Refer to QRH PER-B) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 25.01A 01 DEC 14 COCKPIT DOOR FAULT Ident.: ABN-25-00010505.0002001 / 08 FEB 13 Applicable to: ALL This procedure should be applied, if the Cockpit Door Locking System (CDLS) fails. This failure is indicated when the FAULT light on the center pedestal’s CKPT DOOR panel comes on. CKPT DOOR CONT panel...............................................................................CHECK This panel is located on the overhead panel. It is used to identify the faulty CDLS item, and to verify the status of the pressure sensors and the three electrical latches (referred to as strikes). If two or more electrical latches (strikes) are faulty (C/Bs tripped): The cockpit door is not intrusion-proof. The system may be recovered by performing the following steps: Cockpit door.................................................................................................. OPEN C/Bs..................................................................................................... REENGAGE Note: Only one re-engagement should be attempted. Further C/B tripping requires maintenance action to determine the nature of the failure. COCKPIT DOOR toggle switch.............................................................. RECYCLE Note: This procedure allows the recovery of CDLS normal operation when C/Bs are tripped. If two pressure sensors are faulty: Automatic latch release is unavailable, in case of cockpit decompression. If no LED on the CKPT DOOR CONT panel is on: The CDLS control unit is faulty, therefore, the cockpit door might unlock automatically. If it does not, consider using the cockpit door handle from inside the cockpit to unlock the door Note: In case of a DC BUS 2 fault, no FAULT indication appears on the center pedestal’s CKPT DOOR panel. The CDLS is not electrically-supplied, and is inoperative. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 QUICK REFERENCE HANDBOOK Applicable to: MSN 0232-0472 ABNORMAL AND EMERGENCY PROCEDURES 26.01A 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE Ident.: ABN-26-A-00010507.0001001 / 20 SEP 13 LAND ASAP APPLY IMMEDIATELY IF REQUIRED: CREW OXY MASKS................... USE/100%/EMERG VENT EXTRACT................................................... OVRD CAB FANS................................................................OFF GALLEYS..................................................................OFF SIGNS.........................................................................ON CKPT/CAB COM.......................................... ESTABLISH IF SMOKE SOURCE IMMEDIATELY OBVIOUS, ACCESSIBLE AND EXTINGUISHABLE: FAULTY EQPT.............................................ISOLATE IF SMOKE SOURCE NOT IMMEDIATELY ISOLATED: DIVERSION.................................................. INITIATE DESCENT.....................................................INITIATE Descent to FL 100, or MEA-MORA, or min obstacle clearance altitude At ANY TIME of the procedure, if smoke/fumes becomes the GREATEST THREAT: REMOVAL OF SMOKE/FUMES..............CONSIDER ELEC EMER CONFIG.............................CONSIDER Refer to the end of the procedure to set ELEC EMER CONFIG TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01B 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE (Cont'd) At ANY TIME of the procedure, if situation becomes UNMANAGEABLE: IMMEDIATE LANDING............................CONSIDER Ident.: ABN-26-A-00010510.0003001 / 27 NOV 12 If AIR COND SMOKE SUSPECTED: APU BLEED.........................................................OFF VENT EXTRACT............................................... AUTO ALL CARGO ISOL VALVES................................ OFF PACK 1................................................................ OFF If smoke continues: PACK 1............................................................. ON PACK 2........................................................... OFF If smoke still continues: PACK 2........................................................ ON VENT EXTRACT.....................................OVRD REMOVAL OF SMOKE/FUMES.............. CONSIDER IF CAB EQUIPMENT SMOKE SUSPECTED: If smoke continues EMER EXIT LT................................................. ON COMMERCIAL................................................ OFF SMOKE DISSIPATION.............................. CHECK FAULTY EQPT........................SEARCH/ISOLATE If smoke still continues or when faulty equipment confirmed isolated: COMMERCIAL........................................NORM REMOVAL OF SMOKE/FUMES.............. CONSIDER TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01C 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE (Cont'd) Ident.: ABN-26-A-00010511.0001001 / 27 NOV 12 IF SMOKE SOURCE CANNOT BE DETERMINED AND STILL CONTINUES OR AVNCS/ELECTRICAL SMOKE SUSPECTED: Shed AC BUS 1 as follows: GEN 2................................................. CHECK ON ECAM/ND SEL................................................. F/O ELEC/AC page......................................... SELECT BUS TIE.......................................................... OFF AC ESS FEED.............................................. ALTN GEN 1............................................................. OFF SMOKE DISSIPATION.............................. CHECK If smoke continues: GEN 1.......................................................... ON AC ESS FEED........................................NORM ECAM/ND SEL....................................... NORM Shed AC BUS 2 as follows: GEN 1................................................. CHECK ON BUS TIE............................................ CHECK OFF AC ESS FEED...............................CHECK NORM ECAM/ND SEL.............................. CHECK NORM GEN 2............................................................. OFF SMOKE DISSIPATION.............................. CHECK If smoke continues: GEN 2.......................................................... ON BUS TIE...................................................AUTO REMOVAL OF SMOKE/FUMES.............. CONSIDER ELEC EMER CONFIG..............................CONSIDER TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01D 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE (Cont'd) Ident.: ABN-26-A-00010512.0004001 / 21 MAR 11 TO SET ELEC EMER CONFIG EMER ELEC PWR.......................................... MAN ON WHEN EMER GEN AVAIL: GEN 1................................................................ OFF GEN 2................................................................ OFF APU GEN...........................................................OFF ELEC EMER CONFIG APPLY ECAM PROCEDURE, BUT DO NOT RESET GEN, EVEN IF REQUESTED BY ECAM AT 3 MIN OR 2 000 FT AAL BEFORE LANDING: ATT HDG SWTG.......................................F/O ON 3 ALL GEN..............................................................ON WHEN A/C IS STOPPED: ALL GEN............................................................OFF Applicable to: MSN 0700-1118 SMOKE/FUMES/AVNCS SMOKE Ident.: ABN-26-A-00010507.0001001 / 20 SEP 13 LAND ASAP APPLY IMMEDIATELY IF REQUIRED: CREW OXY MASKS................... USE/100%/EMERG VENT EXTRACT................................................... OVRD CAB FANS................................................................OFF GALLEYS..................................................................OFF SIGNS.........................................................................ON CKPT/CAB COM.......................................... ESTABLISH TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01E 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE (Cont'd) IF SMOKE SOURCE IMMEDIATELY OBVIOUS, ACCESSIBLE AND EXTINGUISHABLE: FAULTY EQPT.............................................ISOLATE IF SMOKE SOURCE NOT IMMEDIATELY ISOLATED: DIVERSION.................................................. INITIATE DESCENT.....................................................INITIATE Descent to FL 100, or MEA-MORA, or min obstacle clearance altitude At ANY TIME of the procedure, if smoke/fumes becomes the GREATEST THREAT: REMOVAL OF SMOKE/FUMES..............CONSIDER ELEC EMER CONFIG.............................CONSIDER Refer to the end of the procedure to set ELEC EMER CONFIG At ANY TIME of the procedure, if situation becomes UNMANAGEABLE: IMMEDIATE LANDING............................CONSIDER Ident.: ABN-26-A-00010510.0009001 / 27 NOV 12 If AIR COND SMOKE SUSPECTED: APU BLEED.........................................................OFF VENT EXTRACT............................................... AUTO ALL CARGO ISOL VALVES................................ OFF PACK 1................................................................ OFF If smoke continues: PACK 1............................................................. ON PACK 2........................................................... OFF TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01F 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE (Cont'd) If smoke still continues: PACK 2........................................................ ON VENT EXTRACT.....................................OVRD REMOVAL OF SMOKE/FUMES.............. CONSIDER IF CAB EQUIPMENT SMOKE SUSPECTED: PAX SYS..............................................................OFF If smoke continues EMER EXIT LT................................................. ON COMMERCIAL................................................ OFF SMOKE DISSIPATION.............................. CHECK FAULTY EQPT........................SEARCH/ISOLATE If smoke still continues or when faulty equipment confirmed isolated: COMMERCIAL........................................NORM PAX SYS................................................ NORM REMOVAL OF SMOKE/FUMES.............. CONSIDER Ident.: ABN-26-A-00010511.0001001 / 27 NOV 12 IF SMOKE SOURCE CANNOT BE DETERMINED AND STILL CONTINUES OR AVNCS/ELECTRICAL SMOKE SUSPECTED: Shed AC BUS 1 as follows: GEN 2................................................. CHECK ON ECAM/ND SEL................................................. F/O ELEC/AC page......................................... SELECT BUS TIE.......................................................... OFF AC ESS FEED.............................................. ALTN GEN 1............................................................. OFF TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01G 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE (Cont'd) SMOKE DISSIPATION.............................. CHECK If smoke continues: GEN 1.......................................................... ON AC ESS FEED........................................NORM ECAM/ND SEL....................................... NORM Shed AC BUS 2 as follows: GEN 1................................................. CHECK ON BUS TIE............................................ CHECK OFF AC ESS FEED...............................CHECK NORM ECAM/ND SEL.............................. CHECK NORM GEN 2............................................................. OFF SMOKE DISSIPATION.............................. CHECK If smoke continues: GEN 2.......................................................... ON BUS TIE...................................................AUTO REMOVAL OF SMOKE/FUMES.............. CONSIDER ELEC EMER CONFIG..............................CONSIDER Ident.: ABN-26-A-00010512.0004001 / 21 MAR 11 TO SET ELEC EMER CONFIG EMER ELEC PWR.......................................... MAN ON WHEN EMER GEN AVAIL: GEN 1................................................................ OFF GEN 2................................................................ OFF APU GEN...........................................................OFF ELEC EMER CONFIG APPLY ECAM PROCEDURE, BUT DO NOT RESET GEN, EVEN IF REQUESTED BY ECAM TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01H 01 DEC 14 SMOKE/FUMES/AVNCS SMOKE (Cont'd) AT 3 MIN OR 2 000 FT AAL BEFORE LANDING: ATT HDG SWTG.......................................F/O ON 3 ALL GEN..............................................................ON WHEN A/C IS STOPPED: ALL GEN............................................................OFF TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.02A 01 DEC 14 REMOVAL OF SMOKE/FUMES Ident.: ABN-26-00010506.0001001 / 01 DEC 14 Applicable to: ALL EMER EXIT LIGHT.................................................... ON PACK FLOW................................................................ HI LDG ELEV.................................. 10 000 FT/MEA-MORA DESCENT (FL 100 or MEA-MORA or minimum obstacle clearance altitude)............................................. INITIATE ATC..................................................................... NOTIFY SMOKE/FUMES/AVNCS SMOKE PROC..... CONTINUE While descending, continue applying the appropriate steps of the SMOKE/FUMES/AVNCS SMOKE paper procedure depending on the suspected smoke source. At FL 100 or MEA-MORA : PACK 1 + 2..........................................................OFF MODE SEL..........................................................MAN MAN VALVE SEL..............................................BOTH MAN V/S CTL.............................................. FULL UP RAM AIR................................................................ON If smoke persists in the cockpit, window opening: MAX SPEED................................................... 230 KT COCKPIT DOOR.............................................. OPEN HEADSET.............................................................. ON PM COCKPIT WINDOW...................................OPEN When window is open: NON-AFFECTED PACK(s)....................................ON VISUAL WARNINGS (noisy CKPT)........... MONITOR SMOKE/FUMES/ AVNCS SMOKE PROC.................. ..................................................................CONTINUE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.03A 01 DEC 14 SMOKE/FIRE FROM LITHIUM BATTERY Ident.: ABN-26-00015935.0001001 / 01 DEC 14 Applicable to: ALL If necessary, transfer control to the flight crew member seated on the opposite side of the fire CKPT/CAB COM.......................................... ESTABLISH STORAGE AFTER Li BAT FIRE cabin procedure........... .................................................... REQUEST INITIATION If there are flames: CREW OXY MASK (PF)......................................USE SMOKE HOOD (PM)........................................... USE HALON EXTINGUISHER.....................................USE If there are no flames or when flames are extinguished: If not possible to remove device from the cockpit: WATER or NON-ALCOHOLIC LIQUID.................. ................................................ POUR ON DEVICE DEVICE................................................. MONITOR If possible to remove device from the cockpit: DEVICE.............................TRANSFER TO CABIN AT ANY TIME of the procedure, if SMOKE becomes the GREATEST THREAT: SMOKE/FUMES REMOVAL procedure...CONSIDER AT ANY TIME of the procedure, if situation becomes UNMANAGEABLE: IMMEDIATE LANDING............................CONSIDER TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.01A 01 DEC 14 LANDING WITH SLATS OR FLAPS JAMMED Ident.: ABN-27-00010513.0001001 / 01 DEC 14 Applicable to: ALL LANDING CONF......................................................................................DETERMINE Refer to QRH PER-27A Landing Distance with Slats and Flaps System Failure Repeat the following until landing configuration is reached: SPEED SEL............................................................................. .VFE NEXT -5 KTS Decelerate towards VFE NEXT -5 kt but not below VLS. In case of turbulence, to avoid VFE exceedance, the pilot may decide to decelerate to a lower speed, but not below VLS. Note: ‐ The autopilot may be used down to 500 ft AGL. As it is not tuned for the abnormal configurations, its behavior can be less than optimum and must be monitored ‐ Approach with A/THR and selected speed is recommended ‐ The OVERSPEED warning, and VLS displayed on the PFD, are computed according to the actual flaps/slats position ‐ VFE and VFE NEXT are displayed on the PFD, according to the FLAPS lever position. If not displayed, use the placard speeds ‐ If VLS is greater than VFE NEXT (overweight landing case), the FLAPS lever can be set in the required next position while the speed is reduced to follow VLS reduction as surfaces extend. The VFE warning threshold should not be triggered. In this case, disconnect the A/THR. A/THR can be reengaged when the landing configuration is established. As speed reduces through VFE NEXT: FLAPS LEVER..........................................................................ONE STEP DOWN Set the FLAPS lever to a minimum of CONF1, in order to enable engagement of the SRS guidance mode, in the case of a go-around. The SRS guidance mode may not engage if the landing gear is up. When landing configuration is established: DECELERATE TO CALCULATED APPROACH SPEED IN FINAL APPROACH FOR GO AROUND If SLATS FAULT: For circuit: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPEED -10 kt For diversion: SELECT CLEAN CONFIGURATION If SLATS jammed at 0: Use normal operating speeds. If SLATS jammed > 0: Recommended speed for diversion: MAX SPEED -10 kt Increased fuel consumption. If FLAPS FAULT: For circuit: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPEED -10 kt TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 27.01B ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 01 DEC 14 LANDING WITH SLATS OR FLAPS JAMMED (Cont'd) For diversion: If FLAPS jammed at 0: SELECT CLEAN CONFIGURATION Use normal operating speeds. If FLAPS jammed > 0: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed for diversion: MAX SPEED -10 kt Increased fuel consumption. Note: ‐ In case the SPD LIM flag is displayed on the PFD, use the MAX SPEED displayed on the ECAM status page ‐ In case of a go-around with CONF FULL selected, the L/G GEAR NOT DOWN warning is triggered at landing gear retraction ‐ In some cases, MAX SPEED -10 KT may be a few knots higher than the VFE. In this situation, pilots may follow the VFE. MAX SPEED Flaps Slats F=0 S=0 NO LIMITATION 0<S≤1 240 kt 1<S 215 kt 0<F≤1 215 kt 1<F≤2 2<F≤3 F>3 196 kt 186 kt 180 kt 205 kt CAUTION For flight with SLATS or FLAPS extended, fuel consumption is increased. Refer to the fuel flow indication. As a guideline, determine the fuel consumption in clean configuration at the same altitude without airspeed limitation (e.g. From ALTERNATE FLIGHT PLANNING tables) and multiply this result by the applicable Fuel Penalty Factor provided in the QRH, Refer to QRH PER-B Fuel Penalty Factors Tables, to obtain the fuel penalty required to reach the destination in the current configuration. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 27.02A 01 DEC 14 A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.03A 01 DEC 14 NO FLAPS NO SLATS LANDING Ident.: ABN-27-00010514.0001001 / 28 FEB 14 Applicable to: ALL SPEED SEL............................................................................................ GREEN DOT Initial approach with autothrust and selected speed is recommended. Autopilot is allowed down to 500 ft AGL. GPWS FLAP MODE..............................................................................................OFF FLAPS LEVER................................................................................................ CONF 1 Disregard the CONF 2 requirement on the ECAM status page. Set the FLAPS lever to CONF1, in order to enable engagement of the SRS guidance mode, in the case of a go-around. The SRS guidance mode may not engage if the landing gear is up. VFE displayed on the PFD depends on the FLAPS lever position, so a false VFE will be given. Plan a long stabilized approach. For final approach: A/THR............................................................................................................... OFF SPD SEL........................................................................................................ VAPP Select VLS on the PFD (or VREF + 50 kt, if VLS not available). At 500 ft, reduce speed to obtain VLS - 5 kt (or VREF + 45 kt, if VLS not available) at touchdown. LDG DIST PROC......................................................................................... APPLY TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.04A 01 DEC 14 SIDESTICK / RUDDER PEDALS STIFF Ident.: ABN-27-00010515.0001001 / 01 DEC 14 Applicable to: ALL Even if the autopilot is disengaged, the sidesticks and/or the rudder pedals may be stiff. This may affect either: ‐ Both sidesticks (CAPT and F/O) at the same time, but not the rudder pedals or ‐ One sidestick and the rudder pedals at the same time. The piloting technique remains the same: The aircraft remains responsive. However, the flight crew should keep in mind that they may need to use extra force on the sidesticks and/or the rudder pedals. AP DISENGAGEMENT................................................................................ CONFIRM CONSIDER TRANSFERRING CONTROL TO PM For decrab, rollout, or engine failure: BE PREPARED TO APPLY EXTRA FORCE ON RUDDER PEDAL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.05A 01 DEC 14 RUDDER JAM/RUDDER PEDAL JAM Ident.: ABN-27-00010516.0001001 / 03 JUN 14 Applicable to: MSN 0232-0472 Rudder jamming may be detected by undue (and adverse) pedal movement during rolling maneuvers. This is because the yaw damper orders can no longer be sent to the rudder, but are fed back to the pedals. Use F/CTL SD page for a visual check of the rudder position. This procedure also applies in case of RUDDER PEDAL JAM. FOR APPROACH AVOID LANDING WITH CROSSWIND from the side where the rudder is deflected. FOR LANDING..................................................................................... USE FLAP 2 GPWS FLAP MODE...........................................................................................OFF If all engines are operative: APPR SPD............................................................................................ VLS + 10 SPEED and TRAJECTORY.....................................................STABILIZE ASAP LDG DIST PROC......................................................................................APPLY In case of an engine-out: APPR SPEED.......................................................................................160 knots SPEED and TRAJECTORY.....................................................STABILIZE ASAP AP + A/THR.................................................................................................. OFF In case of a go-around: SPD.................................................................................. SELECT 160 knots LDG DIST PROC......................................................................................APPLY ON GROUND DIFFERENTIAL BRAKING...................................................................... USE ASAP Do not use asymmetrical thrust reverse Use nosewheel steering handle below 100 kt, only in case of RUDDER PEDAL JAM. RUDDER JAM/RUDDER PEDAL JAM Ident.: ABN-27-00010516.0004001 / 03 JUN 14 Applicable to: MSN 0700-1118 Use F/CTL SD page for a visual check of the rudder position. This procedure also applies in case of RUDDER PEDAL JAM. FOR APPROACH AVOID LANDING WITH CROSSWIND from the side where the rudder is deflected. FOR LANDING..................................................................................... USE FLAP 2 GPWS FLAP MODE...........................................................................................OFF If all engines are operative: SPEED and TRAJECTORY.....................................................STABILIZE ASAP LDG DIST PROC......................................................................................APPLY In case of an engine-out: APPR SPEED.......................................................................................170 knots SPEED and TRAJECTORY.....................................................STABILIZE ASAP TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.05B 01 DEC 14 RUDDER JAM/RUDDER PEDAL JAM (Cont'd) AP + A/THR.................................................................................................. OFF In case of a go-around: SPD.................................................................................. SELECT 170 knots LDG DIST PROC......................................................................................APPLY ON GROUND DIFFERENTIAL BRAKING...................................................................... USE ASAP Do not use asymmetrical thrust reverse Use nosewheel steering handle below 100 kt, only in case of RUDDER PEDAL JAM. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 27.06A 01 DEC 14 RUDDER TRIM RUNAWAY Ident.: ABN-27-00010517.0001001 / 08 FEB 13 Applicable to: MSN 0232-0472 LATERAL CONTROL............................................................ USE TO LEVEL WINGS RUDDER.................................................................................................CENTRALIZE Check the rudder position on the F/CTL SD page Note: This failure will be seen mainly as uncommanded roll (induced by yaw). In most conditions, the aircraft will self stabilize in a steady heading sideslip. For continued flight, either maintain rudder central or leave the aircraft in a steady stabilized heading sideslip, but ensure that all changes between rudder centralized and steady heading sideslip are made smoothly. As speed is reduced, the TLU may gradually open to allow more rudder to be applied by the trim runaway. DURING APPROACH For slats extension: LOWEST SAFE SPEED.........................................................................SELECT In the case of TLU failure, the TLU will fully open when slats are extended, and allow more rudder to be applied than is safe for the structure. Full rudder is not permitted above 160 kt . RUDDER........................................................................... MAINTAIN CENTRAL Care must be taken to keep rudder steady and approximately centralized during slats extension, until the TLU has released. SEC 1.......................................................................................... OFF THEN ON SEC 2.......................................................................................... OFF THEN ON FOR LDG.......................................................................... USE NORMAL CONF RUDDER TRIM RUNAWAY Ident.: ABN-27-00010517.0002001 / 08 FEB 13 Applicable to: MSN 0700-1118 LATERAL CONTROL............................................................ USE TO LEVEL WINGS RUDDER.................................................................................................CENTRALIZE Check the rudder position on the F/CTL SD page Note: This failure will be seen mainly as uncommanded roll (induced by yaw). In most conditions, the aircraft will self stabilize in a steady heading sideslip. For continued flight, either maintain rudder central or leave the aircraft in a steady stabilized heading sideslip, but ensure that all changes between rudder centralized and steady heading sideslip are made smoothly. As speed is reduced, the FCPC may allow more rudder to be applied by the trim runaway. FOR LDG...................................................................................USE NORMAL CONF TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 28.01A 01 DEC 14 FUEL IMBALANCE Ident.: ABN-28-00010520.0001001 / 24 FEB 14 Applicable to: ALL FOB.................................................................................................................. CHECK Compare the FOB + FU, with the FOB at departure. If the difference is significant, or if the FOB + FU decreases, suspect a fuel leak. CAUTION 1.A fuel imbalance may indicate a fuel leak. Do not apply this procedure, if a fuel leak is suspected. Refer to QRH ABN-28 FUEL LEAK. 2.In the case of an ENG FEEDLINE BURST followed by an ENG SHUTDOWN, if fuel of the tank associated to the affected engine is required, do not open the WING XFEED valve and apply the procedure below that corresponds to the case of the WING XFEED valve failed closed. WING X FEED........................................................................................................ ON If the WING X FEED valve is open: On the lighter side: (ALL) FUEL PUMPS (STBY then MAIN 1 and MAIN 2)............................. OFF Note: While pumps are OFF, disregard the corresponding FUEL WING PUMPS LO PR ECAM caution. When fuel balanced: PUMPS (MAIN 1 and MAIN 2 then STBY)...................................................ON WING X FEED..........................................................................................AUTO If the WING X FEED valve is failed closed or in the case of an engine feed line burst: OUTR TK XFR................................................................................................... ON This will connect the inner fuel tanks via the refuelling gallery. STRAIGHT FLIGHT................................................................................MAINTAIN Maintain straight flight legs to apply this procedure. AP..................................................................................................................... OFF Disconnect the Auto Pilot to reach the targeted bank angle and the appropriate rudder position during the maneuver. BANK ANGLE.......................................3 DEG WING DOWN ON LIGHTER SIDE Fuel transfer only occurs if the bank angle is at, or above, 2 ° to 3 °. USE RUDDER TO KEEP HDG Adjust rudder position to keep heading and neutral stick. RUDDER TRIM............................................................................AS NECESSARY When XFR completed: OUTR TK XFR......................................................................................... AUTO NORM ROLL ATTITUDE.....................................................................RETURN RUDDER TRIM...........................................................................NORMAL USE AP ON................................................................................................AS RQRD TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 28.02A 01 DEC 14 FUEL LEAK Ident.: ABN-28-00010522.0005001 / 08 FEB 13 Applicable to: ALL A fuel leak may be detected by: ‐ The sum of FOB and FU is significantly less than FOB at engine start, or is decreasing, or ‐ A passenger observes a fuel spray from an engine/pylon, or a wing tip, or ‐ The total fuel quantity is decreasing at an abnormal rate, or ‐ A fuel imbalance is developing, or ‐ Fuel quantity of a tank is decreasing too fast (leak from engine/pylon, or hole in a tank), or ‐ A tank is overflowing (due to pipe rupture in a tank), or ‐ The Fuel Flow is excessive (leak from engine), or ‐ Fuel is smelt in the cabin. If visibility permits, leak source may be identified by a visual check from the cabin. WHEN A LEAK IS CONFIRMED LAND ASAP Leak from engine/pylon confirmed: Engine fuel leak can be confirmed by excessive fuel flow indication, or a visual check. THR LEVER (of affected engine)................................................................. IDLE ENG MASTER (of affected engine).............................................................. OFF WING X FEED............................................................................ USE AS RQRD If the leak stops, the crossfeed valve can now be opened to re-balance fuel quantity, or to enable use of fuel from both wings. Do not restart the engine. Leak from engine/pylon not confirmed or leak not located: Stop any fuel transfer, and then monitor the depletion rate of each inner tank, to determine if the leak is from an engine or a wing (case 1), or from the Center tank, the Trim tank, or the APU/Trim feeding lines (case 2). WING X FEED.....................................................................MAINTAIN CLOSED Crossfeed valve must remain closed to prevent the leak from affecting both sides. L+R CTR PUMPS......................................................................................... OFF T TANK FEED..............................................................................................ISOL INNER TANKS FUEL QUANTITIES....................................................MONITOR Monitor the depletion rate of each inner tank. CASE 1: If one inner tank depletes faster than the other by at least 500 kg (1 100 lb) in less than 30 min: An engine leak may still be suspected. Therefore: THR LEVER (engine of affected inner tank)...........................................IDLE ENG MASTER (engine of affected inner tank)........................................ OFF FUEL LEAK.................................................................................... MONITOR If leak stops: If the fuel quantity of the affected inner tank stops decreasing, the engine leak is confirmed and stopped. L+R CTR PUMPS.................................................................................ON T TANK FEED..................................................................................AUTO WING X FEED.................................................................. USE AS RQRD The crossfeed valve can now be opened to re-balance fuel quantity, or to enable use of fuel from both wings. Do not restart the engine. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 28.02B 01 DEC 14 FUEL LEAK (Cont'd) If leak continues (after engine shutdown): If the fuel quantity of the affected inner tank continues to decrease, a leak from the wing may be suspected. ENGINE RESTART................................................................. CONSIDER FUEL LOSS REDUCTION proc.............................................. CONSIDER CAUTION Do not apply the FUEL IMBALANCE procedure. Approach and landing can be done, even with one full wing/one empty wing. CASE 2: If both inner tanks deplete at a similar rate: A leak from the Center tank, the Trim tank, or the APU/Trim feeding line may be suspected. L+R CTR PUMPS...................................................................................... ON If fuel smell in the cabin: APU (if ON).........................................................................................OFF T TANK FEED................................................................. MAINTAIN ISOL This prevents additional fuel loss through the APU/Trim feeding line. If no fuel smell in the cabin: A leak from the Trim tank may be suspected. FUEL LOSS REDUCTION proc.............................................. CONSIDER FOR LANDING CAUTION Do not use reversers. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 28.03A 01 DEC 14 FUEL LOSS REDUCTION Ident.: ABN-28-00010523.0002001 / 09 AUG 10 Applicable to: ALL Apply this procedure only if suggested by the FUEL LEAK procedure, and if the flight crew needs to minimize the fuel loss. It covers two types of leak: ‐ A leak from wing: a manual Trim tank transfer (via the Center tank) and/or manual Center tank transfer can be done, to symmetrically transfer fuel to both inner tanks, and avoid automatic transfer to only the least full inner tank. ‐ A leak from the Center tank, or the Trim tank: a manual Trim and/or Center tank transfer to both inner tanks can be done to save some Trim or Center tank fuel. If Center Tank or Trim Tank not empty: L+R CTR PUMPS.............................................................................................. ON CTR TK XFR................................................................................................... MAN T TANK FEED (if not empty)........................................................................ AUTO T TANK MODE (if not empty)......................................................................... FWD When Trim Tank empty: T TANK MODE.........................................................................................AUTO T TANK FEED............................................................................................ISOL When Center Tank empty: CTR TK XFR............................................................................................ AUTO TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 28.04A 01 DEC 14 FUEL JETTISON Ident.: ABN-28-00010524.0003001 / 08 FEB 13 Applicable to: ALL ON MCDU: FUEL PRED key..........................................................................................SELECT JET GW..............................................................................ENTER THE FINAL GW ON OVERHEAD PANEL: T TANK MODE.................................................................................. CHECK AUTO JETTISON ARM................................................................................................... ON JETTISON ACTIVE.............................................................................................. ON Note: If the FUEL T TANK XFR FAULT ECAM warning is triggered, disregard the ECAM procedure. CAUTION During jettison operation, monitor the CG. If either the forward or aft takeoff and landing limit is reached, stop jettison. When jettison is completed, or to manually stop the jettison operation: JETTISON ACTIVE....................................................................................... OFF JETTISON ARM............................................................................................ OFF TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 28.05A ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 01 DEC 14 GRVTY FUEL FEEDING Ident.: ABN-28-00010525.0001001 / 08 FEB 13 Applicable to: MSN 0232-0361, 0968-1118 ENG START SEL...................................................................................................IGN AVOID NEGATIVE G FACTOR DETERMINE GRVTY FEED CEILING Consult the following table to determine the flight altitude limitation. Flight conditions at the time of gravity feeding Gravity feed ceiling Flight time from takeoff more than 30 min (Fuel deaerated) 20 000 ft Flight time from takeoff less than 30 min (Fuel non-deaerated) 15 000 ft DESCEND TO GRVTY FEED CEILING (if applicable) When reaching GRVTY feed ceiling: WING X FEED.............................................................................................CLOSE INR UNUSABLE IF < 2 000 kg (4 400 lb) 2 000 kg (4 400 lb) of fuel per affected tank cannot be used by gravity. GRVTY FUEL FEEDING Ident.: ABN-28-00010525.0003001 / 08 FEB 13 Applicable to: MSN 0466-0700 ENG START SEL...................................................................................................IGN AVOID NEGATIVE G FACTOR DETERMINE GRVTY FEED CEILING Consult the following table to determine the flight altitude limitation. Flight conditions at the time of gravity feeding Gravity feed ceiling Flight time from takeoff more than 30 min (Fuel deaerated) 20 000 ft Flight time from takeoff less than 30 min (Fuel non-deaerated) 15 000 ft 10 000 ft for JP4 or JET B DESCEND TO GRVTY FEED CEILING (if applicable) When reaching GRVTY feed ceiling: WING X FEED.............................................................................................CLOSE INR UNUSABLE IF < 2 000 kg (4 400 lb) 2 000 kg (4 400 lb) of fuel per affected tank cannot be used by gravity. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 28.06A 01 DEC 14 TRIM TANK FUEL UNUSABLE Ident.: ABN-28-00010526.0004001 / 14 SEP 12 Applicable to: ALL T TANK MODE.....................................................................................................FWD T TANK FEED.................................................................................................... OPEN If TRIM TANK FUEL is still unusable: OUTR TK XFR................................................................................................... ON CTR TK PUMPS...............................................................................................OFF MAXIMUM FLIGHT TIME........................................................................4 HOURS After 4 h, depending on the fuel distribution, the aft CG limit may be reached. FOR LANDING If CG > aft CG limit shown below: APPR SPD....................................................................................... VLS +10 KT LDG DIST PROC......................................................................................APPLY To keep the nosewheel on the runway and prevent the aircraft from sitting on its tail, apply continuous braking throughout the landing rollout. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.01A 01 DEC 14 HYD B+Y SYS LO PR SUMMARY Applicable to: MSN 0232-0361, 0968-1118 Ident.: ABN-29-SUM1-00010527.0001001 / 28 APR 14 CRUISE MAX SPD............................................................................................................................................. 330/.82 NO STABILIZER If TRIM locked above 8 UP: MAX SPD.......................................................................................................................................180 KT MANEUVER WITH CARE ALTN LAW : PROT LOST FUEL: Increased fuel consumption (Refer to QRH PER-B) For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-29-SUM1-00010531.0001001 / 08 FEB 13 APPROACH CAT 2 INOP GPWS FLAP MODE................................................................................................................................. OFF FOR LANDING............................................................................................................................USE FLAP 2 SLATS FLAPS SLOW L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN Ident.: ABN-29-SUM1-00010532.0003001 / 19 AUG 10 LANDING FLARE: PITCH AUTHORITY REDUCED (No stabilizer) Only 2 spoilers per wing SPOILERS: Only 2 per wing NO REVERSER BRAKING: NORMAL NO NOSEWHEEL STEERING Ident.: ABN-29-SUM1-00010533.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION FUEL: Increased fuel consumption (Refer to QRH PER-B) HYD B+Y SYS LO PR SUMMARY Applicable to: MSN 0466-0700 Ident.: ABN-29-SUM1-00010527.0001001 / 28 APR 14 CRUISE MAX SPD............................................................................................................................................. 330/.82 NO STABILIZER If TRIM locked above 8 UP: MAX SPD.......................................................................................................................................180 KT MANEUVER WITH CARE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES CRUISE 29.01B 01 DEC 14 Continued from the previous page ALTN LAW : PROT LOST FUEL: Increased fuel consumption (Refer to QRH PER-B) For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-29-SUM1-00010531.0001001 / 08 FEB 13 APPROACH CAT 2 INOP GPWS FLAP MODE................................................................................................................................. OFF FOR LANDING............................................................................................................................USE FLAP 2 SLATS FLAPS SLOW L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN Ident.: ABN-29-SUM1-00010532.0002001 / 19 AUG 10 LANDING FLARE: PITCH AUTHORITY REDUCED (No stabilizer) Only 2 spoilers per wing SPOILERS: Only 2 per wing REVERSERS: All avail BRAKING: NORMAL NO NOSEWHEEL STEERING Ident.: ABN-29-SUM1-00010533.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION FUEL: Increased fuel consumption (Refer to QRH PER-B) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.02A 01 DEC 14 HYD G+B SYS LO PR SUMMARY Applicable to: MSN 0232-0361, 0968-1118 Ident.: ABN-29-SUM2-00010528.0001001 / 28 APR 14 CRUISE SPD BRK...................................................................................................................................DO NOT USE MAX SPD............................................................................................................................................. 330/.82 MANEUVER WITH CARE ALTN LAW : PROT LOST FUEL: Increased fuel consumption (Refer to QRH PER-B) For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-29-SUM2-00010537.0001001 / 08 FEB 13 APPROACH CAT 2 INOP SLATS JAMMED / FLAPS SLOW GPWS FLAP MODE (if Slats < 2)............................................................................................................OFF For landing: If Slats < 2............................................................................................................................ USE FLAP 2 If Slats ≥ 2............................................................................................................................ USE FLAP 3 For Flaps extension: SPD SEL...................................................................................................................... VFE NEXT - 5 KT L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN When in landing CONF and in final approach: DECELERATE TO CALCULATED VAPP Ident.: ABN-29-SUM2-00010538.0003001 / 29 MAR 11 LANDING FLARE: Only one ELEV and 2 spoilers per wing. A/C slightly sluggish SPOILERS: Only 2 per wing REVERSERS: Only N° 2 BRAKING: B ACCU PRESS ONLY (7 applications) NO ANTI-SKID MAX BRK PR....................................................................................................................................1000 PSI NO NOSEWHEEL STEERING Ident.: ABN-29-SUM2-00010539.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION For circuit: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPD - 10 kt / 200 kt For diversion: SELECT CLEAN CONFIGURATION If Slats jammed at zero: Normal operating speeds (MAX SPD 200 kt) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES GO-AROUND If Slats jammed above zero: Recommended speed: 200 kt FUEL: Increased fuel consumption (Refer to QRH PER-B) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 29.02B 01 DEC 14 Continued from the previous page A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.02C 01 DEC 14 HYD G+B SYS LO PR SUMMARY Applicable to: MSN 0466-0700 Ident.: ABN-29-SUM2-00010528.0001001 / 28 APR 14 CRUISE SPD BRK...................................................................................................................................DO NOT USE MAX SPD............................................................................................................................................. 330/.82 MANEUVER WITH CARE ALTN LAW : PROT LOST FUEL: Increased fuel consumption (Refer to QRH PER-B) For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-29-SUM2-00010537.0001001 / 08 FEB 13 APPROACH CAT 2 INOP SLATS JAMMED / FLAPS SLOW GPWS FLAP MODE (if Slats < 2)............................................................................................................OFF For landing: If Slats < 2............................................................................................................................ USE FLAP 2 If Slats ≥ 2............................................................................................................................ USE FLAP 3 For Flaps extension: SPD SEL...................................................................................................................... VFE NEXT - 5 KT L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN When in landing CONF and in final approach: DECELERATE TO CALCULATED VAPP Ident.: ABN-29-SUM2-00010538.0002001 / 29 MAR 11 LANDING FLARE: Only one ELEV and 2 spoilers per wing. A/C slightly sluggish SPOILERS: Only 2 per wing REVERSERS: All avail. BRAKING: B ACCU PRESS ONLY (7 applications) NO ANTI-SKID MAX BRK PR....................................................................................................................................1000 PSI NO NOSEWHEEL STEERING Ident.: ABN-29-SUM2-00010539.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION For circuit: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPD - 10 kt / 200 kt For diversion: SELECT CLEAN CONFIGURATION If Slats jammed at zero: Normal operating speeds (MAX SPD 200 kt) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES GO-AROUND If Slats jammed above zero: Recommended speed: 200 kt FUEL: Increased fuel consumption (Refer to QRH PER-B) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 29.02D 01 DEC 14 Continued from the previous page A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.03A 01 DEC 14 HYD G+Y SYS LO PR SUMMARY Applicable to: MSN 0232-0361, 0968-1118 Ident.: ABN-29-SUM3-00010529.0001001 / 28 APR 14 CRUISE SPD BRK...................................................................................................................................DO NOT USE MAX SPD............................................................................................................................................. 330/.82 MANEUVER WITH CARE ALTN LAW : PROT LOST FUEL: Increased fuel consumption (Refer to QRH PER-B) For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-29-SUM3-00010543.0001001 / 08 FEB 13 APPROACH CAT 2 INOP SLATS SLOW / FLAPS JAMMED GPWS FLAP MODE (IF Flaps < 3)..........................................................................................................OFF For landing: If Flaps < 3........................................................................................................................... USE FLAP 2 If Flaps = 3........................................................................................................................... USE FLAP 3 If Flaps > 3.....................................................................................................................USE FLAP FULL For Slats extension: SPD SEL...................................................................................................................... VFE NEXT - 5 KT L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN When in landing CONF and in final approach: DECELERATE TO CALCULATED VAPP Ident.: ABN-29-SUM3-00010544.0003001 / 30 AUG 10 LANDING FLARE: Only one ELEV and 2 spoilers per wing. A/C slightly sluggish SPOILERS: Only 2 per wing REVERSERS: Only N°1 BRAKING: ALTERNATE NO NOSEWHEEL STEERING Ident.: ABN-29-SUM3-00010545.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION For circuit: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPD - 10 kt / 200 kt For diversion: If Flaps jammed at zero: SELECT CLEAN CONFIGURATION Normal operating speeds (MAX SPD= 200 kt) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES GO-AROUND If Flaps jammed above zero: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPD - 10 kt / 200 kt FUEL: Increased fuel consumption (Refer to QRH PER-B) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 29.03B 01 DEC 14 Continued from the previous page A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.03C 01 DEC 14 HYD G+Y SYS LO PR SUMMARY Applicable to: MSN 0466-0700 Ident.: ABN-29-SUM3-00010529.0001001 / 28 APR 14 CRUISE SPD BRK...................................................................................................................................DO NOT USE MAX SPD............................................................................................................................................. 330/.82 MANEUVER WITH CARE ALTN LAW : PROT LOST FUEL: Increased fuel consumption (Refer to QRH PER-B) For Landing Performance assessment, Refer to QRH PER-C. Ident.: ABN-29-SUM3-00010543.0001001 / 08 FEB 13 APPROACH CAT 2 INOP SLATS SLOW / FLAPS JAMMED GPWS FLAP MODE (IF Flaps < 3)..........................................................................................................OFF For landing: If Flaps < 3........................................................................................................................... USE FLAP 2 If Flaps = 3........................................................................................................................... USE FLAP 3 If Flaps > 3.....................................................................................................................USE FLAP FULL For Slats extension: SPD SEL...................................................................................................................... VFE NEXT - 5 KT L/G gravity extension: MAX SPD.......................................................................................................................................200 KT L/G GRVTY EXTN......................................................................................................................... DOWN When L/G down: L/G LEVER..................................................................................................................................... DOWN When in landing CONF and in final approach: DECELERATE TO CALCULATED VAPP Ident.: ABN-29-SUM3-00010544.0002001 / 30 AUG 10 LANDING FLARE: Only one ELEV and 2 spoilers per wing. A/C slightly sluggish SPOILERS: Only 2 per wing REVERSERS: All avail. BRAKING: ALTERNATE NO NOSEWHEEL STEERING Ident.: ABN-29-SUM3-00010545.0001001 / 28 APR 14 GO-AROUND NO GEAR RETRACTION For circuit: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPD - 10 kt / 200 kt For diversion: If Flaps jammed at zero: SELECT CLEAN CONFIGURATION Normal operating speeds (MAX SPD= 200 kt) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES GO-AROUND If Flaps jammed above zero: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPD - 10 kt / 200 kt FUEL: Increased fuel consumption (Refer to QRH PER-B) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 29.03D 01 DEC 14 Continued from the previous page ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 30.01A 01 DEC 14 DOUBLE AOA HEAT FAILURE Ident.: ABN-30-00010548.0002001 / 08 FEB 13 Applicable to: ALL If icing conditions cannot be avoided: One of affected ADRs...................................................................................... OFF NAV ADR DISAGREE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 31.01A 01 DEC 14 DISPLAY UNIT FAILURE Ident.: ABN-31-00010550.0001001 / 08 FEB 13 Applicable to: MSN 0232-0472 Affected DU is blank or display is distorted: DU (affected)...........................................................................................AS RQRD ECAM/ND SEL (if ECAM DUs affected).......................................................... USE PFD/ND XFR (if EFIS DUs affected)............................................................... USE Diagonal line on the affected DU: DMC SWITCHING (EFIS OR ECAM).....................................................AS RQRD If unsuccessful: DU (affected)............................................................................. OFF THEN ON Note: ND display may disappear, in case too many waypoints and associated information are displayed. Reduce the range, or deselect WPT or CSTR, and the display will automatically recover after about 30 s. Diagonal line on both ECAM DUs: ECAM DMC SWITCHING..................................................................................... 2 Inversion of EWD and SD displays: ECAM UPPER DISPLAY................................................................OFF THEN ON DISPLAY UNIT FAILURE Ident.: ABN-31-00010550.0002001 / 08 FEB 13 Applicable to: MSN 0700-1118 DU is blank (with or without a large letter "F" in amber), or the display is distorted: DU (affected)...........................................................................................AS RQRD The DU can be switched off. ECAM/ND SEL (if ECAM DUs affected).......................................................... USE Transfer SD to F/O or CAPT ND. PFD/ND XFR (if EFIS DUs affected)............................................................... USE INVALID DISPLAY UNIT message is displayed: This may be caused by a DU failure. FOR AUTOMATIC DU RECOVERY................................WAIT MORE THAN 40 s If DU is automatically recovered: No crew action is required. If DU is not recovered: Non-recovered DU ............................................................................AS RQRD The DU can be switched off. INVALID DATA message is displayed (not on all DUs): The failure may be due to a DMC FAULT, or a communication interruption between the DMC and DU. DMC SWITCHING (EFIS OR ECAM).....................................................AS RQRD TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 31.01B 01 DEC 14 DISPLAY UNIT FAILURE (Cont'd) If unsuccessful: DU (affected)............................................................................. OFF THEN ON Note: ND display may disappear, in case too many waypoints and associated information are displayed. Reduce the range, or deselect WPT or CSTR, and the display will automatically recover after about 30 s. INVALID DATA message is displayed on all DUs: The autopilot, autothrust and MCDU navigation data are still available and may be used. FOR AUTOMATIC DUs RECOVERY.............................. WAIT MORE THAN 40 s If all DUs are automatically recovered: No crew action is required. If one or more DUs are not recovered: Non-recovered DUs....................................................................OFF FOR 40 s Non-recovered DUs....................................................... BACK ON sequentially If the initial failure re-occurs (INVALID DATA message appears on all DUs) when switching a given DU back ON: Apply the entire procedure again from the beginning. Leave this specific DU permanently OFF. INVALID DATA message is displayed on the ECAM DUs (EWD and SD): ECAM DMC SWITCHING..................................................................................... 2 This action enables the recovery of both ECAM DUs. Inversion of EWD and SD: ECAM UPPER DISPLAY................................................................OFF THEN ON The action on the ECAM DMC SWITCHING selector produces the same effect. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK ECAM SINGLE DISPLAY Ident.: ABN-31-00010551.0001001 / 08 FEB 13 Applicable to: ALL Only the EWD is available. No SD on the other DUs. To call a SYS page: PRESS AND MAINTAIN the SYS page key on the ECP Overflow on the STATUS page: PRESS AND MAINTAIN the STS key on the ECP The first page of the STATUS is displayed. RELEASE IT, THEN PRESS IT AGAIN WITHIN 2 SECONDS The second page of the STATUS is displayed. CONTINUE UNTIL THE OVERFLOW ARROW DISAPPEARS When the STS key is released for more than 2 s, the EWD is displayed again. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 31.02A 01 DEC 14 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 31.03A 01 DEC 14 EIS DISPLAY DISCREPANCY Ident.: ABN-31-00010552.0001001 / 27 JAN 12 Applicable to: ALL CHECK EWD CHECK SD CHECK PFD CHECK ND The DMC detects a discrepancy between acquisition and display on a DU. This caution is associated with an amber message displayed on the affected DU. In case of EWD display discrepancy, the amber message is displayed on the EWD and on both NDs. DMC/DU SWTG........................................................................................... AS RQRD Note: The failure may be due to a DMC or DU problem. The following part of the procedure is not displayed on ECAM: In case of CHECK EWD or CHECK SD: ECAM SWTG DMC....................................................................................... 1 or 2 DMC 1 or 2 may be selected if not failed. If unsuccessful: Return to normal DMC configuration. In case of CHECK EWD: ECAM UPPER DISPLAY....................................................................... OFF EWD is automatically transferred on SDU. ECAM/ND.................................................................................CAPT or F/O SD may be recovered on CAPT or on F/O NDU. In case of CHECK SD: ECAM/ND......................................................................................AS RQRD ECAM LOWER DISPLAY............................................................. AS RQRD The DU can be switched off. In case of CHECK PFD or CHECK ND: Crosscheck with standby instruments. EFIS DMC (affected side)..................................................................................... 3 If unsuccessful: Return to normal DMC configuration. PFD/ND XFR (affected side)............................................................. AS RQRD DU (affected)......................................................................................AS RQRD The DU can be switched off. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 32.01A 01 DEC 14 LOSS OF BRAKING Ident.: ABN-32-00010553.0001001 / 08 FEB 13 Applicable to: ALL If no braking available: REV.................................................................................................................. MAX BRAKE PEDALS..................................................................................... RELEASE A/SKID & N/W STRG.......................................................................................OFF BRAKE PEDALS......................................................................................... PRESS MAX BRK PR........................................................................................... 1000 PSI If still no braking: PARKING BRAKE...........................SHORT AND SUCCESSIVE APPLICATIONS TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 32.02A 01 DEC 14 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 32.03A 01 DEC 14 L/G GRAVITY EXTENSION Ident.: ABN-32-00010555.0001001 / 07 MAR 13 Applicable to: ALL CAUTION Do not apply this procedure if at least one green triangle is displayed on each landing gear on the WHEEL SD page. This is sufficient to confirm that the landing gear is downlocked. Disregard any possible GPWS "TOO LOW GEAR" aural alert. MAX SPEED..................................................................................................... 200 KT L/G GRVTY EXTN.............................................................................................DOWN CAUTION Both selector guards have to be open before selecting DOWN. When L/G DOWNLOCKED L/G lever.......................................................................................................DOWN GEAR DOWN indications............................................................................CHECK CAUTION N/W STRG is lost. Main and nose gear doors remain open. If successful: Do not reset the freefall system. This avoids undesirable effects, such as further fluid loss in the event of a leak or possible L/G unlocking in the event of a gear selector valve jammed in UP position. Note: Following the use of the freefall system for training purposes in flight, the system can be reset in flight. Provided that the green hydraulic system is available, a reset of the freefall system enables closure of the landing gear doors and operation of the nosewheel steering. If unsuccessful: LDG WITH ABNORMAL L/G Procedure......................................................APPLY Note: 1. One gravity extension reset is allowed in case of L/G GEAR NOT DOWNLOCKED alert display. 2. On the ground the freefall system must not be reset by the flight crew. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 32.04A 01 DEC 14 LANDING WITH ABNORMAL L/G Ident.: ABN-32-00010556.0007001 / 08 FEB 13 Applicable to: ALL CAUTION Do not apply this procedure if at least one green triangle is displayed on each landing gear on the WHEEL SD page. This is sufficient to confirm that the landing gear is downlocked. Disregard any possible GPWS "TOO LOW GEAR" aural alert. PREPARATION CABIN CREW ............................................................................................. NOTIFY ATC............................................................................................................... NOTIFY JETTISON............................................................................................... CONSIDER If NOSE L/G abnormal: CG location (if possible)................................................................................ AFT 10 PAX from front to rear moves the CG roughly 2 % aft. If one MAIN L/G abnormal: FUEL IMBALANCE............................................................................CONSIDER Open all fuel crossfeed valves and switch off the pumps on the side with landing gear normally extended. OXYGEN CREW SUPPLY................................................................................. OFF SIGNS...................................................................................................................ON CABIN and COCKPIT...............................................................................PREPARE ‐ Loose equipment secured ‐ Survival equipment prepared ‐ Belts and shoulder harnesses locked. APPROACH GPWS SYS.........................................................................................................OFF L/G LEVER ......................................................................................CHECK DOWN L/G GRVTY EXTN.........................................................................................RESET AUTOBRAKE......................................................................................DO NOT ARM EMER EXIT LT.....................................................................................................ON COMMERCIAL....................................................................................................OFF CABIN REPORT...........................................................................................OBTAIN JETTISON...........................................................................................................OFF T TANK FEED................................................................................................... ISOL A/SKID & N/W STRG ........................................................................................OFF MAX BRAKE PR....................................................................................... 1 000 PSI If one or both MAIN L/G abnormal: GROUND SPOILERS................................................................... DO NOT ARM BEFORE LANDING RAM AIR ............................................................................................................. ON BRACE FOR IMPACT.................................................................................. ORDER FLARE, TOUCH DOWN AND ROLL OUT Engines should be shut down sufficiently early to ensure fuel is shut off before the nacelles impact, but sufficiently late to ensure adequate hydraulic supplies for the flight controls. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 32.04B 01 DEC 14 LANDING WITH ABNORMAL L/G (Cont'd) Engine pumps continue to supply adequate hydraulic pressure for 30 s after engine shutdown. REVERSE........................................................................................... DO NOT USE If NOSE L/G abnormal: NOSE............................................................................................ MAINTAIN UP After touchdown, keep the nose off the runway by using the elevator. Then, lower the nose onto the runway before elevator control is lost. BRAKES (compatible with elevator efficiency)......................................... APPLY ENG MASTERS............................................................................................ OFF Shut down the engines before nose impact. If one MAIN L/G abnormal: ENG MASTERS (in sequence)..................................................................... OFF After main gear touchdown, shut down the engine on the failure side first, then the other engine before nacelle touchdown. FAILURE SIDE WING...................................................................MAINTAIN UP Use roll control, as necessary, to keep the unsupported wing up as long as possible. DIRECTIONAL CONTROL..................................................................MAINTAIN Use rudder and brakes (maximum 1 000 PSI ) to maintain the runway axis as long as possible. If both MAIN L/G abnormal: ENG MASTERS............................................................................................ OFF Shut down the engines in the flare, before touchdown. PITCH ATTITUDE (at touchdown)...................................... NOT LESS THAN 6° WHEN A/C STOPPED ENG (all) and APU FIRE pushbutton.............................................................. PUSH Pressing the ENG FIRE pb shuts off the related hydraulic pressure within a short time. ENG (all) and APU AGENT........................................................................... DISCH If Evacuation required: EVACUATION........................................................................................ INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs...................................................................................................... OFF If Evacuation not required: CABIN CREW and PASSENGERS (PA)................................................ NOTIFY Ensure that all the landing gears are secured before initiating the disembarkation (before switching OFF the seat belts signs). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK ABNORMAL V ALPHA PROT Ident.: ABN-34-00015281.0001001 / 08 DEC 14 Applicable to: ALL Refer to OEB-49 Abnormal V Alpha Prot TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 34.01A 01 DEC 14 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02A 01 DEC 14 ADR CHECK PROC Ident.: ABN-34-00015215.0001001 / 01 DEC 14 Applicable to: ALL For the ADR CHECK procedure, apply the UNRELIABLE SPEED INDICATION procedure. Refer to QRH ABN-34.02A-UNRELIABLE SPEED INDICATION. Applicable to: MSN 0232-0361 UNRELIABLE SPEED INDICATION Ident.: ABN-34-A-00010566.0004001 / 13 MAY 14 If the safe conduct of the flight is impacted: MEMORY ITEMS AP/FD.............................................................................................................. OFF A/THR.............................................................................................................. OFF PITCH/THRUST: Below THRUST RED ALT...................................................................15° / TOGA Above THRUST RED ALT and Below FL 100....................................... 10° / CLB Above THRUST RED ALT and Above FL 100......................................... 5° / CLB FLAPS (if CONF 0(1)(2)(3)).....................................MAINTAIN CURRENT CONF FLAPS (if CONF FULL)...................................SELECT CONF 3 AND MAINTAIN SPEEDBRAKES..................................................................CHECK RETRACTED L/G..................................................................................................................... UP When at, or above MSA or Circuit Altitude: Level off for troubleshooting. GPS ALTITUDE..........................................................................Display on MCDU Ident.: ABN-34-A-00012101.0018001 / 13 MAY 14 To level off for troubleshooting: AP/FD............................................................................................................... OFF A/THR............................................................................................................... OFF Note: Check the actual slat/flap configuration on ECAM, since flap auto-retraction may occur. PITCH / THRUST FOR INITIAL LEVEL OFF SLATS / FLAPS EXTENDED Above 190 t 190 t - 160 t Below 160 t CONF Speed 3 F 8.0 / 69.9 8.0 / 66.4 8.5 / 62.9 2 F 9.5 / 66.0 9.5 / 61.0 9.0 / 55.0 1+F S 6.5 / 64.3 6.5 / 59.1 6.5 / 53.8 1 S 9.0 / 63.2 9.0 / 58.1 9.0 / 52.8 Pitch (°) / Thrust (% N1) CLEAN FL Speed Pitch (°) / Thrust (% N1) Below FL 250 240 kt 5.0 / 66.1 3.5 / 61.4 2.5 / 59.1 FL 250 - FL 370 260 kt 3.5 / 78.9 2.5 / 75.2 2.0 / 72.1 Above FL 370 M 0.80 3.0 / 84.2 2.5 / 81.6 2.0 / 78.7 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.02B 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) FLYING TECHNIQUE TO STABILIZE SPEED Adjust pitch in order to fly the required flight path. When target pitch is reached, flying intended flight path, adjust thrust to target: If the aircraft pitch tends to increase, aircraft is slow, then increase thrust; If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust. Ident.: ABN-34-A-00012102.0004001 / 13 MAY 14 WHEN FLIGHT PATH IS STABILIZED PROBE/WINDOW HEAT......................................................................................ON TECHNICAL RECOMMENDATIONS Respect Stall Warning and disregard “RISK OF UNDUE STALL WARNING” STATUS message if displayed on ECAM. To monitor speed, refer to IRS Ground Speed variations, or GPS Ground Speed variations. If remaining altitude indication is unreliable: Do not use FPV and/or V/S, which are affected. ATC altitude is affected. Notify the ATC. Refer to GPS altitude : altitude variations may be used to control level flight, and is an altitude cue. Refer to Radio Altimeter. CAUTION If the failure is due to radome destruction, the drag will increase and therefore N1 must be increased by 3 % (CRZ) or 1.5 % (APP). Fuel flow will increase by about 13 %. AFFECTED ADR IDENTIFICATION Crosscheck all speed indications and Refer to QRH PER-A-Operating Speeds table (for F, S speeds) or Refer to QRH OPS-Severe Turbulence table (for speed in clean conf). If at least one ADR is reliable: Faulty ADR(s).............................................................................................OFF REMAINING AIR DATA....................................................................CONFIRM Alternates sources may be used to evaluate the air data: ‐ GPS altitude. ‐ GPS and IRS Ground Speeds, taking into account altitude and wind effect. If affected ADR(s) cannot be identified or all ADRs are affected: ONE ADR..........................................................................................KEEP ON Keep one ADR ON to maintain the STALL WARNING protection. TWO ADR(s).............................................................................................. OFF This prevents the flight control laws from using two coherent but unreliable ADR data. EFIS DMC switching.........................................................................AS RQRD LDG CONF................................................................................... USE FLAP 3 APP SPD........................................................................................... VLS + 10 LDG DIST PROC...................................................................................APPLY TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02C 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) To return to departure airport: Keep takeoff configuration preferably. Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Approaches (Pitch & Thrust Tables). To accelerate and clean up after takeoff: Accelerate and clean up the aircraft in level flight: THRUST................................................................................................ CLB FLAPS......................................................................................... RETRACT Retract from 3 or 2 to 1, once CLB thrust is set. Retract from 1 to 0, when the aircraft pitch is lower than the pitch for S speed (Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION Level-Off (Pitch & Thrust Table)). Once in clean configuration, Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Climb / Cruise / Descent (Pitch & Thrust Tables), Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Approaches (Pitch & Thrust Tables) for flight continuation. Other cases: Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Climb / Cruise / Descent (Pitch & Thrust Tables), Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Approaches (Pitch & Thrust Tables) for flight continuation. Ident.: ABN-34-A-00012104.0024001 / 13 MAY 14 CLIMB Set the thrust to CL. CLEAN FL Speed Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) Below FL 100 10.0 / CLB 11.0 / CLB 12.0 / CLB FL 100 - FL 150 9.0 / CLB 9.0 / CLB 10.0 / CLB 8.0 / CLB 8.0 / CLB 8.5 / CLB FL 200 - FL 250 7.0 / CLB 7.0 / CLB 7.0 / CLB FL 250 - FL 300 5.0 / CLB 5.0 / CLB 5.0 / CLB 4.0 / CLB 4.0 / CLB 3.5 / CLB 3.5 / CLB 3.5 / CLB 3.5 / CLB FL 150 - FL 200 FL 300 - FL 370 Above FL 370 240 kt 260 kt M 0.80 CRUISE Adjust N1 to maintain approximate level flight with pitch attitude held constant. When time permits, Refer to QRH Operational Data (OPS Severe Turbulence) adjust pitch to maintain level flight. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02D 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) CLEAN FL Speed Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) Below FL 250 240 kt 5.0 / 66.1 3.5 / 61.4 2.5 / 59.1 FL 250 - FL 370 260 kt 3.5 / 78.9 2.5 / 75.2 2.0 / 72.1 Above FL 370 M 0.80 3.0 / 84.2 2.5 / 81.6 2.0 / 78.7 190 t - 160 t Below 160 t DESCENT Set the thrust to IDLE. CLEAN FL Speed Above 190 t Pitch (°) / Thrust (% N1) Above FL 370 M 0.80 1.0 / IDLE 0.0 / IDLE -0.5 / IDLE FL 370 - FL 250 260 kt 1.5 / IDLE 0.5 / IDLE -1.0 / IDLE FL 250 - FL 100 240 kt 2.0 / IDLE 0.5 / IDLE -0.5 / IDLE Below FL 100 240 kt 2.0 / IDLE 1.0 / IDLE -0.5 / IDLE Below FL 100 G-DOT 3.0 / IDLE 3.0 / IDLE 3.0 / IDLE Ident.: ABN-34-A-00012105.0024001 / 13 MAY 14 INITIAL AND INTERMEDIATE APPROACH IN LEVEL FLIGHT The approach phase between Green Dot speed (clean configuration) and the landing configuration (CONF 3), is flown in level flight. LANDING GEAR UP IN LEVEL FLIGHT Above 190 t 190 t - 160 t Below 160 t CONF Speed (kts) 0 G-DOT 5.0 / 59.3 5.5 / 54.0 5.0 / 49.1 1 S 9.0 / 63.2 9.0 / 58.1 9.0 / 52.8 1 + F (1) S 6.5 / 64.3 6.5 / 59.1 6.5 / 53.8 2 F 6.0 / 65.1 6.0 / 60.1 6.0 / 54.4 Pitch (°) / Thrust (% N1) LANDING GEAR DOWN IN LEVEL FLIGHT (EXPECT GRVTY EXTENSION) 3 F 6.5 / 70.7 6.5 / 65.5 6.5 / 60.1 (1) Due to the fact that the speed is unreliable, the SFCC may select the 1 + F configuration in approach, instead of 1. FINAL APPROACH AT STANDARD - 3 ° DESCENT FLIGHT PATH LANDING GEAR DOWN CONF Speed (kts) 3 VLS + 10 Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) 4.5 / 52.2 FLYING TECHNIQUE TO STABILIZE SPEED: Adjust pitch in order to fly the required flight path. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 4.5 / 47.7 4.0 / 43.0 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02E 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) When target pitch is reached, flying intended flight path, adjust thrust to target. If the aircraft pitch tends to increase, aircraft is slow, then increase thrust; If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust. Applicable to: MSN 0466-0472 UNRELIABLE SPEED INDICATION Ident.: ABN-34-A-00010566.0004001 / 13 MAY 14 If the safe conduct of the flight is impacted: MEMORY ITEMS AP/FD.............................................................................................................. OFF A/THR.............................................................................................................. OFF PITCH/THRUST: Below THRUST RED ALT...................................................................15° / TOGA Above THRUST RED ALT and Below FL 100....................................... 10° / CLB Above THRUST RED ALT and Above FL 100......................................... 5° / CLB FLAPS (if CONF 0(1)(2)(3)).....................................MAINTAIN CURRENT CONF FLAPS (if CONF FULL)...................................SELECT CONF 3 AND MAINTAIN SPEEDBRAKES..................................................................CHECK RETRACTED L/G..................................................................................................................... UP When at, or above MSA or Circuit Altitude: Level off for troubleshooting. GPS ALTITUDE..........................................................................Display on MCDU Ident.: ABN-34-A-00012101.0016001 / 13 MAY 14 To level off for troubleshooting: AP/FD............................................................................................................... OFF A/THR............................................................................................................... OFF Note: Check the actual slat/flap configuration on ECAM, since flap auto-retraction may occur. PITCH / THRUST FOR INITIAL LEVEL OFF SLATS / FLAPS EXTENDED Above 190 t 190 t - 160 t Below 160 t CONF Speed 3 F 7.5 / 76.6 7.5 / 70.7 7.0 / 64.3 Pitch (°) / Thrust (% N1) 2 F 9.0 / 75.0 9.0 / 69.2 8.5 / 62.4 1+F S 6.0 / 72.7 6.0 / 66.9 6.0 / 60.5 1 S 9.0 / 71.6 9.0 / 65.7 9.0 / 59.5 FL Speed Below FL 250 240 kt 5.0 / 75.7 4.0 / 72.6 2.5 / 68.1 FL 250 - FL 370 260 kt 3.5 / 90.0 3.0 / 87.9 2.0 / 83.9 Above FL 370 M 0.80 3.0 / 94.3 2.5 / 93.4 2.0 / 90.0 CLEAN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE Pitch (°) / Thrust (% N1) A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.02F 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) FLYING TECHNIQUE TO STABILIZE SPEED Adjust pitch in order to fly the required flight path. When target pitch is reached, flying intended flight path, adjust thrust to target: If the aircraft pitch tends to increase, aircraft is slow, then increase thrust; If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust. Ident.: ABN-34-A-00012102.0004001 / 13 MAY 14 WHEN FLIGHT PATH IS STABILIZED PROBE/WINDOW HEAT......................................................................................ON TECHNICAL RECOMMENDATIONS Respect Stall Warning and disregard “RISK OF UNDUE STALL WARNING” STATUS message if displayed on ECAM. To monitor speed, refer to IRS Ground Speed variations, or GPS Ground Speed variations. If remaining altitude indication is unreliable: Do not use FPV and/or V/S, which are affected. ATC altitude is affected. Notify the ATC. Refer to GPS altitude : altitude variations may be used to control level flight, and is an altitude cue. Refer to Radio Altimeter. CAUTION If the failure is due to radome destruction, the drag will increase and therefore N1 must be increased by 3 % (CRZ) or 1.5 % (APP). Fuel flow will increase by about 13 %. AFFECTED ADR IDENTIFICATION Crosscheck all speed indications and Refer to QRH PER-A-Operating Speeds table (for F, S speeds) or Refer to QRH OPS-Severe Turbulence table (for speed in clean conf). If at least one ADR is reliable: Faulty ADR(s).............................................................................................OFF REMAINING AIR DATA....................................................................CONFIRM Alternates sources may be used to evaluate the air data: ‐ GPS altitude. ‐ GPS and IRS Ground Speeds, taking into account altitude and wind effect. If affected ADR(s) cannot be identified or all ADRs are affected: ONE ADR..........................................................................................KEEP ON Keep one ADR ON to maintain the STALL WARNING protection. TWO ADR(s).............................................................................................. OFF This prevents the flight control laws from using two coherent but unreliable ADR data. EFIS DMC switching.........................................................................AS RQRD LDG CONF................................................................................... USE FLAP 3 APP SPD........................................................................................... VLS + 10 LDG DIST PROC...................................................................................APPLY TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02G 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) To return to departure airport: Keep takeoff configuration preferably. Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Approaches (Pitch & Thrust Tables). To accelerate and clean up after takeoff: Accelerate and clean up the aircraft in level flight: THRUST................................................................................................ CLB FLAPS......................................................................................... RETRACT Retract from 3 or 2 to 1, once CLB thrust is set. Retract from 1 to 0, when the aircraft pitch is lower than the pitch for S speed (Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION Level-Off (Pitch & Thrust Table)). Once in clean configuration, Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Climb / Cruise / Descent (Pitch & Thrust Tables), Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Approaches (Pitch & Thrust Tables) for flight continuation. Other cases: Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Climb / Cruise / Descent (Pitch & Thrust Tables), Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Approaches (Pitch & Thrust Tables) for flight continuation. Ident.: ABN-34-A-00012104.0017001 / 13 MAY 14 CLIMB Set the thrust to CL. CLEAN FL Speed Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) Below FL 100 10.5 / CLB 11.0 / CLB 12.5 / CLB FL 100 - FL 150 9.0 / CLB 9.5 / CLB 10.5 / CLB 8.5 / CLB 8.5 / CLB 10.5 / CLB FL 200 - FL 250 7.5 / CLB 7.5 / CLB 7.5 / CLB FL 250 - FL 300 5.5 / CLB 5.0 / CLB 5.5 / CLB 4.5 / CLB 4.0 / CLB 4.0 / CLB 3.5 / CLB 3.5 / CLB 3.5 / CLB FL 150 - FL 200 FL 300 - FL 370 Above FL 370 240 kt 260 kt M 0.80 CRUISE Adjust N1 to maintain approximate level flight with pitch attitude held constant. When time permits, Refer to QRH Operational Data (OPS Severe Turbulence) adjust pitch to maintain level flight. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02H 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) CLEAN FL Speed Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) Below FL 250 240 kt 5.0 / 75.7 4.0 / 72.6 2.5 / 68.1 FL 250 - FL 370 260 kt 3.5 / 90.0 3.0 / 87.9 2.0 / 83.9 Above FL 370 M 0.80 3.0 / 94.3 2.5 / 93.4 2.0 / 90.0 190 t - 160 t Below 160 t DESCENT Set the thrust to IDLE. CLEAN FL Speed Above 190 t Pitch (°) / Thrust (% N1) Above FL 370 M 0.80 1.0 / IDLE 0.0 / IDLE -0.5 / IDLE FL 370 - FL 250 260 kt 1.5 / IDLE 0.5 / IDLE -1.0 / IDLE FL 250 - FL 100 240 kt 2.0 / IDLE 0.5 / IDLE -0.5 / IDLE Below FL 100 240 kt 2.5 / IDLE 0.5 / IDLE -0.5 / IDLE Below FL 100 G-DOT 2.5 / IDLE 2.5 / IDLE 2.5 / IDLE Ident.: ABN-34-A-00012105.0017001 / 13 MAY 14 INITIAL AND INTERMEDIATE APPROACH IN LEVEL FLIGHT The approach phase between Green Dot speed (clean configuration) and the landing configuration (CONF 3), is flown in level flight. LANDING GEAR UP IN LEVEL FLIGHT Above 190 t 190 t - 160 t Below 160 t CONF Speed (kts) 0 G-DOT 5.0 / 67.4 5.5 / 61.5 5.5 / 55.3 1 S 9.0 / 71.7 9.0 / 65.8 9.0 / 59.5 1 + F (1) S 6.0 / 72.7 6.0 / 66.9 6.0 / 60.5 2 F 6.0 / 75.0 6.0 / 69.2 6.0 / 64.0 Pitch (°) / Thrust (% N1) LANDING GEAR DOWN IN LEVEL FLIGHT (EXPECT GRVTY EXTENSION) 3 F 6.5 / 81.5 6.5 / 75.4 6.5 / 69.1 (1) Due to the fact that the speed is unreliable, the SFCC may select the 1 + F configuration in approach, instead of 1. FINAL APPROACH AT STANDARD - 3 ° DESCENT FLIGHT PATH LANDING GEAR DOWN CONF Speed (kts) 3 VLS + 10 Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) 4.5 / 59.0 FLYING TECHNIQUE TO STABILIZE SPEED: Adjust pitch in order to fly the required flight path. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 4.0 / 53.2 4.0 / 48.2 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02I 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) When target pitch is reached, flying intended flight path, adjust thrust to target. If the aircraft pitch tends to increase, aircraft is slow, then increase thrust; If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust. Applicable to: MSN 0700 UNRELIABLE SPEED INDICATION Ident.: ABN-34-A-00010566.0004001 / 13 MAY 14 If the safe conduct of the flight is impacted: MEMORY ITEMS AP/FD.............................................................................................................. OFF A/THR.............................................................................................................. OFF PITCH/THRUST: Below THRUST RED ALT...................................................................15° / TOGA Above THRUST RED ALT and Below FL 100....................................... 10° / CLB Above THRUST RED ALT and Above FL 100......................................... 5° / CLB FLAPS (if CONF 0(1)(2)(3)).....................................MAINTAIN CURRENT CONF FLAPS (if CONF FULL)...................................SELECT CONF 3 AND MAINTAIN SPEEDBRAKES..................................................................CHECK RETRACTED L/G..................................................................................................................... UP When at, or above MSA or Circuit Altitude: Level off for troubleshooting. GPS ALTITUDE..........................................................................Display on MCDU Ident.: ABN-34-A-00012101.0016001 / 13 MAY 14 To level off for troubleshooting: AP/FD............................................................................................................... OFF A/THR............................................................................................................... OFF Note: Check the actual slat/flap configuration on ECAM, since flap auto-retraction may occur. PITCH / THRUST FOR INITIAL LEVEL OFF SLATS / FLAPS EXTENDED Above 190 t 190 t - 160 t Below 160 t CONF Speed 3 F 7.5 / 76.6 7.5 / 70.7 7.0 / 64.3 Pitch (°) / Thrust (% N1) 2 F 9.0 / 75.0 9.0 / 69.2 8.5 / 62.4 1+F S 6.0 / 72.7 6.0 / 66.9 6.0 / 60.5 1 S 9.0 / 71.6 9.0 / 65.7 9.0 / 59.5 FL Speed Below FL 250 240 kt 5.0 / 75.7 4.0 / 72.6 2.5 / 68.1 FL 250 - FL 370 260 kt 3.5 / 90.0 3.0 / 87.9 2.0 / 83.9 Above FL 370 M 0.80 3.0 / 94.3 2.5 / 93.4 2.0 / 90.0 CLEAN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE Pitch (°) / Thrust (% N1) A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.02J 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) FLYING TECHNIQUE TO STABILIZE SPEED Adjust pitch in order to fly the required flight path. When target pitch is reached, flying intended flight path, adjust thrust to target: If the aircraft pitch tends to increase, aircraft is slow, then increase thrust; If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust. Ident.: ABN-34-A-00012102.0009001 / 13 MAY 14 WHEN FLIGHT PATH IS STABILIZED PROBE/WINDOW HEAT......................................................................................ON TECHNICAL RECOMMENDATIONS Respect Stall Warning and disregard “RISK OF UNDUE STALL WARNING” STATUS message if displayed on ECAM. To monitor speed, refer to IRS Ground Speed variations, or GPS Ground Speed variations. If remaining altitude indication is unreliable: Do not use FPV and/or V/S, which are affected. ATC altitude is affected. Notify the ATC. Refer to GPS altitude : altitude variations may be used to control level flight, and is an altitude cue. Refer to Radio Altimeter. CAUTION If the failure is due to radome destruction, the drag will increase and therefore N1 must be increased by 3 % (CRZ) or 1.5 % (APP). Fuel flow will increase by about 13 %. AFFECTED ADR IDENTIFICATION Crosscheck all speed indications and Refer to QRH PER-A-Operating Speeds table (for F, S speeds) or Refer to QRH OPS-Severe Turbulence table (for speed in clean conf). If at least one ADR is reliable: Faulty ADR(s).............................................................................................OFF REMAINING AIR DATA....................................................................CONFIRM Alternates sources may be used to evaluate the air data: ‐ GPS altitude. ‐ GPS and IRS Ground Speeds, taking into account altitude and wind effect. If affected ADR(s) cannot be identified or all ADRs are affected: When above FL 250: ONE ADR ................................................................................... KEEP ON TWO ADRs........................................................................................... OFF This prevents the flight control laws from using two coherent but unreliable ADR data. For flight continuation, Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Climb / Cruise / Descent (Pitch & Thrust Tables). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02K 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) When below FL 250, if speed still unreliable: ALL ADRs P/B ..................................................................................... OFF All ADRs must be switched OFF to replace the PFD's normal speed scale and altitude indication to the Back Up Speed Scale and GPS altitude indication. SPD................................................................................. FLY THE GREEN NAV ADR 1+2+3 FAULT Ident.: ABN-34-A-00012104.0055001 / 13 MAY 14 CLIMB Set the thrust to CL. CLEAN FL Speed FL 250 - FL 300 260 kt FL 300 - FL 370 Above FL 370 M 0.80 Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) 5.5 / CLB 5.0 / CLB 5.5 / CLB 4.5 / CLB 4.0 / CLB 4.0 / CLB 3.5 / CLB 3.5 / CLB 3.5 / CLB CRUISE Adjust N1 to maintain approximate level flight with pitch attitude held constant. When time permits, Refer to QRH Operational Data (OPS Severe Turbulence) adjust pitch to maintain level flight. CLEAN FL Speed Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) FL 250 - FL 370 260 kt 3.5 / 90.0 3.0 / 87.9 2.0 / 83.9 Above FL 370 M 0.80 3.0 / 94.3 2.5 / 93.4 2.0 / 90.0 190 t - 160 t Below 160 t DESCENT Set the thrust to IDLE CLEAN Above 190 t FL Speed Above FL 370 M 0.80 1.0 / IDLE 0.0 / IDLE -0.5 / IDLE FL 370 - FL 250 260 kt 1.5 / IDLE 0.5 / IDLE -1.0 / IDLE Applicable to: MSN 0968-1118 Pitch (°) / Thrust (% N1) UNRELIABLE SPEED INDICATION Ident.: ABN-34-A-00010566.0004001 / 13 MAY 14 If the safe conduct of the flight is impacted: MEMORY ITEMS AP/FD.............................................................................................................. OFF A/THR.............................................................................................................. OFF TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02L 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) PITCH/THRUST: Below THRUST RED ALT...................................................................15° / TOGA Above THRUST RED ALT and Below FL 100....................................... 10° / CLB Above THRUST RED ALT and Above FL 100......................................... 5° / CLB FLAPS (if CONF 0(1)(2)(3)).....................................MAINTAIN CURRENT CONF FLAPS (if CONF FULL)...................................SELECT CONF 3 AND MAINTAIN SPEEDBRAKES..................................................................CHECK RETRACTED L/G..................................................................................................................... UP When at, or above MSA or Circuit Altitude: Level off for troubleshooting. GPS ALTITUDE..........................................................................Display on MCDU Ident.: ABN-34-A-00012101.0018001 / 13 MAY 14 To level off for troubleshooting: AP/FD............................................................................................................... OFF A/THR............................................................................................................... OFF Note: Check the actual slat/flap configuration on ECAM, since flap auto-retraction may occur. PITCH / THRUST FOR INITIAL LEVEL OFF SLATS / FLAPS EXTENDED Above 190 t 190 t - 160 t Below 160 t CONF Speed 3 F 8.0 / 69.9 8.0 / 66.4 8.5 / 62.9 2 F 9.5 / 66.0 9.5 / 61.0 9.0 / 55.0 1+F S 6.5 / 64.3 6.5 / 59.1 6.5 / 53.8 1 S 9.0 / 63.2 9.0 / 58.1 9.0 / 52.8 Pitch (°) / Thrust (% N1) CLEAN FL Speed Pitch (°) / Thrust (% N1) Below FL 250 240 kt 5.0 / 66.1 3.5 / 61.4 2.5 / 59.1 FL 250 - FL 370 260 kt 3.5 / 78.9 2.5 / 75.2 2.0 / 72.1 Above FL 370 M 0.80 3.0 / 84.2 2.5 / 81.6 2.0 / 78.7 FLYING TECHNIQUE TO STABILIZE SPEED Adjust pitch in order to fly the required flight path. When target pitch is reached, flying intended flight path, adjust thrust to target: If the aircraft pitch tends to increase, aircraft is slow, then increase thrust; If the aircraft pitch tends to decrease, aircraft is fast, then decrease thrust. Ident.: ABN-34-A-00012102.0009001 / 13 MAY 14 WHEN FLIGHT PATH IS STABILIZED PROBE/WINDOW HEAT......................................................................................ON TECHNICAL RECOMMENDATIONS Respect Stall Warning and disregard “RISK OF UNDUE STALL WARNING” STATUS message if displayed on ECAM. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.02M 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) To monitor speed, refer to IRS Ground Speed variations, or GPS Ground Speed variations. If remaining altitude indication is unreliable: Do not use FPV and/or V/S, which are affected. ATC altitude is affected. Notify the ATC. Refer to GPS altitude : altitude variations may be used to control level flight, and is an altitude cue. Refer to Radio Altimeter. CAUTION If the failure is due to radome destruction, the drag will increase and therefore N1 must be increased by 3 % (CRZ) or 1.5 % (APP). Fuel flow will increase by about 13 %. AFFECTED ADR IDENTIFICATION Crosscheck all speed indications and Refer to QRH PER-A-Operating Speeds table (for F, S speeds) or Refer to QRH OPS-Severe Turbulence table (for speed in clean conf). If at least one ADR is reliable: Faulty ADR(s).............................................................................................OFF REMAINING AIR DATA....................................................................CONFIRM Alternates sources may be used to evaluate the air data: ‐ GPS altitude. ‐ GPS and IRS Ground Speeds, taking into account altitude and wind effect. If affected ADR(s) cannot be identified or all ADRs are affected: When above FL 250: ONE ADR ................................................................................... KEEP ON TWO ADRs........................................................................................... OFF This prevents the flight control laws from using two coherent but unreliable ADR data. For flight continuation, Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION - Climb / Cruise / Descent (Pitch & Thrust Tables). When below FL 250, if speed still unreliable: ALL ADRs P/B ..................................................................................... OFF All ADRs must be switched OFF to replace the PFD's normal speed scale and altitude indication to the Back Up Speed Scale and GPS altitude indication. SPD................................................................................. FLY THE GREEN NAV ADR 1+2+3 FAULT Ident.: ABN-34-A-00012104.0053001 / 01 DEC 14 CLIMB Set the thrust to CL. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.02N 01 DEC 14 UNRELIABLE SPEED INDICATION (Cont'd) CLEAN FL FL 250 - FL 300 FL 300 - FL 370 Above FL 370 Speed 260 kt M 0.80 Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) 5.0 / CLB 5.0 / CLB 5.0 / CLB 4.0 / CLB 4.0 / CLB 3.5 / CLB 3.5 / CLB 3.5 / CLB 3.5 / CLB CRUISE Adjust N1 to maintain approximate level flight with pitch attitude held constant. When time permits, Refer to QRH Operational Data (OPS Severe Turbulence) adjust pitch to maintain level flight. CLEAN FL Speed Above 190 t 190 t - 160 t Below 160 t Pitch (°) / Thrust (% N1) FL 250 - FL 370 260 kt 3.5 / 78.9 2.5 / 75.2 2.0 / 72.1 Above FL 370 M 0.80 3.0 / 84.2 2.5 / 81.6 2.0 / 78.7 190 t - 160 t Below 160 t DESCENT Set the thrust to IDLE CLEAN Above 190 t FL Speed Above FL 370 M 0.80 1.0 / IDLE 0.0 / IDLE -0.5 / IDLE FL 360 FL - FL 250 260 kt 1.5 / IDLE 0.5 / IDLE -1.0 / IDLE Pitch (°) / Thrust (% N1) TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK 34.03A ABNORMAL AND EMERGENCY PROCEDURES 01 DEC 14 ALL ADR OFF Applicable to: MSN 0700-1118 Ident.: ABN-34-B-00012366.0016001 / 26 MAY 14 SPD..................................................................................................FLY THE GREEN Fly within the green area of the speed scale to ensure safe flight. For slats/flaps retraction, it is better to fly at the top of the green area of the speed scale. CAUTION The altitude displayed on the PFD is a GPS altitude. FM SOURCE..................................................................................................... NORM BACK UP NAV...................................................................................................... USE When all ADRs are OFF, both FMs are lost. Revert to Back Up NAV via the NAV B/UP prompt on the MCDU MENU page. NAVAID TUNING......................................................................................... USE RMP Set both RMPs to NAV. MANUAL CABIN PRESSURE CONTROL MODE SEL........................................................................................................ MAN MAN V/S CTL........................................................................................... AS RQRD MAN CAB PR CTL TGT V/S : CLIMB 500 FT/MIN DESC 300 FT/MIN A/C GPS ALT CAB ALT TGT 410 350 300 250 <200 8 000 6 500 5 000 2 500 0 FOR APPROACH SPD...............................................................................................FLY THE GREEN Before extending the slats/flaps, it is better to fly at the bottom of the speed scale green area, and to be in straight flight. FOR LDG..............................................................................................USE FLAP 3 GPWS FLAP MODE...........................................................................................OFF LDG DIST PROC........................................................................................... APPLY APPR SPD.........................................................................................FLY THE BUG During the approach, the bug indicates Vapp. WHEN FLAP 2: LDG GRVTY EXTN...................................................................................DOWN CAUTION Nosewheel steering is lost. All gear doors remain open. WHEN L/G DOWNLOCKED: L/G lever....................................................................................................DOWN GEAR DOWN indications........................................................................ CHECK TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.03B 01 DEC 14 ALL ADR OFF (Cont'd) DURING FINAL APPROACH: MAN V/S CTL........................................................................................FULL UP CAUTION Check that the outflow valve is fully open, and that cabin altitude is at airfield elevation before opening the doors. Ident.: ABN-34-B-00012367.0002001 / 01 DEC 14 STATUS INOP SYS ADR 1+2+3 F/CTL PROT CAB PR 1+2 RUD TRV LIM AP 1+2 A/THR GPWS GPWS TERR REAC W/S DET PRED W/S DET ATC/XPDR 1 ATC/XPDR 2 TCAS Other INOP SYS RAT automatic extension NWS FLAP AUTO RETRACT FLAP LOAD RELIEF ALPHA LOCK L/G RETRACT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.04A 01 DEC 14 ADR 1 + 2 + 3 FAULT Applicable to: MSN 0232, 0361 Ident.: ABN-34-C-00012472.0003001 / 11 FEB 13 This procedure is not displayed on the ECAM. Only dual ADR warnings are displayed, in case of a triple ADR failure. ADR P/B (all)......................................................................................................... OFF STBY INST............................................................................................................ USE FM SOURCE..................................................................................................... NORM BACK UP NAV...................................................................................................... USE When all ADRs are OFF, both FMs are lost. Revert to Back Up NAV via the NAV B/UP prompt on the MCDU MENU page. NAVAID TUNING......................................................................................... USE RMP Set both RMPs to NAV. Note: Disregard ECAM actions for AIR DATA SWTG and ATC, since they have no effect in case of a total loss of ADRs. F/CTL ALTN LAW (PROT LOST) Note: The STALL WARNING is lost. MAX SPEED................................................................................................... 330/0.82 See the following table for the IAS/MN relationship for 0.82. FL 410 390 370 350 330 310 290 270 and below MAX SPD 243 252 265 278 290 305 317 330 Note: Use manual control for cabin pressurization. MODE SEL..............................................................................................MAN MAN V/S CTL.................................................................................AS RQRD Ident.: ABN-34-C-00012474.0007001 / 08 FEB 13 STATUS MAX SPEED................................................ 330/0.82 RUD WITH CARE ABV 160 KT See (1) APPR PROC FOR LDG......................................... USE FLAP 3 APPR SPD....................................VREF + 15 KT Note: VLS is not displayed on the PFD. LDG DIST PROC...................................... APPLY FOR L/G GRVTY EXTN: MAX SPEED........................................200 KT LDG GRVTY EXTN..............................DOWN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE INOP SYS F/CTL PROT A/THR ADR 1+2+3 AP 1+2 WINDSHEAR DET L/G RETRACT RUD TRV LIM GPWS CAB PR 1+2 Other INOP SYS FLAPS AUTO RETRACT ALPHA LOCK ATC ALTI MODE FLAPS LOAD RELIEF TCAS ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.04B 01 DEC 14 ADR 1 + 2 + 3 FAULT (Cont'd) WHEN L/G DOWNLOCKED: L/G........................................................DOWN DURING FINAL APPR MAN V/S CTL...................................FULL UP ALTN LAW: PROT LOST BOTH PFDs ON SAME FMGC Note: Check speed is below VFE of CONF 1+F (215 kt) before selecting Flaps 1; since ADR parameters are lost, the SFCCs will set CONF 1+F instead of CONF 1. CAUTION Check that the outflow valve is fully open, and the cabin altitude is at airfield elevation before opening the doors. (1) At slats’ extension, full rudder travel authority is recovered. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK Applicable to: MSN 0238-0259, 0466-0472 34.04C 01 DEC 14 ADR 1 + 2 + 3 FAULT Ident.: ABN-34-C-00012472.0048001 / 11 FEB 13 This procedure is not displayed on the ECAM. Only dual ADR warnings are displayed, in case of a triple ADR failure. ADR P/B (all)......................................................................................................... OFF STBY INST............................................................................................................ USE FM SOURCE..................................................................................................... NORM BACK UP NAV...................................................................................................... USE When all ADRs are OFF, both FMs are lost. Revert to Back Up NAV via the NAV B/UP prompt on the MCDU MENU page. NAVAID TUNING......................................................................................... USE RMP Set both RMPs to NAV. Note: Disregard ECAM actions for AIR DATA SWTG and ATC, since they have no effect in case of a total loss of ADRs. F/CTL ALTN LAW (PROT LOST) MAX SPEED................................................................................................... 330/0.82 See the following table for the IAS/MN relationship for 0.82. FL 410 390 370 350 330 310 290 270 and below MAX SPD 243 252 265 278 290 305 317 330 Note: Use manual control for cabin pressurization. MODE SEL..............................................................................................MAN MAN V/S CTL.................................................................................AS RQRD Ident.: ABN-34-C-00012474.0007001 / 08 FEB 13 STATUS MAX SPEED................................................ 330/0.82 RUD WITH CARE ABV 160 KT See (1) APPR PROC FOR LDG......................................... USE FLAP 3 APPR SPD....................................VREF + 15 KT Note: VLS is not displayed on the PFD. LDG DIST PROC...................................... APPLY FOR L/G GRVTY EXTN: MAX SPEED........................................200 KT LDG GRVTY EXTN..............................DOWN WHEN L/G DOWNLOCKED: L/G........................................................DOWN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE INOP SYS F/CTL PROT A/THR ADR 1+2+3 AP 1+2 WINDSHEAR DET L/G RETRACT RUD TRV LIM GPWS CAB PR 1+2 Other INOP SYS FLAPS AUTO RETRACT ALPHA LOCK ATC ALTI MODE FLAPS LOAD RELIEF TCAS ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.04D 01 DEC 14 ADR 1 + 2 + 3 FAULT (Cont'd) DURING FINAL APPR MAN V/S CTL...................................FULL UP ALTN LAW: PROT LOST BOTH PFDs ON SAME FMGC Note: Check speed is below VFE of CONF 1+F (215 kt) before selecting Flaps 1; since ADR parameters are lost, the SFCCs will set CONF 1+F instead of CONF 1. CAUTION Check that the outflow valve is fully open, and the cabin altitude is at airfield elevation before opening the doors. (1) At slats’ extension, full rudder travel authority is recovered. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.05A 01 DEC 14 NAV FM / GPS POS DISAGREE Ident.: ABN-34-00010562.0001001 / 08 FEB 13 Applicable to: MSN 0968-1118 A/C POS...........................................................................................................CHECK The following procedure is not displayed on the ECAM: If the ECAM alert is displayed during takeoff initiation: Continue takeoff and monitor navigation. If the ECAM alert is displayed during Climb, Cruise, or Descent: Check accuracy on the MCDU PROG page: If the ESTIMATED accuracy is below the REQUIRED accuracy: NAV mode and ND ARC/ROSE NAV may be used. If the ESTIMATED accuracy is above the REQUIRED accuracy: HDG/TRK mode and raw data must be used. When possible, compare the positions of both FMs with the GPIRS position, on the MCDU POSITION MONITOR page: If one FM position agrees with the onside GPIRS position: Use the associated AP/FD. If not: Deselect GPS and use raw data. If the ECAM alert is displayed during ILS/LOC approach (LOC green): Continue the approach. If the ECAM alert is displayed during a RNP approach: Go around if visual references are not sufficient. If the ECAM alert is displayed during a GLS approach: Go around if visual references are not sufficient. If the ECAM alert is displayed during a VOR, VOR-DME, NDB, or NDB-DME approach: Select HDG or TRK, and use raw data. NAV FM / GPS POS DISAGREE Ident.: ABN-34-00010562.0042001 / 08 FEB 13 Applicable to: MSN 0232-0700 A/C POS...........................................................................................................CHECK The following procedure is not displayed on the ECAM: If the ECAM alert is displayed during takeoff initiation: Continue takeoff and monitor navigation. If the ECAM alert is displayed during Climb, Cruise, or Descent: Check accuracy on the MCDU PROG page: TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.05B 01 DEC 14 NAV FM / GPS POS DISAGREE (Cont'd) If the ESTIMATED accuracy is below the REQUIRED accuracy: NAV mode and ND ARC/ROSE NAV may be used. If the ESTIMATED accuracy is above the REQUIRED accuracy: HDG/TRK mode and raw data must be used. Consider switching off the terrain functions of the GPWS. When possible, compare the positions of both FMs with the GPIRS position, on the MCDU POSITION MONITOR page: If one FM position agrees with the onside GPIRS position: Use the associated AP/FD. If not: Deselect GPS and use raw data. If the ECAM alert is displayed during ILS/LOC approach (LOC green): Continue the approach. If the ECAM alert is displayed during a RNP approach: Go around if visual references are not sufficient. If the ECAM alert is displayed during a GLS approach: Go around if visual references are not sufficient. If the ECAM alert is displayed during a VOR, VOR-DME, NDB, or NDB-DME approach: Select HDG or TRK, and use raw data. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 34.06A 01 DEC 14 IR ALIGNMENT IN ATT MODE Ident.: ABN-34-00010564.0001001 / 08 FEB 13 Applicable to: ALL If IR alignment is lost, the navigation mode is inoperative (red ATT flag on the PFD, and red HDG flag on the ND). Aircraft attitude and heading may be recovered by applying the following procedure: MODE SELECTOR................................................................................................ ATT LEVEL AIRCRAFT ATTITUDE........................................................................... HOLD CONSTANT AIRCRAFT SPEED.................................................................MAINTAIN Aircraft must stay level, with constant speed, for 30 s. DATA (MCDU KEY)..........................................................................................PRESS Displays the DATA INDEX page. IRS MONITOR (2L KEY)..................................................................................PRESS Displays the IRS MONITOR page. AIRCRAFT HEADING.......................................................................................ENTER The heading must be entered in the SET HDG field (5R key). Due to IRS drift, the magnetic heading must be periodically crosschecked with the standby compass and updated, if required. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.07A 01 DEC 14 EGPWS ALERTS Ident.: ABN-34-00010563.0003001 / 08 FEB 13 Applicable to: MSN 0232-0700 CAUTION During night or IMC conditions, immediately apply the procedure. Do not delay reaction for diagnosis. During daylight VMC conditions, with terrain and obstacles clearly in sight, the alert may be considered cautionary. Take positive corrective action until the alert stops or a safe trajectory is ensured. ″PULL UP″ – ″TERRAIN AHEAD PULL UP″: SIMULTANEOUSLY: AP..................................................................................................................... OFF PITCH....................................................................................................... PULL UP Pull to full backstick and maintain in that position. THRUST LEVERS.........................................................................................TOGA SPEED BRAKE lever...........................................................CHECK RETRACTED BANK........................................................................... WINGS LEVEL or ADJUST When flight path is safe and the warning stops: Decrease pitch attitude and accelerate. When speed is above VLS, and vertical speed is positive: Clean up aircraft, as required. “TERRAIN TERRAIN” – “TOO LOW TERRAIN”: Adjust the flight path, or initiate a go-around. ″TERRAIN AHEAD″: Adjust the flight path. Stop descent. Climb and/or turn, as necessary, based on analysis of all available instruments and information. “SINK RATE” – “DON’T SINK”: Adjust pitch attitude and thrust to silence the alert. “TOO LOW GEAR” – “TOO LOW FLAPS”: Perform a go-around. “GLIDE SLOPE”: Establish the aircraft on the glide slope, or set the G/S MODE pb-sw to OFF, if flight below the glide slope is intentional (non precision approach (NPA)). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.07B 01 DEC 14 EGPWS ALERTS Ident.: ABN-34-00010563.0009001 / 08 FEB 13 Applicable to: MSN 0968-1118 CAUTION During night or IMC conditions, immediately apply the procedure. Do not delay reaction for diagnosis. During daylight VMC conditions, with terrain and obstacles clearly in sight, the alert may be considered cautionary. Take positive corrective action until the alert stops or a safe trajectory is ensured. ″PULL UP″ – ″TERRAIN AHEAD PULL UP″ – ″OBSTACLE AHEAD PULL UP ″: SIMULTANEOUSLY: AP..................................................................................................................... OFF PITCH....................................................................................................... PULL UP Pull to full backstick and maintain in that position. THRUST LEVERS.........................................................................................TOGA SPEED BRAKE lever...........................................................CHECK RETRACTED BANK........................................................................... WINGS LEVEL or ADJUST When flight path is safe and the warning stops: Decrease pitch attitude and accelerate. When speed is above VLS, and vertical speed is positive: Clean up aircraft, as required. “TERRAIN TERRAIN” – “TOO LOW TERRAIN”: Adjust the flight path, or initiate a go-around. ″TERRAIN AHEAD″ – ″OBSTACLE AHEAD″: Adjust the flight path. Stop descent. Climb and/or turn, as necessary, based on analysis of all available instruments and information. “SINK RATE” – “DON’T SINK”: Adjust pitch attitude and thrust to silence the alert. “TOO LOW GEAR” – “TOO LOW FLAPS”: Perform a go-around. “GLIDE SLOPE”: Establish the aircraft on the glide slope, or set the G/S MODE pb-sw to OFF, if flight below the glide slope is intentional (non precision approach (NPA)). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.08A 01 DEC 14 TCAS WARNINGS Ident.: ABN-34-00010565.0004001 / 08 FEB 13 Applicable to: ALL Traffic advisory: “TRAFFIC” messages: Do not perform a maneuver based on a TA alone. Resolution advisory: All ″CLIMB″ and ″DESCEND″ or ″MAINTAIN VERTICAL SPEED MAINTAIN″ or ″ADJUST VERTICAL SPEED ADJUST″ or ″MONITOR VERTICAL SPEED″ type messages: AP (if engaged)................................................................................................ OFF BOTH FDs........................................................................................................ OFF Respond promptly and smoothly to an RA by adjusting or maintaining the pitch, as required, to reach the green area and/or avoid the red area of the vertical speed scale. Note: Avoid excessive maneuvers while aiming to keep the vertical speed just outside the red area of the VSI, and within the green area. If necessary, use the full speed range between Vαmax and VMAX. Respect stall, GPWS, or windshear warning. Notify ATC. The GO AROUND procedure must be performed, when an RA “CLIMB” or “INCREASE CLIMB” is triggered on final approach: Note: Resolution Advisories (RA) are inhibited below 900 ft. When “CLEAR OF CONFLICT” is announced: Resume normal navigation in accordance with ATC clearance. AP/FD can be reengaged as desired. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 36.01A 01 DEC 14 AIR ENG 1+2 BLEED FAULT Ident.: ABN-36-00010567.0004001 / 08 FEB 13 Applicable to: ALL Apply this procedure when both engine bleed supply systems are failed. In this configuration, the CAB PR EXCESS CAB ALT alert may trigger. In this case, apply the ECAM procedure associated to the CAB PR EXCESS CAB ALT alert before continuing this paper procedure. If AIR ENG 1 BLEED FAULT + AIR ENG 2 BLEED FAULT: X BLEED..................................................................................................... CLOSE ENG 1+2 BLEED............................................................................ OFF THEN ON Attempt one reset only. If the fault occurs again, consider the reset unsuccessful. If unsuccessful (no ENG BLEED recovered): DESCENT TO FL 100/MEA-MORA.....................................................INITIATE ENG 1+2 BLEED........................................................................................ OFF APU BLEED................................................................................................ OFF APU.........................................................................................................START WING A.ICE................................................................................................ OFF AVOID ICING CONDITIONS When below FL 220 and APU AVAIL: WING A.ICE................................................................................ KEEP OFF APU BLEED.............................................................................................ON If APU BLEED available: MAX FL 220 ENG 1+2 BLEED................................................................................ ON APU BLEED...................................................................................... OFF If no ENG BLEED recovered: APU BLEED...................................................................................ON ENG 1+2 BLEED......................................................................... OFF If PACK 1 inoperative: X BLEED..............................................................................OPEN If APU BLEED not available: DESCENT TO FL 100/MEA-MORA...................................... CONTINUE APU BLEED...................................................................................... OFF When at or below FL 100/MEA-MORA: ENG 1+2 BLEED...........................................................................ON If no ENG BLEED recovered: ENG 1+2 BLEED....................................................................OFF When ΔP < 1 PSI: RAM AIR............................................................................. ON MAX FL.......................................................... 100/MEA-MORA If severe ice accretion: MIN SPD.......................................................VLS+10 / G DOT MANEUVER WITH CARE APPR SPD.............................................................VLS+10 KT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 36.01B 01 DEC 14 AIR ENG 1+2 BLEED FAULT (Cont'd) LDG DIST PROC.......................................................... APPLY In all other cases: Applicable when at least one engine bleed supply system is failed due to LEAK, ENG FIRE, Start Air Valve Failed Open or APU BLEED LEAK FED BY ENGINE. DESCENT TO FL 100/MEA-MORA..........................................................INITIATE ENG 1+2 BLEED..............................................................................................OFF APU BLEED..................................................................................................... OFF APU.............................................................................................................. START WING A.ICE..................................................................................................... OFF X BLEED..................................................................................................... CLOSE AVOID ICING CONDITIONS If only AIR ENG 2 BLEED FAULT: When at or below FL 100/MEA-MORA: ENG 2 BLEED......................................................................................... ON If no ENG 2 BLEED recovered: ENG 2 BLEED.................................................................................. OFF When ΔP < 1 PSI: RAM AIR........................................................................................ON MAX FL.................................................................... 100/MEA-MORA If severe ice accretion: MIN SPD................................................................. VLS+10 / G DOT MANEUVER WITH CARE APPR SPD....................................................................... VLS+10 KT LDG DIST PROC.................................................................... APPLY If only AIR ENG 1 BLEED FAULT: When at or below FL 220: WING A.ICE................................................................................ KEEP OFF APU BLEED.............................................................................................ON If APU BLEED available: MAX FL 220 ENG 1 BLEED.................................................................................... ON APU BLEED...................................................................................... OFF If no ENG 1 BLEED recovered: APU BLEED...................................................................................ON ENG 1 BLEED............................................................................. OFF If APU BLEED not available: DESCENT TO FL 100/MEA-MORA...................................... CONTINUE APU BLEED...................................................................................... OFF When at or below FL 100/MEA-MORA: ENG 1 BLEED...............................................................................ON TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 36.01C 01 DEC 14 AIR ENG 1+2 BLEED FAULT (Cont'd) If no ENG 1 BLEED recovered: ENG 1 BLEED........................................................................OFF When ΔP < 1 PSI: RAM AIR............................................................................. ON MAX FL.......................................................... 100/MEA-MORA If severe ice accretion: MIN SPD.......................................................VLS+10 / G DOT MANEUVER WITH CARE APPR SPD.............................................................VLS+10 KT LDG DIST PROC.......................................................... APPLY If no AIR ENG 1(2) BLEED FAULT: When at or below FL 100/MEA-MORA and When ΔP < 1 PSI: RAM AIR.................................................................................................. ON MAX FL...............................................................................100/MEA-MORA If severe ice accretion: MIN SPD........................................................................... VLS+10 / G DOT MANEUVER WITH CARE APPR SPD..................................................................................VLS+10 KT LDG DIST PROC...............................................................................APPLY TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 QUICK REFERENCE HANDBOOK 70.01A ABNORMAL AND EMERGENCY PROCEDURES 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING Applicable to: MSN 0232-0472 Ident.: ABN-70-B-00010569.0006001 / 12 JUL 12 If none of the engines recovers, the flight crew must apply this paper procedure when required by the ALL ENG FLAME OUT ECAM procedure. Then, if time permits, the flight crew should clear the ECAM alerts and check the ECAM STATUS page. LAND ASAP RAT................................................................................................................ MAN ON ENG START SEL...................................................................................................IGN THRUST LEVERS................................................................................................ IDLE OPTIMUM RELIGHT SPD.............................................................................. 300/0.82 Increase speed during descent toward 300 kt . Do not exceed MMO. At 300 kt /M 0.82, with all engines stopped, it takes about 15 min to descend from FL 400 to the ground. The distance is about 100 nm. In the case of a speed indication failure (volcanic ash), the pitch attitude for an optimum relight speed is: WEIGHT Pitch (°) At or below 150 000 kg /330 000 lb -2.0 170 000 kg /374 000 lb -1.5 190 000 kg /418 000 lb -1.0 LANDING STRATEGY.............................................................................DETERMINE Determine whether a runway can be reached, or the most appropriate place for a forced landing/ditching. EMER ELEC POWER (if not automatically coupled).....................................MAN ON VHF1......................................................................................................................USE ATC.................................................................................................................. NOTIFY IF NO RELIGHT AFTER 30 s: ENG MASTERS................................................................................. OFF 30S/ON Unassisted start attempts can be repeated until successful, or until APU BLEED is available. IF UNSUCCESSFUL: CREW OXY MASKS (Above FL 100)................................................................ON WHEN BELOW FL 250: APU (if operative)................................................................................... START WHEN BELOW FL 200: WING ANTI ICE.......................................................................................... OFF APU BLEED.................................................................................................. ON IN SEQUENCE: ENG MASTERS (one at a time).............................................. OFF 30S/ON Ident.: ABN-70-B-00012120.0001001 / 21 MAR 11 When APU bleed is available or if engine restart is definitively considered impossible: OPTIMUM SPEED......................................................REFER TO TABLE BELOW GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS) Weight (1 000 kg) At or below FL 200 FL 300 FL 400 240 241 251 261 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.01B 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING (Cont'd) 220 229 239 249 200 217 227 237 180 205 215 225 160 193 203 213 140 181 191 201 120 169 179 189 At green dot speed, the aircraft can fly up to about 3 nm per 1 000 ft (with no wind). Average rate of descent is approximately 1 300 ft/min. CABIN AND COCKPIT...........................................................................PREPARE SEAT BELT/NO SMOKING............................................................................... ON COMMERCIAL..................................................................................................OFF USE RUDDER WITH CARE WHEN BELOW FL 150: RAM AIR............................................................................................................ ON Ident.: ABN-70-B-00012121.0002001 / 24 MAR 11 APPROACH PREPARATION Note: Final descent slope, when configured (CONF 1; L/G DOWN), will be approximately 1.5 nm per 1 000 ft (with no wind). BARO.................................................................................................................. SET CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF Ident.: ABN-70-B-00012122.0037001 / 30 MAR 12 IF FORCED LANDING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for landing (CONF 1 ; L/G DOWN): LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. At slat extension, if FUEL MAN FWD XFR has been selected T TANK MODE...................................................................................AUTO T TANK FEED....................................................................................AUTO MAX SPEED for GRAVITY EXTENSION..............................................200 KT L/G GRVTY EXTN................................................................................. DOWN Disregard “USE MAN PITCH TRIM” on the PFD, because the stabilizer is frozen in the position it was at, when the windmilling was insufficient to provide hydraulic power. When L/G downlocked L/G lever........................................................................................... DOWN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.01C 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING (Cont'd) APPROACH SPEED........................................................................ 170 KT Adjust the speed to the above given Vapp. Nevertheless, to reach the landing field/runway, the approach speed may be adjusted up to 240 kt (max speed with landing gear extended) GND SPLR........................................................................................... ARM MAX BRK PR...............................................................................1 000 PSI AT 2 000 FT AGL CABIN..............................................................................NOTIFY FOR LANDING AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF APU MASTER SW.......................................................................................... OFF BRAKES ON ACCU ONLY AFTER LANDING When the aircraft has stopped: PARKING BRK.............................................................................................ON ATC (VHF1)..........................................................................................NOTIFY FIRE pushbutton (ENG and APU)...........................................................PUSH AGENTS (ENG and APU)......................................................................DISCH If Evacuation required: EVACUATION................................................................................INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ELT................................................................................ CHECK EMITTING If not, switch on the transmitter. If Evacuation not required: CABIN CREW and PASSENGERS (PA)........................................ NOTIFY Ident.: ABN-70-B-00012123.0003001 / 30 MAR 12 IF DITCHING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for ditching (CONF 1 ; L/G UP): LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. At slat extension, if FUEL MAN FWD XFR has been selected T TANK MODE...................................................................................AUTO T TANK FEED....................................................................................AUTO L/G lever......................................................................................... CHECK UP TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK 70.01D ABNORMAL AND EMERGENCY PROCEDURES 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING (Cont'd) APPROACH SPEED............................................................................. 170 KT AT 2 000 FT AGL CABIN............................................................................ NOTIFY FOR DITCHING DITCHING pushbutton...................................................................................... ON Prefer ditching parallel to the swell. If that causes a strong crosswind, ditch into the wind. In all cases, touch down with a pitch attitude of approximately 11 ° Minimize aircraft vertical speed. AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF APU MASTER SW.......................................................................................... OFF AFTER DITCHING ATC (VHF1)...............................................................................................NOTIFY Fire pushbutton (ENG and APU)..................................................................PUSH AGENTS (ENG and APU)...........................................................................DISCH EVACUATION.......................................................................................... INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ELT.......................................................................................... CHECK EMITTING If not, switch on the transmitter ENG ALL ENG FLAMEOUT - FUEL REMAINING Applicable to: MSN 0700-1118 Ident.: ABN-70-B-00010569.0006001 / 12 JUL 12 If none of the engines recovers, the flight crew must apply this paper procedure when required by the ALL ENG FLAME OUT ECAM procedure. Then, if time permits, the flight crew should clear the ECAM alerts and check the ECAM STATUS page. LAND ASAP RAT................................................................................................................ MAN ON ENG START SEL...................................................................................................IGN THRUST LEVERS................................................................................................ IDLE OPTIMUM RELIGHT SPD.............................................................................. 300/0.82 Increase speed during descent toward 300 kt . Do not exceed MMO. At 300 kt /M 0.82, with all engines stopped, it takes about 15 min to descend from FL 400 to the ground. The distance is about 100 nm. In the case of a speed indication failure (volcanic ash), the pitch attitude for an optimum relight speed is: WEIGHT Pitch (°) At or below 150 000 kg /330 000 lb -2.0 170 000 kg /374 000 lb -1.5 190 000 kg /418 000 lb -1.0 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.01E 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING (Cont'd) LANDING STRATEGY.............................................................................DETERMINE Determine whether a runway can be reached, or the most appropriate place for a forced landing/ditching. EMER ELEC POWER (if not automatically coupled).....................................MAN ON VHF1......................................................................................................................USE ATC.................................................................................................................. NOTIFY IF NO RELIGHT AFTER 30 s: ENG MASTERS................................................................................. OFF 30S/ON Unassisted start attempts can be repeated until successful, or until APU BLEED is available. IF UNSUCCESSFUL: CREW OXY MASKS (Above FL 100)................................................................ON WHEN BELOW FL 250: APU (if operative)................................................................................... START WHEN BELOW FL 200: WING ANTI ICE.......................................................................................... OFF APU BLEED.................................................................................................. ON IN SEQUENCE: ENG MASTERS (one at a time).............................................. OFF 30S/ON Ident.: ABN-70-B-00012120.0001001 / 21 MAR 11 When APU bleed is available or if engine restart is definitively considered impossible: OPTIMUM SPEED......................................................REFER TO TABLE BELOW GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS) Weight (1 000 kg) At or below FL 200 FL 300 FL 400 240 241 251 261 220 229 239 249 200 217 227 237 180 205 215 225 160 193 203 213 140 181 191 201 120 169 179 189 At green dot speed, the aircraft can fly up to about 3 nm per 1 000 ft (with no wind). Average rate of descent is approximately 1 300 ft/min. CABIN AND COCKPIT...........................................................................PREPARE SEAT BELT/NO SMOKING............................................................................... ON COMMERCIAL..................................................................................................OFF USE RUDDER WITH CARE WHEN BELOW FL 150: RAM AIR............................................................................................................ ON TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.01F 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING (Cont'd) Ident.: ABN-70-B-00012121.0002001 / 24 MAR 11 APPROACH PREPARATION Note: Final descent slope, when configured (CONF 1; L/G DOWN), will be approximately 1.5 nm per 1 000 ft (with no wind). BARO.................................................................................................................. SET CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF Ident.: ABN-70-B-00012122.0019001 / 30 MAR 12 IF FORCED LANDING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for landing (CONF 1 ; L/G DOWN): LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. At slat extension, if FUEL MAN FWD XFR has been selected T TANK MODE...................................................................................AUTO T TANK FEED....................................................................................AUTO MAX SPEED for GRAVITY EXTENSION..............................................200 KT L/G GRVTY EXTN................................................................................. DOWN Disregard “USE MAN PITCH TRIM” on the PFD, because the stabilizer is frozen in the position it was at, when the windmilling was insufficient to provide hydraulic power. When L/G downlocked L/G lever........................................................................................... DOWN APPROACH SPEED........................................................................ 170 KT Adjust the speed to the above given Vapp. Nevertheless, to reach the landing field/runway, the approach speed may be adjusted up to 240 kt (max speed with slats extended) MAX BRK PR...............................................................................1 000 PSI GND SPLR........................................................................................... ARM AT 2 000 FT AGL CABIN..............................................................................NOTIFY FOR LANDING AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF APU MASTER SW.......................................................................................... OFF BRAKES ON ACCU ONLY AFTER LANDING When the aircraft has stopped: PARKING BRK.............................................................................................ON TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.01G 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING (Cont'd) ATC (VHF1)..........................................................................................NOTIFY FIRE pushbutton (ENG and APU)...........................................................PUSH AGENTS (ENG and APU)......................................................................DISCH If Evacuation required: EVACUATION................................................................................INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs.............................................................................................. OFF ELT................................................................................ CHECK EMITTING If not, switch on the transmitter. If Evacuation not required: CABIN CREW and PASSENGERS (PA)........................................ NOTIFY Ident.: ABN-70-B-00012123.0015001 / 30 MAR 12 IF DITCHING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for ditching (CONF 1 ; L/G UP): LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. At slat extension, if FUEL MAN FWD XFR has been selected T TANK MODE...................................................................................AUTO T TANK FEED....................................................................................AUTO L/G lever......................................................................................... CHECK UP APPROACH SPEED............................................................................. 170 KT AT 2 000 FT AGL CABIN............................................................................ NOTIFY FOR DITCHING DITCHING pushbutton...................................................................................... ON Prefer ditching parallel to the swell. If that causes a strong crosswind, ditch into the wind. In all cases, touch down with a pitch attitude of approximately 11 ° Minimize aircraft vertical speed. AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF APU MASTER SW.......................................................................................... OFF AFTER DITCHING ATC (VHF1)...............................................................................................NOTIFY Fire pushbutton (ENG and APU)..................................................................PUSH TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.01H 01 DEC 14 ENG ALL ENG FLAMEOUT - FUEL REMAINING (Cont'd) AGENTS (ENG and APU)...........................................................................DISCH EVACUATION.......................................................................................... INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs........................................................................................................ OFF ELT.......................................................................................... CHECK EMITTING If not, switch on the transmitter TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.02A 01 DEC 14 ENG ALL ENG FLAMEOUT - NO FUEL REMAINING Applicable to: MSN 0232-0472 Ident.: ABN-70-C-00010570.0004001 / 12 JUL 12 The flight crew must apply this paper procedure when required by the ALL ENG FLAME OUT ECAM procedure. Then, if time permits, the flight crew should clear the ECAM warnings and check the ECAM STATUS page. RAT................................................................................................................ MAN ON THRUST LEVERS................................................................................................ IDLE OPTIMUM SPEED......................................................................230 KT/GREEN DOT GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS) Weight (1000 kg) At or below FL 200 FL 300 FL 400 200 217 227 237 180 205 215 225 160 193 203 213 140 181 191 201 120 169 179 189 At green dot speed, the aircraft can fly up to approximately 3 nm per 1 000 ft (with no wind). Average rate of descent is approximately 1 300 ft/min. LANDING STRATEGY.............................................................................DETERMINE Determine if a runway can be reached, or determine the most appropriate place for a forced landing/ditching. EMER ELEC POWER (if not automatically coupled).....................................MAN ON VHF1......................................................................................................................USE ATC.................................................................................................................. NOTIFY CREW OXY MASKS (Above FL 100).....................................................................ON CABIN AND COCKPIT................................................................................ PREPARE SIGNS......................................................................................................................ON COMMERCIAL.......................................................................................................OFF USE RUDDER WITH CARE WHEN BELOW FL 150: RAM AIR............................................................................................................ ON Ident.: ABN-70-C-00012124.0001001 / 21 MAR 11 APPROACH PREPARATION Note: Final descent slope, when configured (CONF 1; L/G DOWN), will be approximately 1.5 nm per 1 000 ft (with no wind). BARO.................................................................................................................. SET CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF Ident.: ABN-70-C-00012125.0003001 / 30 MAR 12 IF FORCED LANDING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.02B 01 DEC 14 ENG ALL ENG FLAMEOUT NO FUEL REMAINING (Cont'd) At a suitable altitude (not below 3 000 ft AGL) , configure the aircraft for landing (CONF 1; L/G DOWN) : LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. MAX SPEED for GRAVITY EXTENSION..............................................200 KT L/G GRVTY EXTN................................................................................. DOWN Disregard ”USE MAN PITCH TRIM” on the PFD, because the stabilizer is frozen in the position it was at, when the windmilling was insufficient to provide hydraulic power. When L/G downlocked: L/G lever........................................................................................... DOWN APPROACH SPEED........................................................................ 170 KT Adjust the speed to the Vapp given above. However, to reach the landing field/runway, the approach speed may be adjusted up to 240 kt (max speed with slats extended). GND SPLR................................................................................................ ARM MAX BRK PR....................................................................................1 000 PSI AT 2 000 FT AGL CABIN..............................................................................NOTIFY FOR LANDING AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF BRAKES ON ACCU ONLY AFTER LANDING When the aircraft has stopped: PARKING BRK.............................................................................................ON ATC (VHF1)..........................................................................................NOTIFY If Evacuation required: EVACUATION................................................................................INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ELT................................................................................ CHECK EMITTING If not, switch on the transmitter If Evacuation not required: CABIN CREW and PASSENGERS (PA)........................................ NOTIFY Ident.: ABN-70-C-00012126.0003001 / 30 MAR 12 IF DITCHING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.02C 01 DEC 14 ENG ALL ENG FLAMEOUT NO FUEL REMAINING (Cont'd) At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for ditching (CONF 1, L/G UP): LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. L/G lever......................................................................................... CHECK UP APPROACH SPEED............................................................................. 170 KT AT 2 000 FT AGL CABIN............................................................................ NOTIFY FOR DITCHING DITCHING pushbutton...................................................................................... ON Prefer ditching parallel to the swell. If that causes a strong crosswind, ditch into the wind. In all cases, touch down with a pitch attitude of approximately 11 ° Minimize aircraft vertical speed. AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF AFTER DITCHING ATC (VHF1)...............................................................................................NOTIFY EVACUATION.......................................................................................... INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ELT.......................................................................................... CHECK EMITTING If not, switch on the transmitter TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.02D 01 DEC 14 ENG ALL ENG FLAMEOUT - NO FUEL REMAINING Applicable to: MSN 0700-1118 Ident.: ABN-70-C-00010570.0004001 / 12 JUL 12 The flight crew must apply this paper procedure when required by the ALL ENG FLAME OUT ECAM procedure. Then, if time permits, the flight crew should clear the ECAM warnings and check the ECAM STATUS page. RAT................................................................................................................ MAN ON THRUST LEVERS................................................................................................ IDLE OPTIMUM SPEED......................................................................230 KT/GREEN DOT GREEN DOT SPEED WITH ALL ENGINES INOPERATIVE (KNOTS) Weight (1000 kg) At or below FL 200 FL 300 FL 400 200 217 227 237 180 205 215 225 160 193 203 213 140 181 191 201 120 169 179 189 At green dot speed, the aircraft can fly up to approximately 3 nm per 1 000 ft (with no wind). Average rate of descent is approximately 1 300 ft/min. LANDING STRATEGY.............................................................................DETERMINE Determine if a runway can be reached, or determine the most appropriate place for a forced landing/ditching. EMER ELEC POWER (if not automatically coupled).....................................MAN ON VHF1......................................................................................................................USE ATC.................................................................................................................. NOTIFY CREW OXY MASKS (Above FL 100).....................................................................ON CABIN AND COCKPIT................................................................................ PREPARE SIGNS......................................................................................................................ON COMMERCIAL.......................................................................................................OFF USE RUDDER WITH CARE WHEN BELOW FL 150: RAM AIR............................................................................................................ ON Ident.: ABN-70-C-00012124.0001001 / 21 MAR 11 APPROACH PREPARATION Note: Final descent slope, when configured (CONF 1; L/G DOWN), will be approximately 1.5 nm per 1 000 ft (with no wind). BARO.................................................................................................................. SET CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF Ident.: ABN-70-C-00012125.0018001 / 30 MAR 12 IF FORCED LANDING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.02E 01 DEC 14 ENG ALL ENG FLAMEOUT NO FUEL REMAINING (Cont'd) At a suitable altitude (not below 3 000 ft AGL) , configure the aircraft for landing (CONF 1; L/G DOWN) : LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. MAX SPEED for GRAVITY EXTENSION..............................................200 KT L/G GRVTY EXTN................................................................................. DOWN Disregard ”USE MAN PITCH TRIM” on the PFD, because the stabilizer is frozen in the position it was at, when the windmilling was insufficient to provide hydraulic power. When L/G downlocked: L/G lever........................................................................................... DOWN APPROACH SPEED........................................................................ 170 KT Adjust the speed to the Vapp given above. However, to reach the landing field/runway, the approach speed may be adjusted up to 240 kt (max speed with slats extended). GND SPLR................................................................................................ ARM MAX BRK PR..................................................................................... 1000 PSI AT 2 000 FT AGL CABIN..............................................................................NOTIFY FOR LANDING AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF BRAKES ON ACCU ONLY AFTER LANDING When the aircraft has stopped: PARKING BRK.............................................................................................ON ATC (VHF1)..........................................................................................NOTIFY If Evacuation required: EVACUATION................................................................................INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs.............................................................................................. OFF ELT................................................................................ CHECK EMITTING If not, switch on the transmitter If Evacuation not required: CABIN CREW and PASSENGERS (PA)........................................ NOTIFY Ident.: ABN-70-C-00012126.0015001 / 30 MAR 12 IF DITCHING ANTICIPATED APPROACH MIN RAT SPEED........................................................................................140 KT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.02F 01 DEC 14 ENG ALL ENG FLAMEOUT NO FUEL REMAINING (Cont'd) At a suitable altitude (not below 3 000 ft AGL), configure the aircraft for ditching (CONF 1, L/G UP): LAND RECOVERY.......................................................................................ON FLAP 1.................................................................................................SELECT EMER GEN is lost at slats’ extension. The aircraft is supplied by batteries only. L/G lever......................................................................................... CHECK UP APPROACH SPEED............................................................................. 170 KT AT 2 000 FT AGL CABIN............................................................................ NOTIFY FOR DITCHING DITCHING pushbutton...................................................................................... ON Prefer ditching parallel to the swell. If that causes a strong crosswind, ditch into the wind. In all cases, touch down with a pitch attitude of approximately 11 ° Minimize aircraft vertical speed. AT 500 FT AGL BRACE FOR IMPACT............................................................................... ORDER AT TOUCHDOWN ENG MASTERS.............................................................................................. OFF AFTER DITCHING ATC (VHF1)...............................................................................................NOTIFY EVACUATION.......................................................................................... INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs........................................................................................................ OFF ELT.......................................................................................... CHECK EMITTING If not, switch on the transmitter TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.03A 01 DEC 14 ENG RELIGHT (IN FLIGHT) Ident.: ABN-70-00010571.0012001 / 01 DEC 14 Applicable to: MSN 1112-1118 Note: The ECAM may trigger ENG START VALVE FAULT – START VALVE NOT CLOSED before or during the engine relight attempt. In such a case: ‐ If the engine restart is unsuccessful, disregard the ENG START VALVE FAULT procedure and attempt a new relight. ‐ If the engine restart is successful, apply the ENG START VALVE FAULT procedure. MAX GUARANTEED ALTITUDE................................................................. 30 000 FT ENG MASTER (affected engine)...........................................................................OFF THR LEVER (affected engine)................................................................CHECK IDLE ENG START SEL...................................................................................................IGN X BLEED.............................................................................................................OPEN WING ANTI ICE (for starter assisted start)........................................................... OFF ENG MASTER (affected engine)............................................................................ ON Be aware that contrary to autostart on ground, the crew must take appropriate action in case of abnormal start. Engine light up should be achieved within 30 s after fuel flow increases. ‐ Monitor N2 ‐ If not certain about successful relight, move the thrust lever forward and check engine response. When idle reached (AVAIL indication pulses in green) : ENG START SEL......................................................................................... NORM TCAS MODE SEL .......................................................................check TA/RA Check that the selector is at TA/RA since if the ENG SHUT DOWN procedure has been applied, the TCAS mode selector may have been set at TA position. Affected SYS.......................................................................................... RESTORE If no relight: ENG MASTER (affected engine)..................................................................... OFF TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.03B 01 DEC 14 ENG RELIGHT (IN FLIGHT) (Cont'd) IN FLIGHT ENGINE RELIGHT ENVELOPE ENG RELIGHT (IN FLIGHT) Ident.: ABN-70-00010571.0002001 / 01 OCT 12 Applicable to: MSN 0466-0700 MAX GUARANTEED ALTITUDE................................................................. 30 000 FT ENG MASTER (affected engine)...........................................................................OFF THR LEVER (affected engine)................................................................CHECK IDLE ENG START SEL...................................................................................................IGN X BLEED.............................................................................................................OPEN WING ANTI ICE (for starter assisted start)........................................................... OFF ENG MASTER (affected engine)............................................................................ ON Be aware that contrary to autostart on ground, the crew must take appropriate action in case of abnormal start. Engine light up should be achieved within 30 s after fuel flow increases. ‐ Monitor N2 ‐ If not certain about successful relight, move the thrust lever forward and check engine response. When idle reached (AVAIL indication pulses in green) : ENG START SEL......................................................................................... NORM TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.03C 01 DEC 14 ENG RELIGHT (IN FLIGHT) (Cont'd) TCAS MODE SEL ........................................................................ check TA/RA Check that the selector is at TA/RA since if the ENG SHUT DOWN procedure has been applied, the TCAS mode selector may have been set at TA position. Affected SYS.......................................................................................... RESTORE If no relight: ENG MASTER (affected engine)..................................................................... OFF ENG RELIGHT (IN FLIGHT) Ident.: ABN-70-00010571.0001001 / 01 OCT 12 Applicable to: MSN 0232-0361, 0968 Note: The ECAM may trigger ENG START VALVE FAULT – START VALVE NOT CLOSED before or during the engine relight attempt. In such a case: ‐ If the engine restart is unsuccessful, disregard the ENG START VALVE FAULT procedure and attempt a new relight. ‐ If the engine restart is successful, apply the ENG START VALVE FAULT procedure. MAX GUARANTEED ALTITUDE................................................................. 30 000 FT ENG MASTER (affected engine)...........................................................................OFF THR LEVER (affected engine)................................................................CHECK IDLE ENG START SEL...................................................................................................IGN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.03D 01 DEC 14 ENG RELIGHT (IN FLIGHT) (Cont'd) X BLEED.............................................................................................................OPEN WING ANTI ICE (for starter assisted start)........................................................... OFF ENG MASTER (affected engine)............................................................................ ON Be aware that contrary to autostart on ground, the crew must take appropriate action in case of abnormal start. Engine light up should be achieved within 30 s after fuel flow increases. ‐ Monitor N2 ‐ If not certain about successful relight, move the thrust lever forward and check engine response. When idle reached (AVAIL indication pulses in green) : ENG START SEL......................................................................................... NORM TCAS MODE SEL ........................................................................ check TA/RA Check that the selector is at TA/RA since if the ENG SHUT DOWN procedure has been applied, the TCAS mode selector may have been set at TA position. Affected SYS.......................................................................................... RESTORE If no relight: ENG MASTER (affected engine)..................................................................... OFF IN FLIGHT ENGINE RELIGHT ENVELOPE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Applicable to: MSN 0232-0361, 0968-1118 70.04A 01 DEC 14 ENG 1(2) STALL Ident.: ABN-70-A-00010572.0005001 / 08 FEB 13 A stall may be indicated by varying degrees of abnormal engine noises, accompanied by flame from the engine exhaust (and possibly from engine inlet in severe cases), fluctuating performance parameters, sluggish or no thrust lever response, high EGT and/or a rapid EGT rise when thrust lever is advanced. Engine stalls must be reported for maintenance action. Stall is detected by the FADEC: In flight: FUEL ADJUSTED Fuel/Air ratio is automatically decreased until the stall disappears. THR LEVER 1(2)........................................................................................IDLE ENG 1(2) PARAMETERS...................................................................... CHECK If abnormal: ENG MASTER 1(2)................................................................................OFF On ground: THR LEVER 1(2)........................................................................................IDLE ENG MASTER 1(2)..................................................................................... OFF If the crew detects a stall before the ECAM activation: The following non ECAM procedure may be applied: THR LEVER 1(2)............................................................................................. IDLE ENG PARAMETERS 1(2)........................................................................... CHECK Note: If parameter trend toward normal and no redline exceedence exists, monitor the parameters. If abnormal parameters persist above redline: ENG MASTER 1(2)..................................................................................... OFF ENG 1(2) SHUT DOWN Apply ENG SHUT DOWN procedure. Engine restart at crew discretion. If normal parameters: ENG A ICE 1(2)............................................................................................ ON WING A ICE..................................................................................................ON Operation of the engine and wing anti ice will increase the stall margin but EGT will increase accordingly. THR LEVER 1(2).............................................................. SLOWLY ADVANCE If stall does not reoccur: Continue engine operation. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK Applicable to: MSN 0466-0700 ABNORMAL AND EMERGENCY PROCEDURES 70.04B 01 DEC 14 ENG 1(2) STALL Ident.: ABN-70-A-00010573.0001001 / 30 MAR 12 A stall may be indicated by varying degrees of abnormal engine noises, accompanied by flame from the engine exhaust (and possibly from engine inlet in severe cases), fluctuating performance parameters, sluggish or no thrust lever response, high EGT and/or a rapid EGT rise when thrust lever is advanced. Engine stalls must be reported for maintenance action. THR LEVER (affected engine)............................................................................. IDLE ENG PARAMETERS (affected engine)............................................................CHECK If abnormal parameters: ENG MASTER (affected engine)..................................................................... OFF ENG 1(2) SHUT DOWN Engine restart at crew discretion. If normal parameters: ENG A ICE (affected engine)............................................................................ ON WING A ICE.......................................................................................................ON Operation of the engine and wing anti ice will increase the stall margin but EGT will increase accordingly. THR LEVER (affected engine)............................................... SLOWLY ADVANCE If stall does not reoccur: Continue engine operation TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.05A 01 DEC 14 ENG TAILPIPE FIRE Ident.: ABN-70-00010574.0002001 / 08 FEB 13 Applicable to: ALL CAUTION External fire agents can cause severe corrosive damage and should therefore, only be considered after having applied the following procedure: ENG MASTER (affected).......................................................................................OFF AIR BLEED PRESS.................................................................................. ESTABLISH BEACON..................................................................................................................ON When N2 < 30 %: ENG START SEL........................................................................................CRANK MAN START.......................................................................................................ON When burning has stopped: MAN START................................................................................................OFF ENG START SEL.................................................................................... NORM TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 70.06A 01 DEC 14 HIGH ENGINE VIBRATION Ident.: ABN-70-00010575.0002001 / 21 JUL 14 Applicable to: ALL The vibration advisory on ECAM is mainly a guideline for the flight crew to monitor engine parameters more closely. The ECAM vibration advisory alone does not require engine shut down. Note: 1. High engine vibration may be accompanied by cockpit and cabin smoke and/or the smell of burning. This may be due only to compressor blade tip contact with associated abradable seals. 2. High N1 vibration are generally accompanied by perceivable airframe vibrations. High N2 vibration can occur without perceivable airframe vibrations. ENG PARAMETERS........................................................................................ CHECK Check engine parameters and especially EGT; crosscheck with other engine. Report in maintenance logbook. If icing is suspected: An increase of N1 vibration in icing conditions with or without engine anti ice may be due to fan blades and/or spinner icing. Icing may be suspected if N1 vibration occurs without other engine parameters variation. A/THR............................................................................................................... OFF ENG ANTI ICE............................................................................................ CHECK If ENG ANTI ICE is still off, switch it ON at idle fan speed, one engine after the other with approximately 30 s interval. THRUST (one engine at a time)....................................... IDLE THEN INCREASE Reduce thrust to idle if flight conditions permit. To shed ice, it may be necessary to perform several thrust variations between idle and a thrust compatible with the flight phase. For efficient ice shedding, thrust should be increased to at least 80 % N1 if flight conditions permit. After each thrust variation, vibrations should decrease, indicating the progress of the ice shedding. When the ice is shed, vibrations should return to normal and the flight crew can resume normal engine operation. If icing is not suspected: If above vibration advisory: THRUST (affected engine)..................................................................REDUCE If flight conditions permit, reduce thrust to maintain vibration level below the advisory threshold. If the VIB indication does not decrease following thrust reduction, this may indicate other problems on the engine. Note: If possible, shut down the engine after landing for taxing, if vibrations above the advisory threshold are, or have been experienced. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.07A 01 DEC 14 SUSPECTED ENG FUEL SYS CONTAMINATION Ident.: ABN-70-00013978.0004001 / 04 JUN 13 Applicable to: MSN 0466-0700 This procedure must be applied if one of the two following conditions is encountered. In that case, a fuel contamination can be highly suspected. If ECAM caution ENG 1(2) CTL SYS FAULT is triggered with the associated message “AVOID RAPID THRUST CHANGE” or “ENG 1(2) AT IDLE”, and with rapid and continuous N1 fluctuation indications on both engines: A/THR............................................................................................................... OFF If N1 fluctuations on both engines stop: ECAM PROC.......................................................................................... APPLY A/THR............................................................................................... KEEP OFF If N1 fluctuations on both engines continue: ENG FUEL SYS CONTAMINATION PROC........................................... APPLY If ECAM cautions ENG 1 CTL SYS FAULT and ENG 2 CTL SYS FAULT are triggered with the associated message “AVOID RAPID THRUST CHANGE” or “ENG 1(2) AT IDLE”: A/THR............................................................................................................... OFF ENG FUEL SYS CONTAMINATION PROC................................................ APPLY SUSPECTED ENG FUEL SYS CONTAMINATION Ident.: ABN-70-00013978.0003001 / 08 FEB 13 Applicable to: MSN 0232-0361, 0968-1118 This procedure must be applied if one of the two following conditions is encountered. In that case, a fuel contamination can be highly suspected. If ECAM caution ENG 1(2) CTL SYS FAULT is triggered with the associated message “AVOID RAPID THRUST CHANGE” or “ENG 1(2) SLOW RESPONSE”, and with rapid and continuous EPR fluctuation indications on both engines: A/THR............................................................................................................... OFF If EPR fluctuations on both engines stop: ECAM PROC.......................................................................................... APPLY A/THR............................................................................................... KEEP OFF If EPR fluctuations on both engines continue: ENG FUEL SYS CONTAMINATION PROC........................................... APPLY If ECAM cautions ENG 1 CTL SYS FAULT and ENG 2 CTL SYS FAULT are triggered with the associated message “AVOID RAPID THRUST CHANGE” or “ENG 1(2) SLOW RESPONSE”: A/THR............................................................................................................... OFF ENG FUEL SYS CONTAMINATION PROC................................................ APPLY TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 70.07B ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 01 DEC 14 ENG FUEL SYS CONTAMINATION Ident.: ABN-70-00013979.0006001 / 24 FEB 14 Applicable to: MSN 0466-0700 This procedure must be applied if a fuel contamination has been confirmed by the application of the Refer to QRH ABN-70 Suspected ENG Fuel Sys Contamination procedure. This fuel contamination may result, in the worst case, in a loss of engine thrust control. This procedure aims at maintaining the thrust on one engine while minimizing the thrust changes on the other, in order to prevent contaminant from blocking the mechanical devices of engine thrust regulation. In case of ENG 1(2) CTL SYS FAULT on only one engine: ‐ Set and maintain the thrust on the engine affected by the ECAM caution ‐ Minimize the thrust changes on the engine not affected by the ECAM caution In case of ENG 1 and 2 CTL SYS FAULT (both engines affected by the ECAM caution): ‐ Set and maintain the thrust on the first engine affected by the ECAM caution ‐ Minimize the thrust changes on the second engine affected by the ECAM caution WHEN FUEL CONTAMINATION IS CONFIRMED LAND ASAP A/THR...................................................................................................... KEEP OFF MAN THR (ECAM affected or 1st ECAM affected engine)........SET and MAINTAIN Set the thrust (N1) on the applicable engine according to the following table. This thrust should be maintained until final approach. THRUST SETTING (N1) GROSS WEIGHT ( 1 000 kg ) N1(%) 120 130 140 150 160 170 180 190 200 210 220 230 240 71.4 72.1 72.9 73.7 74.5 75.5 76.5 77.5 78.5 79.6 80.8 81.8 83.0 For cruise MAN THR (Non ECAM affected or 2nd ECAM affected engine)......................... ..................................................................................................... SET AS RQRD Minimize thrust changes on the applicable engine. Descent MAN THR (Non ECAM affected or 2nd ECAM affected engine)..................IDLE SPD BRK............................................................................................. AS RQRD Manage the descent using speed brakes as necessary so as to perform a level-off at approximately 3 000 ft AGL and 20 nm from the runway threshold. ATC..........................................................................................................NOTIFY Notify ATC to ensure runway availability for landing. Approach At a suitable altitude (approximately 3 000 ft AGL): LEVEL OFF...................................................................................... INITIATE AIRCRAFT ...............................................................CONFIGURE FOR LDG To decelerate the aircraft, manage early gear extension and/or use speed brakes in order to be fully configured when intercepting the final approach path. FOR LDG.................................................................................. USE FLAP FULL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 70.07C ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 01 DEC 14 ENG FUEL SYS CONTAMINATION (Cont'd) Final approach TARGET SPD............................................................................................. VAPP When fully configured, if the speed trend decreases below VAPP, adjust the thrust on the Non affected ECAM or 2nd ECAM affected engine. In case of overspeed adjust the thrust on the ECAM affected or 1st ECAM affected engine. Landing NORMAL OPS...................................................................................... RESUME Resume normal operations: Retard thrust levers as usual, select reverse thrust and apply brakes as required. ENG FUEL SYS CONTAMINATION Ident.: ABN-70-00013979.0004001 / 24 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 This procedure must be applied if a fuel contamination has been confirmed by the application of the Refer to QRH ABN-70 Suspected ENG Fuel Sys Contamination procedure. This fuel contamination may result, in the worst case, in a loss of engine thrust control. This procedure aims at maintaining the thrust on one engine while minimizing the thrust changes on the other, in order to prevent contaminant from blocking the mechanical devices of engine thrust regulation. In case of ENG 1(2) CTL SYS FAULT on only one engine: ‐ Set and maintain the thrust on the engine affected by the ECAM caution ‐ Minimize the thrust changes on the engine not affected by the ECAM caution In case of ENG 1 and 2 CTL SYS FAULT (both engines affected by the ECAM caution): ‐ Set and maintain the thrust on the first engine affected by the ECAM caution ‐ Minimize the thrust changes on the second engine affected by the ECAM caution WHEN FUEL CONTAMINATION IS CONFIRMED LAND ASAP A/THR...................................................................................................... KEEP OFF MAN THR (ECAM affected or 1st ECAM affected engine)........SET and MAINTAIN Set the thrust (N1) on the applicable engine according to the following table. This thrust should be maintained until final approach. THRUST SETTING (N1) GROSS WEIGHT ( 1 000 kg ) N1(%) 120 130 140 150 160 170 180 190 200 210 220 230 240 62.4 63.0 63.7 64.5 65.2 66.0 66.8 67.7 68.7 69.6 70.6 71.7 73.0 For cruise MAN THR (Non ECAM affected or 2nd ECAM affected engine)......................... ..................................................................................................... SET AS RQRD Minimize thrust changes on the applicable engine. Descent MAN THR (Non ECAM affected or 2nd ECAM affected engine)..................IDLE SPD BRK............................................................................................. AS RQRD Manage the descent using speed brakes as necessary so as to perform a level-off at approximately 3 000 ft AGL and 20 nm from the runway threshold. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.07D 01 DEC 14 ENG FUEL SYS CONTAMINATION (Cont'd) ATC..........................................................................................................NOTIFY Notify ATC to ensure runway availability for landing. Approach At a suitable altitude (approximately 3 000 ft AGL): LEVEL OFF...................................................................................... INITIATE AIRCRAFT ...............................................................CONFIGURE FOR LDG To decelerate the aircraft, manage early gear extension and/or use speed brakes in order to be fully configured when intercepting the final approach path. FOR LDG.................................................................................. USE FLAP FULL Final approach TARGET SPD............................................................................................. VAPP When fully configured, if the speed trend decreases below VAPP, adjust the thrust on the Non affected ECAM or 2nd ECAM affected engine. In case of overspeed adjust the thrust on the ECAM affected or 1st ECAM affected engine. Landing NORMAL OPS...................................................................................... RESUME Resume normal operations: Retard thrust levers as usual, select reverse thrust and apply brakes as required. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.01A 01 DEC 14 CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE Ident.: ABN-80-00010581.0012001 / 08 FEB 13 Applicable to: MSN 0232-0361, 0968-1118 LANDING WEIGHT.......................................................................................... CHECK If the aircraft weight is above the maximum weight for circling in CONF 3 (given in the table below) : The aircraft cannot maintain flight level with CONF 3 and landing gear down. Delay gear extension. Note: ‐ If the approach is flown at less than 750 ft RA, the warning “L/G NOT DOWN” will be triggered. The pilot can cancel aural warning by pressing the EMER CANC pb on the ECAM control panel. ‐ ”TOO LOW GEAR” warning is to be expected, if the landing gear is not downlocked at 500 ft RA. MAXIMUM WEIGHT FOR CIRCLING IN CONF 3 (1000 KG) AIRPORT ELEVATION (feet) OAT (°C) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000 0 220 214 198 186 174 170 158 158 5 220 214 198 186 174 170 158 158 10 220 214 198 186 174 170 158 154 15 220 214 198 186 174 158 158 150 20 220 214 198 184 168 158 154 148 25 220 214 194 176 158 152 148 142 30 220 206 186 170 154 146 142 35 212 200 180 158 148 140 40 206 192 172 158 45 198 182 158 50 186 172 55 172 CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE Ident.: ABN-80-00010581.0013001 / 08 FEB 13 Applicable to: MSN 0466-0700 LANDING WEIGHT.......................................................................................... CHECK If the aircraft weight is above the maximum weight for circling in CONF 3 (given in the table below) : The aircraft cannot maintain flight level with CONF 3 and landing gear down. Delay gear extension. Note: ‐ If the approach is flown at less than 750 ft RA, the warning “L/G NOT DOWN” will be triggered. The pilot can cancel aural warning by pressing the EMER CANC pb on the ECAM control panel. ‐ ”TOO LOW GEAR” warning is to be expected, if the landing gear is not downlocked at 500 ft RA. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.01B 01 DEC 14 CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE (Cont'd) MAXIMUM WEIGHT FOR CIRCLING IN CONF 3 (1000 KG) AIRPORT ELEVATION (feet) OAT (°C) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000 0 224 216 206 198 188 180 172 158 5 224 214 206 196 188 180 158 154 10 224 214 206 196 186 174 158 148 15 222 214 206 194 180 158 154 142 20 222 214 202 186 174 158 148 138 25 222 208 194 180 158 154 144 132 30 214 200 188 174 158 150 138 35 208 194 182 168 156 144 40 198 186 176 158 45 190 180 168 50 182 172 55 176 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02A 01 DEC 14 BOMB ON BOARD Ident.: ABN-80-00010582.0001001 / 08 FEB 13 Applicable to: MSN 0232-0472 IF POSSIBLE, LAND AND EVACUATE THE AIRCRAFT IMMEDIATELY. If it is not possible to land and evacuate the aircraft within 30 min, apply the following procedures: COCKPIT PROCEDURES BACKGROUND To avoid the activation of an altitude-sensitive bomb, the cabin altitude should not exceed the value at which the bomb has been discovered. To reduce the effects of the explosion, the aircraft should fly as long as possible with approximately 1 PSI differential pressure, to help the blast go outwards. 1 PSI differential pressure corresponds to a 2 500 ft difference between the aircraft and the cabin altitude. These conditions are achieved by using the manual pressure control. PROCEDURE The following procedure assumes that it is initiated during climb or cruise: First, maintain the cabin altitude. While maintaining the cabin altitude, descend the aircraft to the cabin altitude + 2 500 ft and maintain ΔP at 1 PSI. During further steps of descent, maintain ΔP at 1 PSI. For landing, reduce the differential pressure to zero, until the final approach. If flight conditions are different, the crew should adapt the procedure, bearing in mind the above-mentioned principles (background paragraph). AIRCRAFT (if climbing).......................................................................LEVEL OFF CABIN PRESS MODE SEL............................................................................MAN CAB ALT................................................................................................MAINTAIN CABIN CREW............................................................................................NOTIFY ATC/COMPANY OPERATIONS................................................................NOTIFY FUEL RESERVES............................................................................. DETERMINE Keep in mind that when flying at cabin altitude + 2 500 ft, the fuel consumption in CONF 1, with landing gear down, will be about 2.1 times that consumed in clean configuration. NEXT SUITABLE AIRPORT..............................................................DETERMINE FCU SPEED SELECTION KNOB..............................................PULL AND TURN Select the most appropriate speed, taking into account the time to destination, the fuel consumption and the fact that low speed could reduce the consequences of possible structural damage, if the bomb explodes. DESCENT TO CAB ALT + 2 500 ft or MEA or minimum obstacle clearance altitude ................................................................................................................. INITIATE AVOID SHARP MANEUVERS TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.02B 01 DEC 14 BOMB ON BOARD (Cont'd) CAB ALT................................................................................................MAINTAIN When at CAB ALT + 2500 ft: 1 PSI ΔP...........................................................................................MAINTAIN GALLEY......................................................................................................OFF When the bomb is secured at the LRBL or cannot be moved: EMER EXIT LT....................................................................................... ON COMMERCIAL...................................................................................... OFF FLAPS (fuel permitting)..................................................... AT LEAST CONF 1 For landing, use normal configuration. LANDING GEAR (fuel permitting, except for flight over water)..............DOWN For any other steps of descent: 1 PSI ΔP...........................................................................................MAINTAIN During approach: CABIN PRESS MODE SEL.................................................................... AUTO When the aircraft on ground and stopped in a remote area (if possible): If Evacuation required: EVACUATION................................................................................INITIATE Avoid exits and exiting on the same side as the bomb and near the bomb. Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . If Evacuation not required: CABIN CREW and PASSENGERS (PA)........................................ NOTIFY CABIN PROCEDURES If a suspect device is found in the cabin: WARNING Do not cut or disconnect any wires and do not open or attempt to gain entry to internal components of a closed or concealed suspect device. Any attempt may result in an explosion. Booby-trapped closed devices have been used on aircraft in the past. WARNING Alternate locations must not be used without consulting with an aviation explosives security specialist. Never take a suspect device to the flight deck. CAUTION The least risk bomb location for the aircraft structure and systems is center of the RH aft cabin door. EOD PERSONNEL ON BOARD...................................................................CHECK Announce: “Is there any EOD personnel on board ?”. By using the initials, only persons familiar with EOD (Explosive Ordnance Disposal) will be made aware of the problem. DO NOT OPEN THE BOMB DO NOT CUT BOMB’S WIRES SECURE BOMB AGAINST SLIPPING TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02C 01 DEC 14 BOMB ON BOARD (Cont'd) PROTECT BOMB AGAINST SHOCKS Secure in the attitude found and do not lift before having checked for an anti-lift ignition device. PASSENGERS..............................................................LEAD AWAY FROM BOMB Move passengers at least 4 seat rows away from the bomb location. On full flights, it may be necessary to double up passengers to achieve standoff from the suspect device. Passengers near the bomb should protect their heads with pillows, blankets. All passengers must remain seated with seatbelts on and, if possible, head below the top of the head rest. Seat backs and tray tables must be in their full upright position. Service items may need to be collected in order to secure tray tables. CREW REST AREAS.............................................................................EVACUATE For aircraft equipped with crew rest areas (FCRC, LDMCR, BCRC). PORTABLE ELECTRONIC DEVICES................................................ SWITCH OFF The cabin crews must command passengers to switch off all portable electronic devices. BOMB.....................................................................CHECK NO ANTI-LIFT DEVICE To check for an anti-lift switch or lever, slide a string or stiff card (such as the emergency information card) under the bomb, without disturbing the bomb. If the string or card cannot be slipped under the bomb, it may indicate that an anti-lift switch or lever is present and that the bomb cannot be moved. If a card is used and can be slid under the bomb, leave it under the bomb and move together with the bomb. If it is not possible to move the bomb, then it should be surrounded with a single thin sheet of plastic (e. g. trash bag), then with wetted materials, and other blast attenuation materials such as seat cushions and soft carry-on baggage. Move personnel as far away from the bomb location as possible. EMERGENCY EQUIPMENT................................................. REMOVE AND STOW Emergency equipment (PBE, fire extinguisher, ...) located close to the LRBL must be removed and stowed in alternate location. GALLEY/IFE POWER.........................................................................................OFF All galley and IFE equipment located close to the LRBL must be switched off. If the bomb can be moved: RH AFT CABIN DOOR SLIDE............................................................... DISARM LEAST RISK BOMB LOCATION (LRBL)............................................ PREPARE Build up a platform of solid baggage against the door up to about 25 cm (10 in) below the middle of the door. On top of this, build up at least 25 cm (10 in) of wetted material such as blankets and pillows. Place a single thin sheet of plastic (e. g. trash bag) on top of the wetted materials. This prevents any possible short circuit. CAUTION Do not omit the plastic sheets, as the suspect device could get wet and possibly short circuit electronic components causing inadvertent device activation. BOMB INDICATION LINE................................................................... POSITION Note: A bomb location indicator line is a 6 ft to 8 ft (1.8 m to 2.4 m) line (e.g. neckties, headset cord, or belts connected together) preferably of constrating color, that helps the responding bomb squad find the precise location of the suspect device within the LRBL stack once constructed. Position the bomb indication line from the location on the platform where you will place the suspect device, EXTENDING outward into the aisle. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02D 01 DEC 14 BOMB ON BOARD (Cont'd) BOMB........................................................................................ MOVE TO LRBL Carefully carry in the attitude found and place on top of the wetted materials in the same attitude and as close to the door structure as possible. CAUTION Ensure that the suspect device, when placed on the stack against the door, is above the slide pack but not against the door handle, and if possible, avoid placement in the view port. LEAST RISK BOMB LOCATION (LRBL)..........................................COMPLETE Place an additional single thin sheet of plastic over the bomb. CAUTION Do not omit the plastic sheets, as the suspect device could get wet and possibly short circuit electronic components causing inadvertent device activation. Build up at 25 cm (10 in) of wetted material around the sides and on top of the bomb. DO NOT PLACE ANYTHING BETWEEN THE BOMB AND THE DOOR, AND MINIMIZE AIRSPACE AROUND THE BOMB. The idea is to build up a protective surrounding of the bomb so that the explosive force is directed in the only unprotected area into the door structure. Fill the area around the bomb with seat cushions and other soft materials such as hand luggage (saturated with water or any other nonflammable liquid) up to the cabin ceiling, compressing as much as possible. Secure the LRBL stack in place using belt, ties or other appropriate materials. The more material stacked around the bomb, the less the damage will be. USE ONLY SOFT MATERIAL. AVOID USING MATERIALS CONTAINING ANY INFLAMMABLE LIQUID AND ANY METAL OBJECTS WHICH COULD BECOME DANGEROUS PROJECTILES. LRBL STACK TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.02E 01 DEC 14 BOMB ON BOARD (Cont'd) PASSENGERS.............................................................................MOVE/ADVISE Move passengers at least 4 seat rows away from the least risk bomb location (RH aft cabin door). On full flights, it may be necessary to double up passengers to achieve standoff from the suspect device. Passengers near the bomb should protect their heads with pillows, blankets. All passengers must remain seated with seatbelts on and, if possible, head below the top of the head rest. Seat backs and tray tables must be in their full upright position. CABIN CREW............................................................ NOTIFY COCKPIT CREW Cabin crew notify the flight crew that the bomb is secured at the LRBL. EVACUATION/DISEMBARKATION.....................................................EXECUTE Evacuate through normal and emergency exits on the opposite side of the "bomb" location. Do not use the door just opposite the "bomb". Use all available airport facilities to disembark without delay. BOMB ON BOARD Ident.: ABN-80-00010582.0003001 / 08 FEB 13 Applicable to: MSN 0700-1118 IF POSSIBLE, LAND AND EVACUATE THE AIRCRAFT IMMEDIATELY. If it is not possible to land and evacuate the aircraft within 30 min, apply the following procedures: COCKPIT PROCEDURES BACKGROUND To avoid the activation of an altitude-sensitive bomb, the cabin altitude should not exceed the value at which the bomb has been discovered. To reduce the effects of the explosion, the aircraft should fly as long as possible with approximately 1 PSI differential pressure, to help the blast go outwards. 1 PSI differential pressure corresponds to a 2 500 ft difference between the aircraft and the cabin altitude. These conditions are achieved by using the manual pressure control. PROCEDURES The following procedure assumes that it is initiated during climb or cruise: First, maintain the cabin altitude. While maintaining the cabin altitude, descend the aircraft to the cabin altitude + 2 500 ft and maintain ΔP at 1 PSI. During further steps of descent, maintain ΔP at 1 PSI. For landing, reduce the differential pressure to zero, until the final approach. If flight conditions are different, the crew should adapt the procedure, bearing in mind the above-mentioned principles (background paragraph). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.02F 01 DEC 14 BOMB ON BOARD (Cont'd) AIRCRAFT (if climbing).......................................................................LEVEL OFF CABIN PRESS MODE SEL............................................................................MAN CAB ALT................................................................................................MAINTAIN CABIN CREW............................................................................................NOTIFY ATC/COMPANY OPERATIONS................................................................NOTIFY FUEL RESERVES............................................................................. DETERMINE Keep in mind that when flying at cabin altitude + 2 500 ft, the fuel consumption in CONF 1, with landing gear down, will be about 2.1 times that consumed in clean configuration. NEXT SUITABLE AIRPORT..............................................................DETERMINE FCU SPEED SELECTION KNOB..............................................PULL AND TURN Select the most appropriate speed, taking into account the time to destination, the fuel consumption and the fact that low speed could reduce the consequences of possible structural damage, if the bomb explodes. DESCENT TO CAB ALT + 2 500 ft or MEA or minimum obstacle clearance altitude ................................................................................................................. INITIATE AVOID SHARP MANEUVERS CAB ALT................................................................................................MAINTAIN When at CABALT + 2500 ft: 1 PSI ΔP...........................................................................................MAINTAIN GALLEY/PAX SYS..................................................................................... OFF FLAPS (fuel permitting)..................................................... AT LEAST CONF 1 For landing, use normal configuration. LANDING GEAR (fuel permitting, except for flight over water)..............DOWN For any other steps of descent: 1 PSI ΔP...........................................................................................MAINTAIN During approach: CABIN PRESS MODE SEL.................................................................... AUTO When the aircraft on ground and stopped in a remote area (if possible): If Evacuation required: EVACUATION................................................................................INITIATE ALL BATs.............................................................................................. OFF If Evacuation not required: CABIN CREW and PASSENGERS (PA)........................................ NOTIFY CABIN PROCEDURES If a suspect device is found in the cabin: WARNING Do not cut or disconnect any wires and do not open or attempt to gain entry to internal components of a closed or concealed suspect device. Any attempt may result in an explosion. Booby-trapped closed devices have been used on aircraft in the past. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02G 01 DEC 14 BOMB ON BOARD (Cont'd) WARNING Alternate locations must not be used without consulting with an aviation explosives security specialist. Never take a suspect device to the flight deck. CAUTION The least risk bomb location for the aircraft structure and systems is center of the RH aft cabin door. EOD PERSONNEL ON BOARD...................................................................CHECK Announce: “Is there any EOD personnel on board ?”. By using the initials, only persons familiar with EOD (Explosive Ordnance Disposal) will be made aware of the problem. DO NOT OPEN THE BOMB DO NOT CUT BOMB’S WIRES SECURE BOMB AGAINST SLIPPING PROTECT BOMB AGAINST SHOCKS Secure in the attitude found and do not lift before having checked for an anti-lift ignition device. PASSENGERS..............................................................LEAD AWAY FROM BOMB Move passengers at least 4 seat rows away from the bomb location. On full flights, it may be necessary to double up passengers to achieve standoff from the suspect device. Passengers near the bomb should protect their heads with pillows, blankets. All passengers must remain seated with seatbelts on and, if possible, head below the top of the head rest. Seat backs and tray tables must be in their full upright position. Service items may need to be collected in order to secure tray tables. CREW REST AREAS.............................................................................EVACUATE For aircraft equipped with crew rest areas (FCRC, LDMCR, BCRC). PORTABLE ELECTRONIC DEVICES................................................ SWITCH OFF The cabin crews must command passengers to switch off all portable electronic devices. BOMB.....................................................................CHECK NO ANTI-LIFT DEVICE To check for an anti-lift switch or lever, slide a string or stiff card (such as the emergency information card) under the bomb, without disturbing the bomb. If the string or card cannot be slipped under the bomb, it may indicate that an anti-lift switch or lever is present and that the bomb cannot be moved. If a card is used and can be slid under the bomb, leave it under the bomb and move together with the bomb. If it is not possible to move the bomb, then it should be surrounded with a single thin sheet of plastic (e. g. trash bag), then with wetted materials, and other blast attenuation materials such as seat cushions and soft carry-on baggage. Move personnel as far away from the bomb location as possible. EMERGENCY EQUIPMENT................................................. REMOVE AND STOW Emergency equipment (PBE, fire extinguisher, ...) located close to the LRBL must be removed and stowed in alternate location. GALLEY/IFE POWER.........................................................................................OFF All galley and IFE equipment located close to the LRBL must be switched off. If the bomb can be moved: RH AFT CABIN DOOR SLIDE............................................................... DISARM TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02H 01 DEC 14 BOMB ON BOARD (Cont'd) LEAST RISK BOMB LOCATION (LRBL)............................................ PREPARE Build up a platform of solid baggage against the door up to about 25 cm (10 in) below the middle of the door. On top of this, build up at least 25 cm (10 in) of wetted material such as blankets and pillows. Place a single thin sheet of plastic (e. g. trash bag) on top of the wetted materials. This prevents any possible short circuit. CAUTION Do not omit the plastic sheets, as the suspect device could get wet and possibly short circuit electronic components causing inadvertent device activation. BOMB INDICATION LINE................................................................... POSITION Note: A bomb location indicator line is a 6 ft to 8 ft (1.8 m to 2.4 m) line (e.g. neckties, headset cord, or belts connected together) preferably of constrating color, that helps the responding bomb squad find the precise location of the suspect device within the LRBL stack once constructed. Position the bomb indication line from the location on the platform where you will place the suspect device, EXTENDING outward into the aisle. BOMB........................................................................................ MOVE TO LRBL Carefully carry in the attitude found and place on top of the wetted materials in the same attitude and as close to the door structure as possible. CAUTION Ensure that the suspect device, when placed on the stack against the door, is above the slide pack but not against the door handle, and if possible, avoid placement in the view port. LEAST RISK BOMB LOCATION (LRBL)..........................................COMPLETE Place an additional single thin sheet of plastic over the bomb. CAUTION Do not omit the plastic sheets, as the suspect device could get wet and possibly short circuit electronic components causing inadvertent device activation. Build up at 25 cm (10 in) of wetted material around the sides and on top of the bomb. DO NOT PLACE ANYTHING BETWEEN THE BOMB AND THE DOOR, AND MINIMIZE AIRSPACE AROUND THE BOMB. The idea is to build up a protective surrounding of the bomb so that the explosive force is directed in the only unprotected area into the door structure. Fill the area around the bomb with seat cushions and other soft materials such as hand luggage (saturated with water or any other nonflammable liquid) up to the cabin ceiling, compressing as much as possible. Secure the LRBL stack in place using belt, ties or other appropriate materials. The more material stacked around the bomb, the less the damage will be. USE ONLY SOFT MATERIAL. AVOID USING MATERIALS CONTAINING ANY INFLAMMABLE LIQUID AND ANY METAL OBJECTS WHICH COULD BECOME DANGEROUS PROJECTILES. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02I 01 DEC 14 BOMB ON BOARD (Cont'd) LRBL STACK PASSENGERS.............................................................................MOVE/ADVISE Move passengers at least 4 seat rows away from the least risk bomb location (RH aft cabin door). On full flights, it may be necessary to double up passengers to achieve standoff from the suspect device. Passengers near the bomb should protect their heads with pillows, blankets. All passengers must remain seated with seatbelts on and, if possible, head below the top of the head rest. Seat backs and tray tables must be in their full upright position. CABIN CREW............................................................ NOTIFY COCKPIT CREW Cabin crew notify the flight crew that the bomb is secured at the LRBL. EVACUATION/DISEMBARKATION.....................................................EXECUTE Evacuate through normal and emergency exits on the opposite side of the "bomb" location. Do not use the door just opposite the "bomb". Use all available airport facilities to disembark without delay. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.03A 01 DEC 14 DITCHING Ident.: ABN-80-00010583.0007001 / 01 DEC 14 Applicable to: MSN 0232-0472 This procedure applies when engines are running. If engines are not running, Refer to QRH ABN-70 ENG ALL ENG FLAMEOUT - FUEL REMAINING - DITCHING or Refer to QRH ABN-70 ENG ALL ENG FLAMEOUT - NO FUEL REMAINING – DITCHING which has been amended to include the ditching procedure, when the engines are not running. PREPARATION ATC/TRANSPONDER (if available)................................... NOTIFY/SELECT A7700 Notify ATC of the nature of emergency and state intentions. Select transponder code A7700 or transmit the distress message on: (VHF) 121.5 MHz or (HF) 2 182 kHz or 8 364 kHz. CABIN and COCKPIT...............................................................................PREPARE ‐ Loose equipment secured. ‐ Survival equipment prepared. ‐ Belts and shoulder harnesses locked. JETTISON.............................................................................................................ON GPWS SYS.........................................................................................................OFF GPWS TERR...................................................................................................... OFF SIGNS...................................................................................................................ON EMER EXIT LT.....................................................................................................ON COMMERCIAL....................................................................................................OFF LDG ELEV.............................................................................................. SELECT 00 BARO.................................................................................................................. SET Omit the normal approach and landing checklist. CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF APPROACH L/G lever............................................................................................................... UP SLATS and FLAPS.................................................................................MAX AVAIL JETTISON...........................................................................................................OFF AT 2 000 FT AGL CAB PRESS MODE SEL...................................................................CHECK AUTO BLEED (ENGs and APU)................................................................................... OFF CABIN................................................................................NOTIFY FOR DITCHING DITCHING pushbutton......................................................................................... ON Prefer ditching parallel to the swell. If that causes a strong crosswind, ditch into the wind. In all cases, touch down with a pitch attitude of approximately 11 °. Minimize aircraft vertical speed. AT 500 FT AGL BRACE FOR IMPACT.................................................................................. ORDER AT TOUCHDOWN ENG MASTERS..................................................................................................OFF APU MASTER SWITCH.....................................................................................OFF AFTER DITCHING ATC (VHF 1).................................................................................................NOTIFY FIRE pushbutton (ENG and APU)...................................................................PUSH TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.03B 01 DEC 14 DITCHING (Cont'd) AGENTS (ENG and APU)..............................................................................DISCH EVACUATION............................................................................................. INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ELT..............................................................................................CHECK EMITTING If not, switch on the transmitter. DITCHING Ident.: ABN-80-00010583.0019001 / 01 DEC 14 Applicable to: MSN 0700-1118 This procedure applies when engines are running. If engines are not running, Refer to QRH ABN-70 ENG ALL ENG FLAMEOUT - FUEL REMAINING - DITCHING or Refer to QRH ABN-70 ENG ALL ENG FLAMEOUT - NO FUEL REMAINING – DITCHING which has been amended to include the ditching procedure, when the engines are not running. PREPARATION ATC/TRANSPONDER (if available)................................... NOTIFY/SELECT A7700 Notify ATC of the nature of emergency and state intentions. Select transponder code A7700 or transmit the distress message on: (VHF) 121.5 MHz or (HF) 2 182 kHz or 8 364 kHz. CABIN and COCKPIT...............................................................................PREPARE ‐ Loose equipment secured. ‐ Survival equipment prepared. ‐ Belts and shoulder harnesses locked. JETTISON.............................................................................................................ON GPWS SYS.........................................................................................................OFF GPWS TERR...................................................................................................... OFF SIGNS...................................................................................................................ON EMER EXIT LT.....................................................................................................ON COMMERCIAL....................................................................................................OFF LDG ELEV.............................................................................................. SELECT 00 BARO.................................................................................................................. SET Omit the normal approach and landing checklist. CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF APPROACH L/G lever............................................................................................................... UP SLATS and FLAPS.................................................................................MAX AVAIL JETTISON...........................................................................................................OFF AT 2 000 FT AGL CAB PRESS MODE SEL...................................................................CHECK AUTO BLEED (ENGs and APU)................................................................................... OFF CABIN................................................................................NOTIFY FOR DITCHING TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.03C 01 DEC 14 DITCHING (Cont'd) DITCHING pushbutton......................................................................................... ON Prefer ditching parallel to the swell. If that causes a strong crosswind, ditch into the wind. In all cases, touch down with a pitch attitude of approximately 11 °. Minimize aircraft vertical speed. AT 500 FT AGL BRACE FOR IMPACT.................................................................................. ORDER AT TOUCHDOWN ENG MASTERS..................................................................................................OFF APU MASTER SWITCH.....................................................................................OFF AFTER DITCHING ATC (VHF 1).................................................................................................NOTIFY FIRE pushbutton (ENG and APU)...................................................................PUSH AGENTS (ENG and APU)..............................................................................DISCH EVACUATION............................................................................................. INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs............................................................................................................OFF ELT..............................................................................................CHECK EMITTING If not, switch on the transmitter. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.04A 01 DEC 14 FORCED LANDING Ident.: ABN-80-00010584.0029001 / 07 MAY 13 Applicable to: MSN 0232-0472 This procedure is applicable if the engines are running. If the engines are not running, Refer to the QRH ABN 70 ENG ALL ENG FLAMEOUT - FUEL REMAINING procedure or Refer to the QRH ABN 70 ENG ALL ENG FLAMEOUT - NO FUEL REMAINING procedure: It provides the applicable forced landing procedure if the engines are not running. PREPARATION ATC/TRANSPONDER (if available)................................... NOTIFY/SELECT A7700 Notify ATC of the nature of emergency and state intentions. Select transponder code A7700, or transmit the distress message on: (VHF) 121.5 MHz or (HF) 2 182 kHz or 8 364 kHz. CABIN and COCKPIT...............................................................................PREPARE ‐ Loose equipment secured ‐ Survival equipment prepared ‐ Belts and shoulder harnesses locked. JETTISON.............................................................................................................ON GPWS SYS ....................................................................................................... OFF GPWS TERR...................................................................................................... OFF SIGNS...................................................................................................................ON EMER EXIT LT.....................................................................................................ON COMMERCIAL....................................................................................................OFF LDG ELEV.......................................................................................................... SET BARO.................................................................................................................. SET Omit the normal approach and landing checklist. CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF APPROACH RAM AIR...............................................................................................................ON L/G lever......................................................................................................... DOWN SLATS and FLAPS.................................................................................MAX AVAIL GND SPLR.........................................................................................................ARM JETTISON...........................................................................................................OFF MAX BRK PR............................................................................................. 1000 PSI AT 2 000 FT AGL CABIN................................................................................. NOTIFY FOR LANDING AT 500 FT AGL BRACE FOR IMPACT.................................................................................. ORDER AT TOUCHDOWN ENG MASTERS..................................................................................................OFF APU MASTER SW............................................................................................. OFF BRAKES ON ACCU ONLY AFTER LANDING When the aircraft has stopped : PARKING BRK................................................................................................ON ATC (VHF 1)........................................................................................... NOTIFY FIRE pushbutton (ENG and APU)..............................................................PUSH TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.04B 01 DEC 14 FORCED LANDING (Cont'd) AGENTS (ENG and APU).........................................................................DISCH If Evacuation required : EVACUATION...................................................................................INITIATE ELT................................................................................... CHECK EMITTING If not, switch on the transmitter. If Evacuation not required : CABIN CREW and PASSENGERS (PA)........................................... NOTIFY FORCED LANDING Ident.: ABN-80-00010584.0034001 / 07 MAY 13 Applicable to: MSN 0700-1118 This procedure is applicable if the engines are running. If the engines are not running, Refer to the QRH ABN 70 ENG ALL ENG FLAMEOUT - FUEL REMAINING procedure or Refer to the QRH ABN 70 ENG ALL ENG FLAMEOUT - NO FUEL REMAINING procedure: It provides the applicable forced landing procedure if the engines are not running. PREPARATION ATC/TRANSPONDER (if available)................................... NOTIFY/SELECT A7700 Notify ATC of the nature of emergency and state intentions. Select transponder code A7700, or transmit the distress message on: (VHF) 121.5 MHz or (HF) 2 182 kHz or 8 364 kHz. CABIN and COCKPIT...............................................................................PREPARE ‐ Loose equipment secured ‐ Survival equipment prepared ‐ Belts and shoulder harnesses locked. JETTISON.............................................................................................................ON GPWS SYS ....................................................................................................... OFF GPWS TERR...................................................................................................... OFF SIGNS...................................................................................................................ON EMER EXIT LT.....................................................................................................ON COMMERCIAL....................................................................................................OFF LDG ELEV.......................................................................................................... SET BARO.................................................................................................................. SET Omit the normal approach and landing checklist. CREW MASKS/OXY SUPPLY (below FL 100)..................................................OFF APPROACH RAM AIR...............................................................................................................ON L/G lever......................................................................................................... DOWN SLATS and FLAPS.................................................................................MAX AVAIL GND SPLR.........................................................................................................ARM JETTISON...........................................................................................................OFF MAX BRK PR............................................................................................. 1000 PSI AT 2 000 FT AGL CABIN................................................................................. NOTIFY FOR LANDING TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.04C 01 DEC 14 FORCED LANDING (Cont'd) AT 500 FT AGL BRACE FOR IMPACT.................................................................................. ORDER AT TOUCHDOWN ENG MASTERS..................................................................................................OFF APU MASTER SW............................................................................................. OFF BRAKES ON ACCU ONLY AFTER LANDING When the aircraft has stopped : PARKING BRK................................................................................................ON ATC (VHF 1)........................................................................................... NOTIFY FIRE pushbutton (ENG and APU)..............................................................PUSH AGENTS (ENG and APU).........................................................................DISCH If Evacuation required : EVACUATION...................................................................................INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs................................................................................................. OFF ELT................................................................................... CHECK EMITTING If not, switch on the transmitter. If Evacuation not required : CABIN CREW and PASSENGERS (PA)........................................... NOTIFY TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.05A 01 DEC 14 EMER DESCENT Ident.: ABN-80-00010585.0001001 / 03 DEC 13 Applicable to: ALL IMMEDIATE ACTIONS CREW OXYGEN MASKS.................................................................................... ON EMER DESCENT......................................................................... ANNOUNCE (PA) The flight crew must inform the cabin of emergency descent on the PA system. SIGNS...................................................................................................................ON EMER DESCENT........................................................................................INITIATE The recommendation is to descend with the AP engaged: ‐ Turn the ALT knob and pull ‐ Turn the HDG/TRK knob and pull ‐ Adjust the target SPD/MACH. THRUST.............................................................................................................IDLE ‐ If autothrust is engaged, check that THR IDLE appears on the FMA ‐ If autothrust is not engaged, retard the thrust levers. SPD BRK.......................................................................................................... FULL WHEN DESCENT ESTABLISHED EMER DESCENT FL 100, or minimum allowable altitude. SPEED.....................................................................................MAX/APPROPRIATE CAUTION Descend at the maximum appropriate speed. If structural damage is suspected, use the flight controls with care and reduce speed as appropriate. Landing gear may be extended below 21 000 ft. In such a case, speed must be reduced to VLO/VLE. ENG START SEL................................................................................................IGN ATC............................................................................................................... NOTIFY Notify ATC of the nature of the emergency, and state intention. If not in contact with ATC, transmit a distress message on one of the following frequencies: (VHF) 121.5 MHz, or (HF) 2 182 kHz, or 8 364 kHz. ATC XPDR 7700.....................................................................................CONSIDER Squawk 7700 unless otherwise specified by ATC. To save oxygen, set the oxygen diluter selector to the N position. If the oxygen diluter selector remains at 100 %, the quantity of oxygen may not be sufficient for the entire emergency descent profile. MAX FL....................................................................................................... 100/MEA If CAB ALT > 14 000 ft: CAB OXY MASKS................................................................................. MAN ON This action confirms that the passenger oxygen masks are released. Note: Notify the cabin crew, when the aircraft reaches a safe flight level, and when cabin oxygen in no more necessary. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.06A 01 DEC 14 OVERSPEED RECOVERY Ident.: ABN-80-00014729.0001001 / 16 APR 14 Applicable to: ALL As soon as the speed exceeds VMO/MMO, apply the following actions: AP : KEEP ON SPEED BRAKE LEVER............................................................................... AS RQRD Note: The use of speed brakes results in a reduction of the speed envelope. THRUST REDUCTION................................................................................ MONITOR If the A/THR is OFF: ALL THR LEVERS...........................................................................................IDLE If the AP automatically disengages: HIGH SPEED PROTECTION : ACTIVE IN NORM LAW The activation of the high speed protection results in an automatic pitch up in order to reduce the speed. While the speed is above VMO/MMO: SPEED BRAKE LEVER : AS RQRD PITCH ATT.................................................... ADJUST SMOOTHLY AS RQRD When the speed is below VMO/MMO with a sufficient margin to VMO/MMO: SPEED BRAKE LEVER..........................................................................AS RQRD If the A/THR is OFF: ALL THR LEVERS...................................................................... MAN ADJUST If the AP is OFF: FLIGHT PATH............................................................. RECOVER SMOOTHLY In the case of severe turbulence: Refer to QRH OPS - Severe Turbulence TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.07A 01 DEC 14 OVERWEIGHT LANDING Ident.: ABN-80-00010586.0029001 / 08 FEB 13 Applicable to: MSN 0466-0700 Automatic landing is certified up to the Maximum Landing Weight (MLW). Autoland flight tests have, however, been successful up to 229 t. Depending on the situation (e.g. emergency or other) and provided that the runway is approved for automatic landing, the flight crew can decide to perform an autoland up to 229 t. JETTISON ............................................................................................CONSIDER LDG CONF.......................................................................................... AS REQUIRED Use the ECAM flap setting, if required for abnormal operations. In all other cases: ‐ FULL is preferred for optimized landing performance ‐ If the aircraft weight is above the maximum weight for go-around (given in the table below), use FLAP 3 for landing. In all cases, if the landing configuration is different from FLAP FULL, use 1 + F for go-around. LDG DIST.........................................................................................................CHECK PACK 1 and 2.......................................................................OFF or supplied by APU Selecting packs OFF (or supplied from APU) will increase the maximum thrust available from the engines, in the event of a go-around. In the final stages of approach: TARGET SPEED.............................................................................................. VLS Reduce speed to reach VLS at runway threshold. Touch down as smoothly as possible (Maximum V/S at touchdown 360 ft/min). At main landing gear touchdown: REVERSE THRUST........................................................... USE MAX AVAILABLE After nosewheel touchdown: BRAKES..........................................................................APPLY AS NECESSARY Maximum braking may be used after nosewheel touchdown. But, if landing distance permits, delay or reduce braking to take full benefit of the available runway length. Landing complete: BRAKE FANS.................................................................................. ON if available Be prepared for tire deflation, if temperatures exceed 800 °C. MAXIMUM WEIGHT FOR GO AROUND IN CONF 3 (1000 KG) OAT (°C) AIRPORT ELEVATION (FT) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000 10 243 232 217 203 188 173 159 145 15 243 231 217 202 186 169 154 140 20 243 231 217 200 181 164 148 135 25 242 231 214 194 175 157 143 132 30 240 222 206 187 168 151 138 35 230 213 197 179 161 40 220 204 189 172 45 210 194 180 50 200 184 55 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.07B 01 DEC 14 OVERWEIGHT LANDING Ident.: ABN-80-00010586.0020001 / 08 FEB 13 Applicable to: MSN 0232-0361, 0968-1118 Automatic landing is certified up to the Maximum Landing Weight (MLW). Autoland flight tests have, however, been successful up to 229 t. Depending on the situation (e.g. emergency or other) and provided that the runway is approved for automatic landing, the flight crew can decide to perform an autoland up to 229 t. JETTISON ............................................................................................CONSIDER LDG CONF.......................................................................................... AS REQUIRED Use the ECAM flap setting, if required for abnormal operations. In all other cases: ‐ FULL is preferred for optimized landing performance ‐ If the aircraft weight is above the maximum weight for go-around (given in the table below), use FLAP 3 for landing. In all cases, if the landing configuration is different from FLAP FULL, use 1 + F for go-around. LDG DIST.........................................................................................................CHECK PACK 1 and 2.......................................................................OFF or supplied by APU Selecting packs OFF (or supplied from APU) will increase the maximum thrust available from the engines, in the event of a go-around. In the final stages of approach: TARGET SPEED.............................................................................................. VLS Reduce speed to reach VLS at runway threshold. Touch down as smoothly as possible (Maximum V/S at touchdown 360 ft/min). At main landing gear touchdown: REVERSE THRUST........................................................... USE MAX AVAILABLE After nosewheel touchdown: BRAKES..........................................................................APPLY AS NECESSARY Maximum braking may be used after nosewheel touchdown. But, if landing distance permits, delay or reduce braking to take full benefit of the available runway length. Landing complete: BRAKE FANS ............................................................................ ON if available Be prepared for tire deflation, if temperatures exceed 800 °C. MAXIMUM WEIGHT FOR GO AROUND IN CONF 3 (1000 KG) OAT (°C) AIRPORT ELEVATION (FT) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000 10 239 231 219 205 191 175 160 147 15 239 231 219 205 190 173 158 145 20 239 231 219 203 187 171 155 142 25 239 231 216 200 183 166 152 140 30 237 225 211 193 176 161 148 35 230 219 201 185 170 40 222 208 191 176 45 211 195 181 50 196 181 55 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.08A 01 DEC 14 STALL RECOVERY Ident.: ABN-80-00013762.0001001 / 08 FEB 13 Applicable to: ALL As soon as any stall indication (could be aural warning, buffet...) is recognized, apply the immediate actions: NOSE DOWN PITCH CONTROL..................................................................... APPLY This will reduce angle of attack Note: In case of lack of pitch down authority, reducing thrust may be necessary. BANK....................................................................................................WINGS LEVEL When out of stall (no longer stall indications) : THRUST.....................................................INCREASE SMOOTHLY AS NEEDED Note: In case of one engine inoperative, progressively compensate the thrust asymmetry with rudder. SPEEDBRAKES...................................................................CHECK RETRACTED FLIGHT PATH.................................................................. RECOVER SMOOTHLY If in clean configuration and below 20 000 ft : FLAP 1..................................................................................................SELECT Note: If a risk of ground contact exists, once clearly out of stall (no longer stall indications), establish smoothly a positive climb gradient. STALL WARNING AT LIFTOFF Ident.: ABN-80-00013763.0001001 / 08 FEB 13 Applicable to: ALL Spurious stall warning may sound in NORMAL law, if an angle of attack probe is damaged. In this case, apply immediately the following actions: THRUST..............................................................................................................TOGA AT THE SAME TIME: PITCH ATTITUDE..................................................................................................15 ° BANK....................................................................................................WINGS LEVEL Note: When a safe flight path and speed are achieved and maintained, if stall warning continues, consider it as spurious. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.09A 01 DEC 14 TAILSTRIKE Ident.: ABN-80-00010587.0001001 / 08 FEB 13 Applicable to: ALL In the event of a tailstrike, apply the following procedure: LAND ASAP MAX FL..................................................................................................... 100 or MSA Limit to FL 100 or to MSA to minimize structural stress. Return to the airport for damage assessment. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.10A 01 DEC 14 VOLCANIC ASH ENCOUNTER Ident.: ABN-80-00010588.0001001 / 01 DEC 14 Applicable to: ALL If the aircraft enters a volcanic ash cloud: 180 ° TURN.............................................................................................. INITIATE ATC.............................................................................................................NOTIFY A/THR............................................................................................................... OFF THRUST (conditions permitting)...............................................................REDUCE CREW OXYGEN MASKS............................................................ON/100 %/EMER CABIN CREW.............................................................................................NOTIFY PASSENGER OXYGEN..........................................................................AS RQRD ENG ANTI ICE................................................................................................... ON WING ANTI ICE................................................................................................. ON PACK FLOW........................................................................................................ HI Note: If CARGO VENTILATION system is installed, it is recommended to switch off the CARGO ISOL VALVES, to prevent a cargo smoke warning being triggered. ENGINE PARAMETERS........................................................................ MONITOR AIRSPEED INDICATIONS......................................................................MONITOR If airspeed is unreliable or lost, Refer to QRH ABN-34 UNRELIABLE SPEED INDICATION procedure. Note: If all engines flame out and speed indications are lost, Refer to QRH ABN-70 ALL ENG FLAMEOUT procedure to get the required pitch attitude for the optimum relight speed. In case of engine failure, switch off the wing anti ice before engine restart. Note: If visibility is insufficient for approach due to windshield/window damage, consider AUTOLAND. If AUTOLAND is not available, consider opening the sliding window on the PF’s side (maximum speed 230 kt), after cabin depressurization. To manually depressurize the cabin: CAB PRESS MODE selector ........................................................... MAN MAN V/S CTL ............................................................................FULL UP Due to the increased noise level, pay particular attention to visual warnings. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.11A 01 DEC 14 WINDSHEAR Ident.: ABN-80-00010589.0001001 / 10 JUN 13 Applicable to: ALL A red flag “WINDSHEAR” message is displayed on each PFD, associated with an aural “WINDSHEAR” message, repeated three times. If windshear is detected, either by the system or by pilot observation, apply the following recovery technique: At takeoff: If before V1: The takeoff should only be rejected if significant airspeed variations occur below indicated V1, and the pilot decides that there is sufficient runway remaining to stop the airplane. If after V1: THR LEVERS...........................................................................................TOGA REACHING VR.................................................................................... ROTATE SRS ORDERS.....................................................................................FOLLOW If necessary, the flight crew may pull the sidestick fully back Note: If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °. Then if necessary, to prevent a loss in altitude, increase the pitch attitude. Airborne initial climb or landing: THR LEVERS AT TOGA..........................................................SET OR CONFIRM AP (if engaged)....................................................................................... KEEP ON SRS ORDERS..........................................................................................FOLLOW If necessary, the flight crew may pull the sidestick fully back Note: 1. Autopilot disengages if the angle of attack values goes above α prot. 2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °. Then if necessary, to prevent a loss in altitude, increase the pitch attitude. DO NOT CHANGE CONFIGURATION (SLATS/FLAPS, GEAR) UNTIL OUT OF WINDSHEAR. CLOSELY MONITOR FLIGHT PATH AND SPEED. RECOVER SMOOTHLY TO NORMAL CLIMB OUT OF WINDSHEAR. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.12A 01 DEC 14 WINDSHEAR AHEAD Ident.: ABN-80-00010590.0002001 / 28 FEB 14 Applicable to: ALL The “W/S AHEAD” message is displayed on each PFD. The color of the message depends on the severity and location of the windshear. Note: When a predictive windshear alert (″WINDSHEAR AHEAD″ or ″GO AROUND WINDSHEAR AHEAD″) is triggered, if the flight crew makes a positive verification that no hazard exists, then the alert may be disregarded, as long as: ‐ There are no other signs of possible windshear conditions, and ‐ The reactive windshear system is operational. Known cases of spurious predictive windshear alerts have been reported at some airports, during either takeoff or landing, due to the specific obstacle environment. However, always rely on any reactive windshear (″WINDSHEAR″). W/S AHEAD RED Takeoff: Associated with a synthetic aural voice: “WINDSHEAR AHEAD, WINDSHEAR AHEAD”. Before takeoff: Delay takeoff, or select the most favorable runway. During takeoff run: Reject takeoff. Note: The predictive windshear alerts are inhibited above 100 kt, until 50 ft. When airborne: THR LEVERS........................................................................................TOGA As usual, the slat/flap configuration can be changed, provided the windshear is not entered. AP (if engaged)............................................................................... KEEP ON SRS ORDERS..................................................................................FOLLOW If necessary, the flight crew may pull the sidestick fully back. Note: 1. Autopilot disengages if the angle of attack values goes above α prot. 2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 °. Then if necessary, to prevent a loss in altitude, increase the pitch attitude. Landing: Associated with a synthetic aural voice: “GO AROUND, WINDSHEAR AHEAD”. GO AROUND......................................................................................PERFORM AP (if engaged).................................................................................... KEEP ON If necessary, the flight crew may pull the sidestick fully back. Note: 1. Autopilot disengages if the angle of attack values goes above α prot. 2. If the FD bars are not displayed, move toward an initial pitch attitude of 17.5 ° . Then, if necessary, to prevent a loss in altitude, increase the pitch attitude. W/S AHEAD AMBER Apply precautionary measures, as indicated below: Before takeoff: Delay Takeoff until conditions are improved. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.12B 01 DEC 14 WINDSHEAR AHEAD (Cont'd) "Assess conditions for a safe Takeoff by": • Using observations and experience, • Checking weather conditions. Select the most favorable runway (considering location of the likely windshear). Use the weather radar or the predictive windshear system, before the takeoff run, to ensure a flight path clear of any potential problem areas. Select TOGA thrust. Closely monitor airspeed and airspeed trend during the takeoff run to detect early signs of windshear. During approach: Delay landing or divert to another airport until conditions are more favorable. "Assess conditions for a safe landing by": • Using observations and experience, • Checking weather conditions. Use the weather radar or predictive windshear system. Select the most favorable runway, in conjunction with the most appropriate runway approach aid. Select FLAPS 3. Use managed speed in approach phase. Check both FDs engaged in ILS, GLS ,FPA or V/S Engage autopilot, for more accurate approach and earlier information of beam deviation when ILSor GLS available. Note: ‐ When using the GS mini function, associated with managed speed, the system will carry extra speed in strong wind conditions. ‐ In the case of strong or gusty crosswind greater than 20 kt, Refer to QRH PER-C VAPP Determination without Failure for VAPP determination. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.13A 01 DEC 14 COCKPIT WINDSHIELD / WINDOW ARCING Ident.: ABN-80-00010591.0001001 / 08 FEB 13 Applicable to: ALL Affected WINDSHIELD/WINDOW WHC reset button..........................................PULL Pull the Window Heat Computer reset button that is located on the affected side, in case of : ‐ Electrical arcing of the cockpit windshield/window, or ‐ Burning smell or smoke identified as coming from the bottom left corner of CAPT windshield or bottom right corner of the F/O windshield. • WINDSHIELD/WINDOW LEFT SIDE - WHC 1 (261 VU) • WINDSHIELD/WINDOW RIGHT SIDE - WHC 2 (262 VU). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE 80.14A ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 01 DEC 14 COCKPIT WINDSHIELD / WINDOW CRACKED Ident.: ABN-80-00010893.0001001 / 08 FEB 13 Applicable to: ALL DIAGNOSIS OF INNER PLY......................................................................PERFORM Touch the crack(s) with a pen (or carefully with fingernail) to determine if there is a crack on the cockpit side. If no crack on cockpit side: No limitation The inner ply is not affected. Therefore, the window/windshield is still able to sustain the differential pressure up to the maximum flight level. If cracks on cockpit side: MAX FL..................................................................................................... 230/MEA The inner ply is affected. The flight crew is not able to easily determine if other plies are affected. Descend to FL 230/MEA and reduce differential pressure to 5 PSI. Note: The maximum flight level is restricted to FL 230/MEA to obtain ΔP 5 PSI, without resulting in an excessive cabin altitude and an EXCESS CAB ALT warning. The following procedure enables maintaining ΔP 5 PSI in manual cabin pressure mode: CAB PRESS MODE SEL................................................................................ MAN MAN V/S CTL......................................................................................... AS RQRD Disregard the CAB ALT TARGET table displayed on the ECAM and set the cabin altitude according to the table below: ΔP = 5 PSI FL 100 150 200 230 CABIN ALTITUDE 0 3 000 6 000 8 000 When starting the descent for approach: CAB PRESS MODE SEL......................................................................... AUTO Note: If visibility is insufficient for approach due to windshield/window damage, consider AUTOLAND. If AUTOLAND is not available, consider opening the sliding window (maximum speed 230 kt) on the PF’s side, after cabin depressurization. To manually depressurize the cabin: CAB PRESS MODE SEL....................................................................... MAN MAN V/S CTL.................................................................................. FULL UP Due to the increased noise level, pay particular attention to visual warnings. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.15A 01 DEC 14 ECAM ADVISORY CONDITIONS Applicable to: MSN 0232-0361, 0968-1118 SYSTEM CONDITIONS RECOMMENDED ACTION Ident.: ABN-80-A-00010592.0001001 / 08 FEB 13 CAB VERT SPD V/S > 1 800 ft/min or V/S < -1 800 ft/min CAB ALT CAB PRESS ALT ≥ 8 800 ft COND CPC changeover is recommended, MODE SEL: MAN AFTER 3 s, MODE SEL: AUTO MODE SEL: MAN Manual pressure control ΔP ≥ 1.5 PSI in phase 7 LDG ELEV: ADJUST if unsuccessful, MODE SEL: MAN Manual pressure control PACK LO FLOW Pack flow not sufficient to satisfy temperature demand. PACK FLOW: INCREASE Ident.: ABN-80-A-00010594.0001001 / 24 JUN 13 ELEC IDG OIL TEMP T > 151 °C Reduce IDG load, if possible (GALLEY or COMMERCIAL or GEN OFF). If required, restore when temperature has dropped. Restrict use of the generator to a short time, if temperature rises again excessively. Ident.: ABN-80-A-00010595.0002001 / 24 FEB 14 FUEL Difference between L and R wing fuel FUEL MANAGEMENT: CHECK quantities is greater than 3 000 kg (6 614 lb) If a fuel leak is suspected, Refer to QRH ABN-28 FUEL LEAK. Ident.: ABN-80-A-00010596.0006001 / 08 FEB 13 CKPT OXY Pulses Green: When pressure is < 600 PSI OXY/DOOR Amber: When pressure is < 300 PSI If mask is not being used check if it is correctly stowed. PAX OXY 200 < pressure < 1 200 PSI Ident.: ABN-80-A-00010597.0001001 / 08 FEB 13 APU LOW OIL LEVEL The APU may be started and operated for 15 h, if there is no oil leak. EGT high (inhibited during APU start) Ident.: ABN-80-A-00010598.0003001 / 24 FEB 14 ENG OIL TEMP An increase in oil temperature during normal steady-state operation 163 °C < T < 177 °C indicates a system malfunction and should be closely-monitored for After 20 min , advisory is replaced by ECAM other engine malfunction symptoms. caution. The first recommended action is to reduce the thrust to decrease oil The indication turns amber. temp. An increase in oil temperature could be related to the IDG oil cooling system. To reduce oil temperature increase before limits are reached, the following are recommended: Reduce GEN load, or turn off GEN. If the oil temperature continues to rise, mechanically disconnect the IDG. OIL QTY < 3 quarts If oil quantity is low at high power setting, expect level increase after power reduction. NAC TEMP > 230 °C Monitor engine parameters and crosscheck with other engine. VIBRATION N1 ≥ 5.2 units N2 ≥ 5.6 units Refer to QRH ABN-70 High Engine Vibration. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.15B 01 DEC 14 ECAM ADVISORY CONDITIONS Applicable to: MSN 0466-0700 SYSTEM CONDITIONS RECOMMENDED ACTION Ident.: ABN-80-A-00010592.0001001 / 08 FEB 13 CAB VERT SPD V/S > 1 800 ft/min or V/S < -1 800 ft/min CAB ALT CAB PRESS ALT ≥ 8 800 ft COND CPC changeover is recommended, MODE SEL: MAN AFTER 3 s, MODE SEL: AUTO MODE SEL: MAN Manual pressure control ΔP ≥ 1.5 PSI in phase 7 LDG ELEV: ADJUST if unsuccessful, MODE SEL: MAN Manual pressure control PACK LO FLOW Pack flow not sufficient to satisfy temperature demand. PACK FLOW: INCREASE Ident.: ABN-80-A-00010594.0001001 / 24 JUN 13 ELEC IDG OIL TEMP T > 151 °C Reduce IDG load, if possible (GALLEY or COMMERCIAL or GEN OFF). If required, restore when temperature has dropped. Restrict use of the generator to a short time, if temperature rises again excessively. Ident.: ABN-80-A-00010595.0002001 / 24 FEB 14 FUEL Difference between L and R wing fuel FUEL MANAGEMENT: CHECK quantities is greater than 3 000 kg (6 614 lb) If a fuel leak is suspected, Refer to QRH ABN-28 FUEL LEAK. Ident.: ABN-80-A-00010596.0006001 / 08 FEB 13 CKPT OXY Pulses Green: When pressure is < 600 PSI OXY/DOOR Amber: When pressure is < 300 PSI If mask is not being used check if it is correctly stowed. PAX OXY 200 < pressure < 1 200 PSI Ident.: ABN-80-A-00010597.0001001 / 08 FEB 13 APU LOW OIL LEVEL The APU may be started and operated for 15 h, if there is no oil leak. EGT high (inhibited during APU start) Ident.: ABN-80-A-00010598.0002001 / 24 FEB 14 OIL TEMP 160 °C < T < 175 °C for 15 min An increase in oil temperature during normal steady-state operation indicates a system malfunction and should be closely-monitored for other engine malfunction symptoms. An increase in oil temperature could be related to the IDG oil cooling system. To reduce oil temperature increase before limits are reached, the following are recommended: Reduce GEN load, or turn off GEN. If the oil temperature continues to rise, mechanically disconnect the IDG. OIL QTY < 2 quarts If oil quantity is low at high power setting, expect level increase after power reduction. NAC TEMP > 260 °C Monitor engine parameters and crosscheck with other engine. VIBRATION N1 ≥ 5.7 units N2 ≥ 5.6 units Refer to QRH ABN-70 High Engine Vibration. ENG TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.16A 01 DEC 14 TRIPPED C/B RE - ENGAGEMENT Ident.: ABN-80-00010640.0001001 / 21 MAR 11 Applicable to: ALL TRIPPED C/B REENGAGEMENT In flight, do not reengage a circuit breaker (C/B) that has tripped by itself, unless the Captain judges it necessary to do so for the safe continuation of the flight. This procedure should be adopted only as a last resort, and only one reengagement should be attempted. On ground, do not reengage the C/B of the fuel pump(s) of any tank. For all other C/Bs, if the flight crew coordinates the action with maintenance, the flight crew may reengage a tripped C/B, provided that the cause of the tripped C/B is identified. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.17A 01 DEC 14 COMPUTER RESET - GENERAL Ident.: ABN-80-00010641.0001001 / 14 AUG 12 Applicable to: ALL RESET OF COMPUTERS This table lists the computers that may be reset following abnormal behavior, or a detected fault. Most of the computers’ reset capability is provided on the overhead RESET panel: Those with an asterisk* are reset on the system control panel. To reset a computer: ‐ Set the related normal cockpit control OFF, or pull the corresponding reset pb, ‐ Wait 3 s, if a normal cockpit control is used (unless a different time is indicated), or 1 s if a reset pb is used, ‐ Set the related normal cockpit control ON, or push the corresponding reset pb, ‐ Wait 3 s for the end of the reset. WARNING Do not reset more than one computer at a time, unless instructed to do so. The following table lists the various computers for which manual reset capability is provided: • On the overhead RESET panels, • On the system control panel. For each computer reset, the table lists the effects and/or precautions where applicable ("NIL" indicates no additional effects and/or precautions apply). ‐ A computer reset has to be attempted when: • recommended by an ECAM procedure or • recommended by a paper procedure. ‐ In all other circumstances, where a failure is suspected or detected, there is no specific recommendations as to whether a reset should be performed or not, except those where a reset is specifically forbidden. Manual reset on ground triggers complete power up test. The number of reset attempts is not limited. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330 QUICK REFERENCE HANDBOOK 80.18A 01 DEC 14 COMPUTER RESET TABLE Applicable to: ALL ATA EQUIPMENT REMARKS Ident.: ABN-80-F-00010642.0001001 / 18 NOV 11 PACK CONT ZONE CONT NIL VENT CONT AEVC CPC 21 To force a CPC changeover: ‐ SELECT MAN MODE SEL AFTER 3 s: ‐ SELECT AUTO MODE SEL The inactive CPC may then be reset (check the CAB PRESS SD page ). During the reset phase, the following cabin effects may occur: ‐ cabin lights may come on at full intensity ‐ cabin chimes may sound Ident.: ABN-80-F-00010645.0001001 / 01 DEC 14 FCU ‐ In flight: • When PART FCU is displayed as INOP SYS, do not reset the FCU • When FCU is displayed as INOP SYS, check FCU targets after the reset ‐ On ground: • The flight crew can reset the FCU when either FCU or PART FCU is displayed as INOP SYS • The FCU has to be reconfigured after the reset Note: FMGEC and FM Following a total FCU reset either in flight or on ground, FCU targets are FCU entries (selected modes). FMGEC or FM resets result in onside AP disconnection (if engaged). Resynchronization of both FMs will occur after a reset sequence, with associated messages on the MCDU and ND : ‐ PLEASE WAIT ‐ MAP NOT AVAIL 22 It is recommended to use the FMGEC reset pb , rather than the FM reset pb. Note: MCDU blank or locked Due to electrical transient, MANUAL FMGS RESET procedure may be unsuccessful. If so and on ground, the flight crew may attempt the same procedure with engines not running. ‐ Set MCDU (affected) to OFF ‐ Wait 10 s ‐ Set MCDU (affected) to ON Note: Wait after the message "PLEASE WAIT" disappears before using MCDU. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18B 01 DEC 14 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00016076.0001001 / 01 DEC 14 CIDS In the event of active CIDS reset (usually CIDS 1 when both are operative), a complete power-up test is performed: ‐ In flight, the test lasts about 20 s: • The cabin light comes on at full intensity. If selected, dimming is lost and must be reselected after the test. • PA, CALL, and INTERPHONE functions are interrupted and have to be reselected after the test. • FAP cabin temperature corrections are lost, and have to be reselected after the test. ‐ On ground, the test lasts about 80 s, and also includes: • A sequential cabin loudspeakers’ test (triggers a tone for about 10 s). • The cabin light may flash briefly. Dimming selection is lost (as in flight). Note: 23 After a CIDS reset is performed, the following messages may be displayed temporarily on the ECAM: ‐ SMOKE LAVATORY DET FAULT ‐ SMOKE VIDEO 1(2)(3)(4) DET FAULT ACP/AMU NIL RMP * In case of freezing of one RMP (impossibility to interchange the ACTIVE and STBY radio navigation or communication frequencies,...), all the RMPs have to be reset, one after the other, to recover a normal operation. In order to be reset, RMPs must be switched off at least 5 s by using the ON/OFF selector on the RMP control panels. SATCOM SATCOM may be reset when PAX communication system is lost. The PAX SATCOM system can be reset by switching the PAX SATCOM pushbutton OFF for at least 1 s and then on. Wait 5 min, and then perform the CINS reset (Refer to QRH ABN-80 Computer Reset Table - 46 - Information System). Ident.: ABN-80-F-00010647.0001001 / 24 APR 13 GPCU * 24 GPCU reset may be attempted, if the AVAIL and ON lights do not light up. 1. Press once the affected EXT A(B) pb to reset the functions of GPCU. 2. Check the GPU is connected to the aircraft, then started. 3. Check AVAIL light is ON and press the EXT A(B) pb to connect the GPU. If unsuccessful, check GPU voltage and frequency (bite is available on batteries only). BCL * Use BAT pb to reset the BCL. Do not reset the BCL when ELEC BAT 1(2) FAULT caution is triggered, and BAT OFF selection is requested by the ECAM. Ident.: ABN-80-F-00010648.0001001 / 21 MAR 11 Commercial equipments and galleys 25 On ground When the commercial equipment and/or galley loads have been shed by the ECMU, they can be recovered when more electrical power is available. If COMMERCIAL OFF is displayed on the ELEC SD page: Switch the COMMERCIAL pb OFF then ON. IF GALLEY SHED or GALLEY PARTIALLY SHED is displayed on the ELEC SD page: Switch the GALLEY pb OFF then ON. Do not reset more than one pushbutton at a time. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18C 01 DEC 14 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00010649.0001001 / 17 NOV 11 SDCU Only a simultaneous reset of SDCU 1 and SDCU 2 is authorized. On ground: ‐ Simultaneously pull both SDCU 1 reset pb and SDCU 2 reset pb ‐ Wait 2 min ‐ Simultaneously push both SDCU 1 reset pband SDCU 2 reset pb ‐ Wait 3 min for the system restart to be completed 26 In flight: ‐ Simultaneously pull both SDCU 1 reset pb and SDCU 2 reset pb ‐ Wait 3 s ‐ Simultaneously push both SDCU 1reset pband SDCU 2 reset pb ‐ Wait 15 s for the system restart to be completed Ident.: ABN-80-F-00010650.0002001 / 21 AUG 13 PRIM and SEC * ‐ PRIM/SEC may be reset, except in the following case: • The ELEC DC BUS 2 FAULT caution is present. Note: Do not attempt a reset because this would result in a loss of related PRIM/SEC ‐ If a reset is performed on ground, it must be followed by a flight controls’ check 27 WARNING Do not reset more than one computer at a time. Note: When a PRIM reset is performed on ground, the crew must check the pitch trim position. FCDC NIL Ident.: ABN-80-F-00010651.0003001 / 24 FEB 14 FCMC 28 ‐ If the reset is done before engine start, the ZFW and ZFWCG must be re-entered on the MCDU INIT B page, ‐ If the reset is done after engine start, the actual GW and CG displayed on the MCDU FUEL PRED page are computed by the FE. However, the GW computed by the FE may be less accurate, therefore, when time permits: • If the reset is successful, the actual GW and CG must be re-entered on the MCDU FUEL PRED page, • If the reset is unsuccessful, the flight crew must determine the FOB from the engine start fuel quantity minus the FU quantity indication. In the case of triggering of FUEL ZFW ZFCG DISAGREE, if the ZFW, ZFWCG, ECAM GW are the same as the loadsheet values, but the difference between the ECAM CG and the loadsheet CG is more than 2 %: On ground: ‐ Reinsert the ZFW and ZFCG values. If the ECAM caution is still displayed after reinsertion: • Simultaneously pull FCMC 1 and FCMC 2 reset buttons • Simultaneously push FCMC 1 and FCMC 2 reset buttons. If unsuccessful, on ground: ‐ Simultaneously pull FCMC 1, FCMC 2, FMGEC 1 and FMGEC 2 reset buttons ‐ Simultaneously push FCMC 1, FCMC 2, FMGEC 1 and FMGEC 2 reset buttons. Refer to QRH ABN-80 Computer Reset Table - 22 - Auto Flight for additional information regarding the FMGEC resets. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18D 01 DEC 14 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00010652.0001001 / 21 MAR 11 30 PHC WHC Associated heating is interrupted, when the reset pb is pulled. Ident.: ABN-80-F-00010653.0001001 / 21 MAR 11 31 DU (ECAM, PFD, ND) * If DU reset is unsuccessful, DMC (driving the affected DU) reset may be attempted. DMC EFIS/ECAM displays are lost for 40 s on ground after reset or power-up. FWC NIL SDAC NIL Ident.: TDU / ABN-80-F-00015048.0001001 / 07 OCT 13 BSCU* In flight: Not authorized. On ground and only for the following cases: In case of BRAKES RESIDUAL BRAKING: ‐ STOP aircraft, ‐ Set PARK BRK handle to ON, ‐ Set A/SKID & N/W STRG sw to OFF, ‐ Set A/SKID & N/W STRG sw to ON. In case of WHEEL N/W STRG FAULT: Case A If the three conditions below are fulfilled: ‐ the WHEEL N/W. STRG FAULT alert was triggered just after engine start ‐ the NW STRG DISC memo was displayed before the start of the pushback (before the aircraft starts moving) ‐ the NW STRG DISC memo remained displayed even after the pushback is finished (nosewheel steering selector bypass pin is in the steering position). Apply the below reset procedure. If the ECAM alert disappears after the reset, the flight crew may continue the flight without troubleshooting. 32 Case B In all other cases, including in case of doubt on the above conditions, troubleshooting must be performed before continuing the flight, even if the ECAM alert disappears after the reset. For a return to the gate : ‐ Apply the below reset procedure ‐ The taxi speed must not exceed 10 kt. Reset Procedure: ‐ STOP aircraft, ‐ Set PARK BRK handle to ON, ‐ Confirm that towing bar is disconnected, ‐ Set A/SKID & N/W STRG sw to OFF, ‐ Set A/SKID & N/W STRG sw to ON. Note: LGCIU After any BSCU reset: 1. Check brake efficiency, 2. Check absence of aircraft veering, 3. Record the BSCU reset in the logbook. An LGCIU reset must neither be done during landing gear maneuvers, nor just prior to touchdown. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18E 01 DEC 14 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00014555.0001001 / 27 MAY 13 ENG BLEED ENG BLEED reset is only authorized in the two following cases: ‐ CASE A: AIR ENG 1(2) BLEED FAULT alert ‐ CASE B: AIR ENG 1(2) BLEED NOT CLSD alert Note: Do not attempt more than one reset. CASE A: AIR ENG 1(2) BLEED FAULT alert: On ground or in flight • If the PACK (non-affected side) is operative, and If the Wing Anti-Ice is OFF: ‐ ENG BLEED (affected side).......................................................OFF 36 ▪ If the ENG BLEED (affected side) pb-sw FAULT light is on: ‐ Delay application of the reset until FAULT light extinguishes. ▪ If the ENG BLEED (affected side) pb-sw FAULT light is off: ‐ X BLEED........................................................................AUTO Disregard the AIR ABNORM BLEED CONFIG alert. ‐ PACK (affected side)...........................................................ON ‐ ENG BLEED (affected side)................................................ON ‐ Check that the affected Engine Bleed Valve is open on the BLEED SD page. • If AIR ENG (AFFECTED) BLEED FAULT alert reoccurs, or If Engine Bleed Valve (affected side) not open on the BLEED SD page: - ENG BLEED (affected side).......................................OFF - X BLEED.................................................................OPEN Note: Record the ENG BLEED reset in the logbook (successful or unsuccessful). CASE B: AIR ENG 1(2) BLEED NOT CLSD alert: On ground only ‐ ENG BLEED (affected side).......................................................OFF ▪ If the ENG BLEED (affected side) pb-sw FAULT light is on: ‐ Delay application of the reset until FAULT light extinguishes. ▪ If the ENG BLEED (affected side) pb-sw FAULT light is off: ‐ ENG BLEED (affected side)...............................................ON Note: Record the ENG BLEED reset in the logbook (successful or unsuccessful). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18F 01 DEC 14 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00010655.0001001 / 17 NOV 11 VSC In case all toilets of one or both sides are shut down (on the cabin aft C/B panel): ‐ RESET VACUUM TOILET SYSTEM (blue pb). Repeated use of the blue reset pb is not recommended. If this does not fix the problem, apply the following procedure for both system sides on the cabin aft C/B panel (VACUUM TOILET SYSTEM). Do not apply the following procedure in case of a waste tank overfill. On the cabin aft C/B panel: ‐ PULL C/B SYSTEM (both) and VACUUM GEN (both) (4 C/Bs). ‐ PULL C/B LAVATORY POWER (LH and RH) (8 C/Bs). ‐ PUSH C/B LAVATORY POWER (LH and RH) (8 C/Bs). LH and RH SYSTEM and both VACUUM GEN C/Bs remain pulled. 38 In this configuration: • The waste quantity indication is lost. • The protection against waste tank overfill is lost. • Do not use toilets when the aircraft is below 16 000 ft. • Do not use toilets on ground, during servicing. Ident.: ABN-80-F-00015509.0001001 / 01 DEC 14 ATSU When the ATSU is reset, ADS-C connections are no longer active. The ATC center(s) assumes that the connection is still active because a disconnection message has not been sent to the ATC center(s). Therefore, the ATC center(s) will not attempt to re-establish ADS-C contracts with the aircraft, even after re-notification. ATSU reset, with the ATSU 1 reset sw on 261 VU (overhead panel), should only be attempted, if: ‐ ″INVALID DATA″ is displayed on the DCDU. ‐ Key selection has no effect on the DCDU or any of the MCDU ATSU DATALINK submenus. 46 AINS Use the AINS reset sw on the 262 VU (overhead panel) to reset the AINS. Note: CINS An AINS reset may take up to 20 min If there is a malfunction of the CINS and if the reset by the cabin crew is unsuccessful, the flight crew can attempt to reset the system using the CINS reset button (overhead panel): pull the button then push it. Note: The CINS reset may take up to 10 min. Ident.: ABN-80-F-00010657.0001001 / 21 MAR 11 49 ECB * Reset must only be attempted when APU speed is below 7 % Ident.: ABN-80-F-00010658.0001001 / 21 MAR 11 52 PSCU NIL Ident.: ABN-80-F-00010659.0004001 / 04 MAR 13 EIVMU 70 During reset, and the subsequent 5 s, the following occurs: ‐ On the corresponding engine: ‐ Loss of thrust reverser. ‐ Loss of vibration indication. ‐ If idle is selected, only high idle is available. ‐ Loss of MAN start and wet crank. ‐ Loss of bleed corrections on N1 limit. ‐ On all engines: • Loss of A/THR • Loss of Flex/Derated T.O. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 QUICK REFERENCE HANDBOOK NORMAL PROCEDURES TABLE OF CONTENTS NP 1/2 01 DEC 14 Normal Procedures NP-NP Airline Policy........................................................................................... 1/16 Safety Exterior Inspection.......................................................................2/16 Preliminary Cockpit Preparation............................................................. 2/16 Cockpit Preparation................................................................................ 3/16 Before Pushback or Start....................................................................... 5/16 ENG Start............................................................................................... 6/16 After Start............................................................................................... 6/16 Taxi......................................................................................................... 6/16 Before Takeoff........................................................................................ 7/16 Takeoff.................................................................................................... 7/16 After Takeoff........................................................................................... 8/16 Climb.......................................................................................................8/16 Cruise......................................................................................................9/16 Descent Preparation............................................................................... 9/16 Descent...................................................................................................9/16 Aircraft Configuration for Approach...................................................... 10/16 Approach using LOC G/S Guidance.................................................... 11/16 Approach using FINAL APP Guidance.................................................11/16 Approach using FPA Guidance............................................................ 12/16 Landing................................................................................................. 13/16 Go Around............................................................................................ 14/16 After Landing........................................................................................ 14/16 Parking..................................................................................................15/16 Securing the Aircraft.............................................................................15/16 Normal Checklist NP-NCL Before Start...............................................................................................C3 After Start..................................................................................................C3 Before Takeoff.......................................................................................... C3 After Takeoff / Climb.................................................................................C3 Approach................................................................................................... C3 Landing......................................................................................................C3 After Landing.............................................................................................C3 Parking...................................................................................................... C3 Securing the Aircraft................................................................................. C3 Takeoff CG / TRIM POS.......................................................................... C3 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK NORMAL PROCEDURES TABLE OF CONTENTS Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP 2/2 01 DEC 14 A330 NORMAL PROCEDURES QUICK REFERENCE HANDBOOK NP-NP 1/16 01 DEC 14 AIRLINE POLICY Ident.: NP-NP-18700050.9001001 / 01 DEC 14 Applicable to: ALL The Airline Policy chapter contains a set of rules defined by TAM. These rules were created and are always being updated according to TAM's needs as well as local regulations. Flight safety, operational eficiency, punctuality and passenger confort are the main goals of TAM's policies. All rules may be found on the Airline's General Operating Manual (MGO - Manual Geral de Operações), but the ones that directly affect procedures contained on the FCOM may be found in this manual. GENERAL POLICIES ‐ The CM1 must be the left hand seat pilot ‐ The CM2 must be the right hand seat pilot The CM2 is not allowed to taxi the aircraft. The only exceptions are the following: ‐ The CM2 is a Instructor Captain. In this case, he/she may taxi at any time ‐ In case of Pilot Incapactation, the co-pilot may only taxi the aircraft to clear the runway. Once the aircraft gets to the taxiway, it must be stopped and a pushback tractor must be used to continue taxi to the gate. The co-pilot may not perform a 180 degree turn. In this case, the aircraft must remain on the runway and ATC must be notified. FMGS DATA The following actions are assigned to the pilots as they are described (either being CM1 or CM2): ‐ The PF is responsible for the FMGS initialization and data insertion ‐ The PNF must always perform the data confirmation REJECTED TAKEOFF Please observe the following rules regarding Rejected Takeoffs (RTO): ‐ If the Co-Pilot is flying as PF, he may even callout a failure but only the Captain may call STOP and perform the RTO actions. As soon as the Captain calls STOP, the Co-Pilot becomes the PNF. ‐ If the CM1 is a Captain under training and is flying as PF, he/she may make the decision and perform the RTO actions. In this case, the Instructor Captain (CM2) will continue as PNF. ‐ If it happens that the CM1 is a Captain under training and is flying as PF but the Instructor Captain (CM2) thinks a stop is required, the Instructor will call STOP and the Captain under training will perform the RTO actions. Note: This procedure must be carefully briefed so that both pilots understand each other's actions. Both Emergency and Rejected Takeoff Briefings must be done by either the Instructor Captain or the Captain under training. FLIGHT OPERATIONS PUBLICATIONS The Flight Crew must be updated and aware of all Flight Operations Bulletins, such as: ‐ Technical Bulletin ‐ Airport Info ‐ Flight Standards Informative The publications listed above are the ones that have major impact on airline policy and operational procedures. It is important to remember that other documents published by the Flight Operations and Flight Safety Department that are not listed here might have valuable information for the flight as well. SINGLE PACK ON GROUND A controlled use of PACKS on ground is an Airbus initiative that has been put into practice by TAM. The procedures related to the use of PACKS on ground are described in the appropriate sections of this manual, but an overall may be seen below. As a normal procedure, during ground operations, PACK 1 is the only PACK to be used. PACK 2 must be used as following: When boarding starts: PACK 2................................................................................................................ ON TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 2/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK After Engine Start: PACK 2...............................................................................................................OFF The Single Pack On Ground procedure must not be used if: ‐ The airport is at 9 200 ft or higher ‐ The cabin temperature reaches 26°C. In this case, the Captain may set the PACK 2 sw to ON to improve passenger and crew confort ‐ Operational needs or weather conditions require so ONE ENGINE TAXI IN The ONE ENGINE TAXI IN is the standard operating procedure when taxiing in the aircraft. It must not be performed if one or more of the following conditions apply: ‐ Overweight landing / high gross weight. ‐ Slippery taxiways. ‐ Uphill slopes. ‐ Low visibility conditions. ‐ APU not working. ‐ The Captain considers the procedure will have and impact on the flight's safety or workload will increase too much after landing / during taxi. SAFETY EXTERIOR INSPECTION Ident.: NP-NP-00010661.0001001 / 29 OCT 14 Applicable to: ALL CM1 CM2 * WHEEL CHOCKS........................................................ CHECK * L/G DOORS...............................................CHECK POSITION * APU AREA................................................................... CHECK PRELIMINARY COCKPIT PREPARATION Ident.: NP-NP-00010662.9001003 / 01 DEC 14 Applicable to: ALL CM1 CM2 DOCUMENTATION AND MAINTENANCE...................... VERIFY EMER EQPT.....................................................................CHECK * GEAR PINS and COVERS.......CHECK ONBOARD/STOWED ENG MASTERS 1, 2............................................................. OFF * OEB IN QRH................................................................CHECK ENG START selector........................................... CHECK NORM * WEATHER RADAR........................................................... OFF L/G lever............................................................................ DOWN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 3/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page CM1 CM2 Both WIPER selectors........................................................... OFF BAT .......................................................................CHECK/AUTO EXT PWR pb-sw...........................................................AS RQRD APU FIRE............................................................... CHECK/TEST APU .................................................................................. START When the APU is AVAIL: * EXT PWR pb-sw......................................................AS RQRD AIR COND panel....................................................................SET * COCKPIT LIGHT......................................................AS RQRD * ECAM RCL pb..............................................................PRESS * ECAM OXY PRESS/HYD QTY/ENG OIL QTY ........... CHECK FLAPS............................................................ CHECK POSITION * SPD BRK lever........................CHECK RET AND DISARMED * PARKING BRAKE handle................................................... ON * ACCU/BRAKES PRESS.............................................. CHECK ALTN BRAKING............................................................... CHECK * OEB IN QRH .............................................................. CHECK RAIN REPELLENT........................................................... CHECK * GEAR PINS and COVERS.......CHECK ONBOARD/STOWED * EXTERIOR WALKAROUND...................................PERFORM COCKPIT PREPARATION Ident.: NP-NP-00010663.0014001 / 01 DEC 14 Applicable to: ALL CM1 CM2 OVERHEAD PANEL: * ALL WHITE LIGHTS.......................................... EXTINGUISH * AIRFIELD DATA..........................................................OBTAIN TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 4/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page CM1 CM2 * RCDR GND CTL pb-sw......................................................ON CAPT & PURS/CAPT sw.................................................... CAPT * ALL IR MODE selector.................................................... NAV * RESET BUTTONS (left side).......................................CHECK EXTERIOR LIGHTS...............................................................SET * SIGNS................................................................................SET PROB/WINDOW HEAT.......................................................AUTO LDG ELEV ........................................................................ AUTO VALVE SEL.........................................................................BOTH * PACK 1............................................................................... ON * PACK 2.................................................................... AS RQRD * PACK FLOW............................................................AS RQRD BAT ..................................................................................CHECK FUEL T. TANK................................................................... AUTO ENG FIRE.............................................................. CHECK/TEST DATA LOADER........................................................CHECK OFF MAINT panel.....................................................................CHECK VENT panel...................................................................... CHECK PA (3rd occupant).......................................................... RECEPT CVR TEST pb...................................................................PRESS * RESET BUTTONS (right side).....................................CHECK CTR INSTRUMENT PANEL: * ISIS / STBY INST........................................................ CHECK * NORTH REF ...............................................................CHECK ECAM SWITCHING..........................................................CHECK * CLOCK.................................................................CHECK/SET LDG GEAR GRVTY EXTN sw.............................................. OFF * A/SKID & NW STRG sw.....................................................ON PEDESTAL: ACP ................................................................................. CHECK * PARK BRK...............................................................AS RQRD COCKPIT DOOR..............................................................CHECK SWITCHING PANEL......................................................... NORM * THRUST LEVERS.............................................. CHECK IDLE * REVERSER LEVERS...............................................STOWED * ENG MASTERS.................................................. CHECK OFF * ENG START Selector......................................CHECK NORM * ATC .................................................................................. SET RMP ...................................................................................... SET * MSG RECORD (MCDU).............................................. ERASE * ADS (MCDU)................................................. CHECK ARMED * ACARS....................................................................INITIALIZE * FMS ..................................................... PREPARE (PF TASK) * FMS PREPARATION .............................CHECK (PNF TASK) •When both flight crewmembers seated: GLARESHIELD: GLARESHIELD: TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 5/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page CM1 CM2 * LOUDSPEAKER knob.......................................................SET * LOUDSPEAKER knob....................................................... SET * BAROMETRIC REFERENCE........................................... SET * BAROMETRIC REFERENCE............................................ SET * FD ........................................................................ CHECK ON * FD .........................................................................CHECK ON * LS ........................................................................... AS RQRD * LS ............................................................................AS RQRD * ND mode and range..........................................................SET * ND mode and range.......................................................... SET * ADF/VOR selector................................................... AS RQRD * ADF/VOR selector....................................................AS RQRD * FCU .................................................................................. SET LATERAL CONSOLE: LATERAL CONSOLE: OXY MASK.......................................................................... TEST OXY MASK...........................................................................TEST INSTRUMENT PANEL: INSTRUMENT PANEL: EFIS DMC selector........................................................... NORM EFIS DMC selector........................................................... NORM PFD-ND brightness......................................................... ADJUST PFD-ND brightness..........................................................ADJUST * PFD-ND ...................................................................... CHECK * PFD-ND .......................................................................CHECK * LDG ELEV (ECAM).......................................... CHECK AUTO * IRS ALIGN....................................................................CHECK * ECAM STATUS........................................................... CHECK TAKEOFF BRIEFING................................PERFORM (PF TASK) BEFORE PUSHBACK OR START Ident.: NP-NP-00010664.9001002 / 01 DEC 14 Applicable to: ALL CM1 CM2 LOADSHEET.................................................. CHECK (PF TASK) FOB ................................................................................. CHECK FOB ................................................................................. CHECK TO DATA.......................................... ENTER/REVISE (PF TASK) TO DATA..................................................... CHECK (PNF TASK) SEATING POSITION.......................................................ADJUST SEATING POSITION.......................................................ADJUST FMS PERF TO page...................................SELECT (PF TASK) FMS F-PLN page .................................... SELECT (PNF TASK) EXT PWR .............................................................CHECK AVAIL EXT PWR DISCONNECTION ................................... REQUEST BEFORE START C/L down to the line...................... COMPLETE BEFORE START C/L down to the line...................... COMPLETE SAFETY CHECK ............................................................ OBTAIN PUSHBACK/START CLEARANCE..................................OBTAIN WINDOWS/DOORS..........................................CHECK CLOSED WINDOWS/DOORS..........................................CHECK CLOSED SLIDES............................................................... CHECK ARMED SLIDES............................................................... CHECK ARMED BEACON sw ........................................................................... ON THRUST LEVERS.................................................................IDLE NW STRG DISC............................................. CHECK AS RQRD PARK BRK ACCU PRESS...............................................CHECK PARKING BRK ............................................................AS RQRD BEFORE START C/L below the line......................... COMPLETE BEFORE START C/L below the line......................... COMPLETE PUSH BACK.....................................................................ORDER ELAPSED TIME............................................................AS RQRD TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 6/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK ENG START Ident.: NP-NP-00010665.0001001 / 29 OCT 14 Applicable to: ALL CM1 CM2 ENG START selector..................................................... IGN START ENGINE 1 START......................................................... ANNOUNCE ENG MASTER switch 1................................................................ ON ENG IDLE PARAMETERS.................................................... CHECK ENGINE 2 START......................................................... ANNOUNCE REPEAT THE START SEQUENCE FOR ENG 2 AFTER START Ident.: NP-NP-00010666.0005001 / 01 DEC 14 Applicable to: ALL CM1 CM2 ENG START selector........................................................ NORM APU BLEED pb-sw ...............................................................OFF GND SPOILERS................................................................... ARM ENG ANTI ICE pb-sw ..................................................AS RQRD RUD TRIM...........................................................................ZERO WING ANTI ICE pb-sw ................................................AS RQRD FLAPS.................................................................................... SET APU MASTER SW....................................................... AS RQRD PITCH TRIM...........................................................................SET PACK 2.........................................................................AS RQRD NWS TOWING FAULT LT .................................CHECK off ECAM STATUS................................................................ CHECK ECAM STATUS................................................................ CHECK CLEAR TO DISCONNECT....................................... ANNOUNCE N/W STEER DISC MEMO.................. CHECK NOT DISPLAYED AFTER START C/L .................................................. COMPLETE AFTER START C/L .................................................. COMPLETE TAXI Ident.: NP-NP-00010667.0030001 / 01 DEC 14 Applicable to: ALL CM1 CM2 EXTERIOR LIGHTS............................................................... SET TAXI CLEARANCE.......................................................... OBTAIN •Taxi clearance obtained: PARKING BRAKE handle......................................................OFF THRUST LEVERS........................................................ AS RQRD BRAKES............................................................................CHECK BRAKES............................................................................CHECK FLT CTL .......................................................................... CHECK FLT CTL .......................................................................... CHECK • ATC clearance obtained: ATC CLEARANCE........................................................CONFIRM T.O DATA......................................................................... CHECK FMS F-PLAN/SPD .............................................REVISE/CHECK FCU ALT/HDG ...................................................................... SET BOTH FD .................................................................. CHECK ON PFD/ND ........................................................................... CHECK PFD/ND ........................................................................... CHECK TAKEOFF BRIEFING................................................... CONFIRM RADAR and PREDICTIVE WINDSHEAR SYSTEM..... ON/AUTO ATC CODE........................................................... CONFIRM/SET TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 7/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page CM1 CM2 TERR ON ND............................................................... AS RQRD TERR ON ND............................................................... AS RQRD AUTO BRK ...........................................................................MAX T.O CONFIG pb ..................................................................TEST T.O MEMO ..................................................... CHECK NO BLUE CABIN REPORT............................................................RECEIVE CABIN REPORT............................................................RECEIVE BEFORE TAKEOFF C/L down to the line................. COMPLETE BEFORE TAKEOFF C/L down to the line................. COMPLETE BEFORE TAKEOFF Ident.: NP-NP-00010668.0001001 / 17 NOV 14 Applicable to: ALL CM1 CM2 BRAKE TEMP ................................................................. CHECK BRAKE FAN pb-sw (if brake fan running).....................OFF TAKEOFF/LINE UP CLEARANCE.................................. OBTAIN EXTERIOR LIGHTS............................................................... SET TCAS Mode selector .............................................. TA or TA/RA APPROACH PATH................................ CLEARED OF TRAFFIC APPROACH PATH................................ CLEARED OF TRAFFIC CABIN CREW.................................................................. ADVISE ENG START selector................................................... AS RQRD SLIDING TABLE............................................................STOWED SLIDING TABLE............................................................STOWED TAKEOFF RUNWAY.................................................... CONFIRM TAKEOFF RUNWAY.................................................... CONFIRM PACKS 1................................................................................ OFF PACKS 2.................................................................. CHECK OFF BEFORE TAKEOFF C/L below the line.................... COMPLETE BEFORE TAKEOFF C/L below the line.................... COMPLETE TAKEOFF Ident.: NP-NP-00010669.0003001 / 01 DEC 14 Applicable to: ALL PF PNF TAKEOFF..................................................................ANNOUNCE BRAKES........................................................................RELEASE THRUST LEVERS................................................. FLX or TOGA CHRONO........................................................................... START The Captain places hand on thrust levers until V1 DIRECTIONAL CONTROL....................................USE RUDDER FMA ......................................................................... ANNOUNCE PFD/ND ....................................................................... MONITOR •BELOW 80 kt: N1 (EPR).......................................................................... CHECK THRUST SET........................................................... ANNOUNCE PFD and ENG indications............................................ MONITOR •AT 100 kt: ONE HUNDRED KNOTS..........................................ANNOUNCE 100 kt ...............................................................................CHECK •AT V1 -5 kt: V1 ............................................................................ ANNOUNCE •AT VR: ROTATION....................................................................... ORDER ROTATION.............................................ANNOUNCE/PERFORM •WHEN POSITIVE CLIMB: POSITIVE CLIMB..................................................... ANNOUNCE L/G UP..............................................................................ORDER L/G ........................................................................... SELECT UP TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 8/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page PF PNF AP ................................................................................AS RQRD •AT THR RED ALT: THRUST LEVERS................................................................... CL PACK 1 ...................................................................................ON •AT F SPEED: FLAPS 1........................................................................... ORDER FLAPS 1.......................................................................... SELECT •AT S SPEED: FLAPS 0........................................................................... ORDER FLAPS 0.......................................................................... SELECT GND SPLRS .................................................................. DISARM EXTERIOR LIGHTS............................................................... SET PACK 2 ...................................................................................ON AFTER TAKEOFF Ident.: NP-NP-00010670.0001001 / 01 DEC 14 Applicable to: ALL PF PNF APU BLEED pb-sw ......................................................AS RQRD APU MASTER SW ...................................................... AS RQRD ENG START selector................................................... AS RQRD TCAS Mode selector ........................................................ TA/RA ANTI ICE pb-sw .......................................................... AS RQRD AFTER TAKEOFF/CLIMB C/L down to the line.........COMPLETE AFTER TAKEOFF/CLIMB C/L down to the line.........COMPLETE CLIMB Ident.: NP-NP-00010671.0007001 / 04 MAR 14 Applicable to: ALL PF PNF MCDU.......................................................................... PERF CLB MCDU..................................................................................F-PLN FCU/FMGS............................................................SET IF AP ON FCU/FMGS.......................................................... SET IF AP OFF •At transition altitude: BAROMETRIC REFERENCE..............SET STD/CROSSCHECK BAROMETRIC REFERENCE..............SET STD/CROSSCHECK AFTER TAKEOFF/CLIMB C/L below the line............COMPLETE AFTER TAKEOFF/CLIMB C/L below the line............COMPLETE RADAR........................................... ADJUST AS APPROPRIATE ENG ANTI ICE............................................................. AS RQRD •At 10 000 ft: LAND LIGHTS sw.................................................................. OFF SEAT BELTS sw.......................................................... AS RQRD EFIS option...................................................................AS RQRD EFIS option...................................................................AS RQRD ECAM MEMO..................................................................REVIEW NAVAIDS........................................................................... CLEAR SEC F-PLN...................................................................AS RQRD OPT/MAX ALT.................................................................. CHECK TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 9/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK CRUISE Ident.: NP-NP-00010672.0003001 / 01 DEC 14 Applicable to: ALL PF PNF ECAM MEMO/SD PAGES.............................................. REVIEW FLIGHT PROGRESS........................................................CHECK FUEL.............................................................................MONITOR STEP FLIGHT LEVEL................................... AS APPROPRIATE NAVIGATION ACCURACY.......................................... MONITOR RADAR........................................... ADJUST AS APPROPRIATE EMERGENCY BRIEFING........................................... PERFORM DESCENT PREPARATION Ident.: NP-NP-00010673.0002001 / 01 DEC 14 Applicable to: ALL PF PNF WEATHER AND LANDING INFORMATION................... OBTAIN LANDING PERFORMANCE.........................................CONFIRM LANDING PERFORMANCE............................................. CHECK FMS .............................................................................PREPARE FMS PREPARATION........................................................CHECK LDG ELEV........................................................................ CHECK AUTO BRK .................................................................. AS RQRD APPR BRIEFING.........................................................PERFORM TERR ON ND .....................................................AS RQRD TERR ON ND .....................................................AS RQRD RADAR........................................... ADJUST AS APPROPRIATE ENG ANTI ICE pb-sw ..................................................AS RQRD WING ANTI ICE pb-sw ................................................AS RQRD DESCENT CLEARANCE................................................. OBTAIN CLEARED ALTITUDE ON FCU ............................................SET DESCENT Ident.: NP-NP-00010674.0005001 / 01 DEC 14 Applicable to: ALL PF PNF DESCENT....................................................................... INITIATE MCDU .................................................. PROG/PERF DESCENT MCDU .............................................................................. F-PLN DESCENT...................................................... MONITOR/ADJUST •When the aircraft approaches the transition level, and when cleared for an altitude: BAROMETRIC REFERENCE.......................SET/CROSSCHECK BAROMETRIC REFERENCE......................SET/CROSSCHECK ECAM STATUS................................................................CHECK •At 10 000 ft: LAND LIGHTS sw ..................................................................ON CABIN CREW..................................................................ADVISE SEAT BELTS sw ....................................................................ON EFIS option pb .................................................................. CSTR EFIS option pb ................................................................. CSTR LS pb ........................................................................... AS RQRD LS pb .......................................................................... AS RQRD RADIO NAV ....................................................... SELECT/IDENT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 10/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page PF PNF ENG START selector ..................................................AS RQRD •If GPS PRIMARY not available: NAV ACCY........................................................................ CHECK APPROACH C/L........................................................ COMPLETE APPROACH C/L....................................................... COMPLETE AIRCRAFT CONFIGURATION FOR APPROACH Ident.: NP-NP-00014801.0002001 / 01 DEC 14 Applicable to: ALL PF PNF INITIAL APPROACH: F-PLN SEQUENCING..................................................... ADJUST •Approx 15 nm from touchdown: APPR PHASE.............................. ACTIVATE or set green dot (1) MANAGED SPEED...........................................................CHECK FLIGHT PATH.............................................................. MONITOR NAV ACCURACY.........................................................MONITOR SPEED BRAKES lever ................................................AS RQRD RADAR........................................... ADJUST AS APPROPRIATE INTERMEDIATE/FINAL APPROACH: •At green dot: FLAPS 1........................................................................... ORDER FLAPS 1.......................................................................... SELECT S SPEED ..................................................... CHECK OR SET (1) TCAS ............................................................ TA or TA/RA •At 2 500 ft AGL: FLAPS 2........................................................................... ORDER FLAPS 2.......................................................................... SELECT F SPEED........................................................CHECK OR SET(1) •When FLAPS 2 L/G DOWN....................................................................... ORDER L/G .....................................................................SELECT DOWN AUTO BRAKE.............................................................. CONFIRM GRND SPLRS....................................................................... ARM EXTERIOR LIGHTS............................................................... SET •When L/G down: FLAPS 3........................................................................... ORDER FLAPS 3.......................................................................... SELECT ECAM WHEEL PAGE...................................................... CHECK •When FLAPS 3: FLAPS FULL.................................................................... ORDER FLAPS FULL................................................................... SELECT VAPP ............................................................ CHECK OR SET(1) A/THR ........................................................ CHECK SPD or OFF WING A. ICE (if not required)................................................OFF SLIDING TABLE.................................................................STOW SLIDING TABLE.................................................................STOW LDG MEMO..................................................... CHECK NO BLUE CABIN REPORT............................................................RECEIVE CABIN REPORT............................................................RECEIVE CABIN CREW.................................................................. ADVISE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 11/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page PF PNF LDG C/L ................................................................... COMPLETE LDG C/L ................................................................... COMPLETE ANNOUNCE ANY FMA MODIFICATION FLT PARAMETERS..................................................... MONITOR Announce any deviation in excess of: • V/S : 1 200 ft/min • IAS : speed target +10 kt; VAPP -5 kt • PITCH : 0 ° nose down; 10 ° nose up • BANK : 7 ° (1) PF if AP is ON, PNF if AP is OFF. The PF may request that this action is performed by the PNF depending on the situation. APPROACH USING LOC G/S GUIDANCE Ident.: NP-NP-00014802.0001001 / 01 DEC 14 Applicable to: ALL PF PNF INITIAL / INTERMEDIATE APPROACH: APPR pb on FCU ............................................................ PRESS BOTH AP ......................................................................ENGAGE LOC ................................................................... CHECK ARMED G/S .................................................................... CHECK ARMED LOC CAPTURE............................................................MONITOR G/S CAPTURE............................................................. MONITOR GO-AROUND ALT ............................................................ SET(1) FINAL APPROACH: FLT PARAMETERS..................................................... MONITOR Announce any deviation in excess of: • LOC : ½ dot • GLIDE : ½ dot •At minimum + 100 ft: ONE HUNDRED ABOVE..........................................ANNOUNCE •At minimum: CONTINUE or GO-AROUND................................... ANNOUNCE MINIMUM......................................... MONITOR OR ANNOUNCE (1) PF if AP is ON, PNF if AP is OFF. The PF may request that this action is performed by the PNF depending on the situation. APPROACH USING FINAL APP GUIDANCE Ident.: NP-NP-00014803.0002001 / 01 DEC 14 Applicable to: ALL PF PNF DESCENT PREPARATION: WEATHER AND LANDING INFO................................... OBTAIN F-PLN A Page...................................................................CHECK F-PLN A Page..................................................................CHECK PROG Page............................................................... COMPLETE PROG Page.............................................................. COMPLETE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 12/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page PF PNF GO-AROUND STRATEGY.............................................. REVIEW DESCENT: •At 10 000 ft NAV ACCURACY..............................................................CHECK •For RNAV(GNSS): GPS PRIMARY......................................................CHECK BARO REF ............................................................................ SET INITIAL/INTERMEDIATE/FINAL APPROACH: POSITION..................................................................... MONITOR APPR pb on FCU .............................................................PRESS APP NAV ..................................CHECK ARMED OR ENGAGED FINAL.................................................................. CHECK ARMED •At Final Descent Point: FINAL APP ................................................... CHECK ENGAGED GO-AROUND ALT ........................................................................ SET(1) FLT PARAMETERS.....................................................MONITOR Announce any deviation in excess of: • XTK > 0.1 nm • V/DEV > ½ dot •At minimum + 100 ft: ONE HUNDRED ABOVE......................................... ANNOUNCE •At minimum: CONTINUE or GO-AROUND....................................ANNOUNCE MINIMUM.........................................MONITOR OR ANNOUNCE (1) PF if AP is ON, PNF if AP is OFF. The PF may request that this action is performed by the PNF depending on the situation. APPROACH USING FPA GUIDANCE Ident.: NP-NP-00014804.0002001 / 01 DEC 14 Applicable to: ALL PF PNF DESCENT PREPARATION: F-PLN A Page...................................................................CHECK F-PLN A Page.................................................................. CHECK PROG Page...............................................................COMPLETE PROG Page.............................................................. COMPLETE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 13/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page PF PNF GO-AROUND STRATEGY..............................................REVIEW DESCENT: •At 10 000 ft: NAV ACCURACY..............................................................CHECK •For RNAV(GNSS): GPS PRIMARY ....................................................CHECK INITIAL/INTERMEDIATE/FINAL APPROACH: LATERAL GUIDANCE MODE.................. SET FOR APPROACH •For LOC ONLY, ILS G/S OUT and back course localizer approaches: LOC pb-sw ...........................................................PRESS LOC / LOC B/C ..................................... CHECK ARMED LATERAL path.......................................................... INTERCEPT TRK FPA (Bird)............................................................... SELECT FPA FOR FINAL APPROACH............................................... SET •At 0.3 nm from the Final Descent Point: FPA pb ................................................................................ PULL FPA ...............................................................CHECK ENGAGED POSITION/FLT PATH....................................MONITOR/ADJUST GO-AROUND ALT ........................................................................SET(1) FLT PARAMETERS..................................................... MONITOR Announce any deviation in excess of: • Approach using NAV MODE: XTK > 0.1 nm • Approach using LOC or LOC B/C MODE: LOC ½ dot • Approach using TRK MODE ▪ VOR: ½ dot or 2.5 ° ▪ NDB: 5 ° •At minimum + 100 ft: ONE HUNDRED ABOVE......................................... ANNOUNCE •At minimum: CONTINUE or GO-AROUND....................................ANNOUNCE MINIMUM......................................... MONITOR OR ANNOUNCE (1) PF if AP is ON, PNF if AP is OFF. The PF may request that this action is performed by the PNF depending on the situation. LANDING Ident.: NP-NP-00010678.0003001 / 24 FEB 14 Applicable to: ALL PF PNF •In stabilized approach conditions, at approx. 40 ft: FLARE......................................................................... PERFORM ATTITUDE.................................................................... MONITOR THRUST LEVERS.................................................................IDLE •At touchdown: DEROTATION................................................................ INITIATE ALL REVERSER LEVERS....................REV MAX OR REV IDLE GRND SPLRS............................................. CHECK/ANNOUNCE REVERSERS.............................................. CHECK/ANNOUNCE DIRECTIONAL CONTROL.............................................ENSURE DIRECTIONAL CONTROL...........................................MONITOR BRAKES....................................................................... AS RQRD DECELERATION.........................................CHECK/ANNOUNCE •At 70 kt: ALL REVERSER LEVERS....................................................IDLE 70 kt .........................................................................ANNOUNCE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 14/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page PF PNF •At taxi speed: ALL REVERSER LEVERS................................................. STOW •Before 20 kt: AUTO BRK...............................................................DISENGAGE GO AROUND Ident.: NP-NP-00010679.0001001 / 01 DEC 14 Applicable to: ALL PF PNF THRUST LEVERS............................................................. TOGA ROTATION.................................................................. PERFORM GO AROUND............................................................ANNOUNCE FLAPS lever ................................................. SELECT AS RQRD FMA ......................................................................... ANNOUNCE POSITIVE CLIMB..................................................... ANNOUNCE L/G UP..............................................................................ORDER L/G ........................................................................... SELECT UP AP................................................................................. AS RQRD NAV or HDG mode.......................................................AS RQRD •AT GA THR RED ALT: THRUST LEVERS................................................................... CL •AT GA ACCEL ALT: SPEED..........................................................................MONITOR •AT F SPEED: FLAPS 1........................................................................... ORDER FLAPS 1.......................................................................... SELECT •AT S SPEED: FLAPS 0........................................................................... ORDER FLAPS 0.......................................................................... SELECT GND SPLRS .................................................................. DISARM EXTERIOR LIGHTS............................................................... SET AFTER TAKEOFF C/L down to the line.................... COMPLETE AFTER TAKEOFF C/L down to the line.................... COMPLETE AFTER LANDING Ident.: NP-NP-00010680.0001001 / 01 DEC 14 Applicable to: ALL CM1 CM2 GRND SPLRS................................................................. DISARM EXTERIOR LIGHTS............................................................... SET RADAR.........................................................................OFF/STBY PREDICTIVE WINDSHEAR .........................................OFF ENG START selector........................................................ NORM FLAPS.......................................................................... RETRACT TCAS ..................................................................SET on standby ATC ............................................................................. AS RQRD PACK 2 ................................................................................. OFF APU .................................................................................. START ANTI ICE...................................................................... AS RQRD BRAKE TEMP ................................................................. CHECK TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 15/16 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page CM1 CM2 AFTER LDG C/L .................................................COMPLETE(1) AFTER LDG C/L .................................................COMPLETE(1) •If the One Engine Taxi will be applied: ENGINE 2 SHUTDOWN ENG 2 MASTER.................................................................... OFF (1) The After Landing Checklist is performed silently. PARKING Ident.: NP-NP-00010681.9001002 / 01 DEC 14 Applicable to: ALL CM1 CM2 ACCU PRESS.................................................................. CHECK ANTI-ICE................................................................................ OFF PARKING BRAKE handle ...................................................... ON APU BLEED pb-sw .................................................................ON ELAPSED TIME.................................................................. STOP ENG 1 MASTER sw ............................................................. OFF ENG 2 MASTER sw ........................................CHECK OFF/OFF SLIDE DISARM................................................................ ORDER SLIDE DISARM.........................................................ANNOUNCE SLIDE DISARMED............................................................CHECK BEACON light ....................................................................... OFF SEAT BELTS sw .................................................................. OFF FUEL PUMPS........................................................................ OFF EXTERIOR LIGHTS............................................................... SET ATC .................................................................... SET on standby GROUND CONTACT................................................ ESTABLISH IRS PERFORMANCE.......................................................CHECK FUEL QTY .......................................................................CHECK STATUS............................................................................ CHECK PARKING BRK ............................................................AS RQRD BRAKE FAN ...............................................................OFF DUs......................................................................................... DIM DUs......................................................................................... DIM PARKING C/L ...........................................................COMPLETE PARKING C/L ...........................................................COMPLETE SECURING THE AIRCRAFT Ident.: NP-NP-00010682.0001001 / 01 DEC 14 Applicable to: ALL CM1 CM2 PARK BRK ................................................................CHECK ON ADIRS (1 + 2 + 3)................................................................. OFF OXY CREW SUPPLY pb ......................................................OFF EXTERIOR LIGHTS...............................................................OFF GND SELECT CTL sw................................................. AS RQRD APU BLEED pb-sw ...............................................................OFF EXT PWR pb ...............................................................AS RQRD APU MASTER SW.................................................................OFF EMER EXIT LT sw ............................................................... OFF SIGNS sw ............................................................................. OFF BAT 1 + 2 + APU ................................................................. OFF SECURING THE A/C C/L ....................................... COMPLETE SECURING THE A/C C/L ....................................... COMPLETE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 NORMAL PROCEDURES QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 16/16 01 DEC 14 A330 QUICK REFERENCE HANDBOOK IN FLIGHT PERFORMANCE TABLE OF CONTENTS PER 1/2 01 DEC 14 Speeds PER-A Operating Speeds.....................................................................................1/2 Green Dot Speed..................................................................................... 1/2 VLS........................................................................................................... 1/2 Fuel Penalty Factors PER-B Use of Fuel Penalty Factor Tables...........................................................1/4 Fuel Penalty Factors/ECAM Alert Table.................................................. 2/4 Fuel Penalty Factors/Inop Sys Table....................................................... 3/4 Landing Performance Assessment PER-C Method to Determine Aircraft Performance at Landing without or with a Single Failure............................................................................................1/6 Method to Determine Aircraft Performance at Landing with Several Failures..................................................................................................... 2/6 Runway Condition Assessment Matrix for Landing..................................3/6 VAPP Determination without Failure........................................................ 5/6 VAPP Determination with Failure............................................................. 6/6 Landing Distance without Failure PER-D Landing Distance without Failure ............................................................1/4 Landing Distance with Electrical System Failure PER-24 Landing Distance with Flight Controls System Failure PER-27 Landing Distance with Slats and Flaps System Failure PER-27A Landing Distance with Fuel System Failure PER-28 Landing Distance with Hydraulic System Failure PER-29 Landing Distance with Anti Ice System Failure PER-30 Landing Distance with Brake System Failure PER-32 Landing Distance with Navigation System Failure PER-34 Landing Distance with Bleed System Failure PER-36 Landing Distance with Engine System Failure PER-70 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK IN FLIGHT PERFORMANCE TABLE OF CONTENTS PER 2/2 01 DEC 14 Continued from the previous page One Engine Inoperative PER-E Ceilings..................................................................................................... 1/8 Gross Flight Path Descent at Green Dot Speed...................................... 3/8 Cruise at Long Range Cruise speed........................................................5/8 In Cruise Quick Check Long Range.........................................................7/8 All Engines Operative PER-G Optimum & Maximum Altitudes.............................................................. 1/10 In Cruise Quick Check at a Given Mach Number.................................. 3/10 Cost Index for Long Range Cruise SpeeD.............................................5/10 Standard Descent...................................................................................6/10 Quick Determination Table of Alternate Flight Planning.........................8/10 Flight Without Cabin Pressurization PER-H In Cruise Quick Check FL 100 Long Range............................................ 1/2 Miscellaneous PER-I Ground Distance / Air Distance Conversion.............................................1/6 IAS / MACH Conversion...........................................................................2/6 ISA Temperature and Pressure Altitude Correction................................. 3/6 Wind Component......................................................................................5/6 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-A 1/2 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK OPERATING SPEEDS Ident.: PER-A-00010699.0014001 / 04 FEB 13 Applicable to: ALL OPERATING SPEEDS (KT) Weight (1000 KG) S VLS CONF 1 F (1) VLS CONF 2 VLS CONF 3 VREF 240 205 187 168 165 159 157 220 197 179 161 158 152 150 200 187 170 153 150 145 143 180 178 162 145 143 138 136 160 168 152 137 135 130 128 140 157 143 128 126 122 120 120 147 133 123 118 118 118 (1) For approach : In CONF 2 : Add 14 %. F is limited to 133 kt (low limit). In CONF 3 : Add 4 %. F is limited to 128 kt (low limit). GREEN DOT SPEED Ident.: PER-A-00010700.0001001 / 04 FEB 13 Applicable to: ALL GREEN DOT SPEED (KT) ALL ENGINES OPERATIVE Weight (1000 KG) at or below FL 200 FL 300 FL 400 240 251 261 271 220 239 249 259 200 227 237 247 180 215 225 235 160 203 213 223 140 191 201 211 120 179 189 199 GREEN DOT SPEED WITH ONE OR TWO ENGINES INOP : Subtract 10 kt from these values. VLS Ident.: PER-A-00010701.0014001 / 04 FEB 13 Applicable to: ALL VLS CONF 0 (KT) Weight (1000 KG) 1.23 VS 0.3 g buffet margin FL 0 FL 100 FL 200 FL 300 FL 300 FL 400 240 209 222 237 245 245 – 220 200 207 226 233 233 – 200 190 192 214 220 220 243 180 181 181 200 206 206 221 160 170 171 182 194 194 203 140 159 159 163 181 177 187 120 148 148 148 164 161 171 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-A 2/2 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-B 1/4 01 DEC 14 USE OF FUEL PENALTY FACTOR TABLES Ident.: PER-B-00014176.0001001 / 06 APR 12 Applicable to: ALL USE OF THE FUEL PENALTY FACTORS The Fuel Penalty Factors provided in the following tables are conservative values, given as a guideline in order to increase the crew awareness and to help the decision making. Note: In case of failure impacting the fuel consumption, the fuel predictions provided by the FMS are no longer reliable (except in One Engine Inoperative OEI condition). The flight crew must still compute and monitor the actual fuel consumption. Refer to the following tables in order to assess the impact of the failure on the fuel consumption after any ECAM alert that: ‐ Displays the line INCREASED FUEL CONSUMP in the STATUS SD page, or ‐ Displays Flight Control Surfaces in the INOP SYS, or ‐ Impacts the Landing Gears or Landing Gear Doors retraction (when extended). The Fuel Penalty Factors given in these tables have been calculated taking into account: ‐ The FUEL CRITICAL INOP SYS, and ‐ The aircraft configuration, speed or altitude described in the CONDITIONS column. Ensure that all these conditions are well met before applying the corresponding Fuel Penalty Factor. METHODOLOGY The methodology is the following: ‐ Check the ECAM ALERT table to determine if a Fuel Penalty Factor is applicable depending on the CONDITIONS column, then ‐ Check the INOP SYS table in order to determine if, according to the actual aircraft status, there is a Fuel Penalty Factor applicable depending on the CONDITIONS column ‐ If only one Fuel Penalty Factor (FPF) is applicable: TRIP FUEL PENALTY = (FOB - EFOB at DEST) x FPF The FMS fuel predictions must be recomputed to take into account this trip fuel penalty. ‐ If two or more Fuel Penalty Factors (FPF) are applicable: TRIP FUEL PENALTY = (FOB - EFOB at DEST) x ( FPF1 + FPF2 +...) The FMS fuel predictions must be recomputed to take into account this trip fuel penalty. Note: Due to previous failures in flight or dispatch under MEL, some failures could have an impact on the fuel consumption: ‐ Without being mentioned in the ECAM ALERT table (only through INOP SYS table), or ‐ If mentioned in the ECAM ALERT table, with additional INOP SYS (other than the one(s) described in the FUEL CRITICAL INOP SYS column for this specific ECAM alert) impacting also the fuel consumption. Example: • Dispatch with the PRIM 3 inoperative under MEL • F/CTL SEC 1 FAULT ECAM caution in flight • These two failures lead to the loss of the left outboard aileron • INOP SYS will displayed “L OUTR AIL” There is no F/CTL SEC 1 FAULT entry in the ECAM table, however there is an entry L(R) INR(OUTR) AIL in the INOP SYS table. Apply the Fuel Penalty Factor related to the INOP SYS “L OUTR AIL” partially extended. Therefore, TRIP FUEL PENALTY = (FOB - EFOB at DEST) x 15 % TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-B 2/4 01 DEC 14 FUEL PENALTY FACTORS/ECAM ALERT TABLE Ident.: PER-B-00014177.0001001 / 05 NOV 12 Applicable to: ALL SYS ECAM ALERT L(R) INR (OUTR) AIL FAULT FUEL CRITICAL INOP SYS 35 % L(R) INR (OUTR) AIL If one or both aileron(s) is/are indicated or L+R INR (OUTR) AIL partially extended 15 % SPLR FAULT If one spoiler is suspected fully extended (2) Cruise Conditions: OPT SPEED................ COST INDEX 0 Set Cost Index (CI) to 0 and use managed speed. CRUISE ALT.................AS REQUIRED Current Flight Level (FL) may not be maintained due to increased drag. Maintain a cruise FL as high as possible. 45 % If one spoiler or one pair of spoilers is partially extended (zero hinge moment) 8% PART SPLRS with BLUE HYD If spoiler 2 or 3 is partially extended after the Up to 7 % (3) loss of the B hydraulic system (1) PART SPLRS with GREEN HYD If spoiler 1 or 5 is partially extended after the Up to 8 % (3) loss of the G hydraulic system (1) PART SPLRS with YELLOW HYD If spoiler 4 or 6 is partially extended after the Up to 15 % (3) loss of the Y hydraulic system (1) ELEV REDUND LOST - If ailerons are preset upwards 20 % FLAPS FAULT/LOCKED FLAPS If Flaps are extended 120 % SLATS FAULT/LOCKED SLATS If Slats are extended 50 % SLATS+FLAPS If Slats and Flaps are extended 150 % B SYS LO PR PART SPLRS If spoilers 2 and 3 are indicated extended (at the time of the failure) 16 % G SYS LO PR PART SPLRS If spoilers 1 and 5 are indicated extended (at the time of the failure) 16 % Y SYS LO PR PART SPLRS If spoilers 4 and 6 are indicated extended (at the time of the failure) 16 % G+B SYS LO PR L+R INR AIL SPLR (1+2+3+5) L ELEV G+Y SYS LO PR L+R OUTR AIL SPLR (1+4+5+6) R ELEV B+Y SYS LO PR SPLR (2+3+4+6) STABILIZER Spoilers 2, 3, 4 and 6 (1) 0% to 15 % (4) L/G RETRACT All landing gears are extended 180 % All landing gears doors are extended 15 % SLATS + FLAPS FAULT/LOCKED HYD FUEL PENALTY FACTOR If one aileron is indicated fully extended (upwards or downwards) L(R) INR (OUTR) AIL SPLR (affected) F/CTL CONDITIONS Both inner ailerons are failed Spoilers 1, 2, 3 and 5 (1) 20 % to 30 % (4) Both outer ailerons are failed Spoilers 1, 4, 5 and 6 (1) 20 % to 30 % (4) Left elevator is failed RAT is extended Right elevator is failed RAT is extended Stabilizer is jammed RETRACTION FAULT L(R) LENGTHENING FAULT L/G GEAR NOT UPLOCKED GEAR UPLOCK FAULT DOORS NOT CLOSED L/G DOOR (1) During the flight, the spoiler(s) may gradually extend and increase(s) the fuel consumption. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK PER-B 3/4 01 DEC 14 (2) A visual inspection, if time permits, can confirm the full extension of the spoiler. (3) The maximum value of the Fuel Penalty Factor provided in the table considers that the two pairs of corresponding spoilers gradually extend during the flight. (4) The minimum value of the Fuel Penalty Factor provided in the table considers that all spoilers remain retracted. The maximum value has been calculated considering that all impacted spoilers gradually extend during the flight. FUEL PENALTY FACTORS/INOP SYS TABLE Ident.: PER-B-00014178.0001001 / 06 APR 12 Applicable to: ALL SYS INOP SYS L(R) INR (OUTR) AIL or L+R INR (OUTR) AIL F/CTL FUEL PENALTY FACTOR If one or both aileron(s) is/are indicated partially extended 15 % FLAPS If Flaps are extended 120 % SLATS If Slats are extended 50 % If Slats and Flaps are extended 150 % All landing gears doors are extended 15 % SLATS+FLAPS L/G CONDITIONS L/G DOOR TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-B 4/4 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-C 1/6 01 DEC 14 METHOD TO DETERMINE AIRCRAFT PERFORMANCE AT LANDING WITHOUT OR WITH A SINGLE FAILURE Ident.: PER-C-00015213.0001001 / 01 DEC 14 Applicable to: ALL Use the following method to determine the runway landing performance level, the FLAPS lever position for landing, the VAPP, and the Factored Landing Distance (FLD): TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-C 2/6 01 DEC 14 METHOD TO DETERMINE AIRCRAFT PERFORMANCE AT LANDING WITH SEVERAL FAILURES Ident.: PER-C-00015214.0001001 / 28 FEB 14 Applicable to: ALL Use the following method to determine the runway landing performance level, the FLAPS lever position for landing, the VAPP, and the Factored Landing Distance (FLD): TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK RUNWAY CONDITION ASSESSMENT MATRIX FOR LANDING Ident.: PER-C-00014117.0006001 / 21 JUL 14 Applicable to: MSN 0700-1118 Note: For Automatic Approach, Landing and Roll Out limitations, refer to FCOM LIM-22. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-C 3/6 01 DEC 14 IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK RUNWAY CONDITION ASSESSMENT MATRIX FOR LANDING Ident.: PER-C-00014117.0002001 / 21 JUL 14 Applicable to: MSN 0232-0472 Note: For Automatic Approach, Landing and Roll Out limitations, refer to FCOM LIM-22. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-C 4/6 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-C 5/6 01 DEC 14 VAPP DETERMINATION WITHOUT FAILURE Ident.: PER-C-00014116.0008001 / 28 FEB 14 Applicable to: ALL The FMGS performs the following VAPP computation for landing in normal configuration (CONF 3 or CONF FULL). TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK VAPP DETERMINATION WITH FAILURE Ident.: PER-C-00014312.0006001 / 28 FEB 14 Applicable to: ALL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-C 6/6 01 DEC 14 PER-D 1/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK LANDING DISTANCE WITHOUT FAILURE Ident.: PER-D-00014090.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine (1) reverse thrust, manual landing , VAPP=VLS without APPR COR. 6 - DRY Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope + 70 + 40 + 120 + 40 (2) WGT FULL 1 310 + 140 SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied + 20 - 10 + 670 3 1 360 + 160 + 80 + 50 + 120 + 40 + 20 - 10 + 790 FULL 1 670 + 120 + 100 + 50 + 150 + 50 + 20 0 + 70 3 1 750 + 130 + 100 + 60 + 160 + 50 + 20 0 + 80 FULL 2 220 + 160 + 130 + 80 + 220 + 70 + 30 - 30 + 100 3 2 340 + 170 + 140 + 80 + 220 + 70 + 40 - 30 + 110 (1) Automatic Landing correction: if CONF FULL, add 260m. If CONF 3, add 240m. (2) Weight correction: if CONF FULL, subtract 40m per 10T below 190T. If CONF 3, subtract 50m per 10T below 190T. 5 - GOOD Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 1 600 + 170 + 120 + 80 + 220 + 70 + 40 - 30 + 490 3 1 700 + 190 + 130 + 80 + 240 + 70 + 50 - 30 + 580 FULL 1 760 + 170 + 120 + 80 + 220 + 70 + 50 - 20 + 110 3 1 870 + 190 + 130 + 80 + 240 + 80 + 60 - 30 + 140 FULL 2 220 + 160 + 130 + 80 + 220 + 70 + 30 - 30 + 100 3 2 340 + 190 + 140 + 80 + 220 + 70 + 40 - 30 + 120 (1) Automatic Landing correction: if CONF FULL, add 300m. If CONF 3, add 280m. (2) Weight correction: if CONF FULL, subtract 60m per 10T below 190T. If CONF 3, subtract 80m per 10T below 190T. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 1 820 + 130 + 100 + 70 + 200 + 60 + 60 - 60 + 550 3 1 920 + 140 + 110 + 70 + 210 + 60 + 70 - 70 + 660 FULL 1 980 + 130 + 100 + 70 + 210 + 60 + 70 - 80 + 90 3 2 090 + 140 + 110 + 70 + 210 + 70 + 80 - 90 + 110 FULL 2 220 + 160 + 130 + 80 + 220 + 80 + 60 - 30 + 100 3 2 350 + 170 + 140 + 80 + 230 + 70 + 60 - 30 + 110 (1) Automatic Landing correction: if CONF FULL, add 290m. If CONF 3, add 270m. (2) Weight correction: if CONF FULL, subtract 60m per 10T below 190T. If CONF 3, subtract 80m per 10T below 190T. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-D 2/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK 3 - MEDIUM Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 2 030 + 150 + 110 + 80 + 240 + 60 + 90 - 90 + 520 3 2 150 + 160 + 120 + 80 + 240 + 70 + 110 - 100 + 630 FULL 2 170 + 150 + 110 + 80 + 240 + 70 + 100 - 110 + 100 3 2 300 + 160 + 120 + 80 + 250 + 80 + 120 - 120 + 120 FULL 2 310 + 160 + 130 + 90 + 250 + 70 + 90 - 40 + 110 3 2 440 + 170 + 140 + 90 + 250 + 80 + 110 - 60 + 120 (1) Automatic Landing correction: if CONF FULL, add 300m. If CONF 3, add 280m. (2) Weight correction: if CONF FULL, subtract 70m per 10T below 190T. If CONF 3, subtract 90m per 10T below 190T. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 2 340 + 270 + 170 + 130 + 390 + 120 + 150 - 110 + 350 3 2 560 + 310 + 190 + 150 + 430 + 130 + 190 - 120 + 430 FULL 2 410 + 270 + 170 + 130 + 400 + 110 + 150 - 120 + 160 3 2 630 + 310 + 190 + 150 + 430 + 130 + 200 - 140 + 190 FULL 2 460 + 270 + 170 + 130 + 400 + 110 + 150 - 60 + 150 3 2 690 + 310 + 180 + 150 + 440 + 130 + 200 - 90 + 180 (1) Automatic Landing correction: if CONF FULL, add 340m. If CONF 3, add 330m. (2) Weight correction: if CONF FULL, subtract 100m per 10T below 190T. If CONF 3, subtract 130m per 10T below 190T. 1 - POOR Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 3 600 + 270 + 170 + 170 + 570 + 150 + 730 - 300 + 350 3 3 920 + 310 + 180 + 180 + 600 + 160 + 860 - 360 + 430 FULL 3 670 + 270 + 160 + 170 + 580 + 140 + 740 - 320 + 160 3 3 990 + 300 + 180 + 180 + 600 + 160 + 870 - 380 + 190 FULL 3 710 + 270 + 170 + 170 + 580 + 150 + 740 - 330 + 150 3 4 040 + 310 + 180 + 190 + 610 + 160 + 860 - 390 + 180 (1) Automatic Landing correction: if CONF FULL, add 340m. If CONF 3, add 330m. (2) Weight correction: if CONF FULL, subtract 130m per 10T below 190T. If CONF 3, subtract 160m per 10T below 190T. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-D 3/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK LANDING DISTANCE WITHOUT FAILURE Ident.: PER-D-00014090.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine (1) reverse thrust, manual landing , VAPP=VLS without APPR COR. 6 - DRY Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope + 70 + 40 + 120 + 40 (2) WGT FULL 1 310 + 150 SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied + 20 0 + 670 3 1 360 + 160 + 80 + 50 + 130 + 40 + 20 0 + 790 FULL 1 670 + 120 + 100 + 60 + 150 + 50 + 20 0 + 70 3 1 750 + 130 + 100 + 60 + 160 + 50 + 20 0 + 80 FULL 2 220 + 170 + 130 + 80 + 220 + 70 + 30 - 10 + 110 3 2 340 + 170 + 140 + 80 + 220 + 70 + 40 - 10 + 110 (1) Automatic Landing correction: if CONF FULL, add 230m. If CONF 3, add 200m. (2) Weight correction: if CONF FULL, subtract 40m per 10T below 190T. If CONF 3, subtract 50m per 10T below 190T. 5 - GOOD Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 1 600 + 170 + 120 + 80 + 220 + 70 + 50 - 20 + 490 3 1 700 + 190 + 130 + 90 + 240 + 70 + 50 - 20 + 590 FULL 1 760 + 180 + 120 + 80 + 220 + 70 + 50 - 10 + 110 3 1 870 + 190 + 130 + 80 + 240 + 80 + 60 - 20 + 130 FULL 2 220 + 170 + 130 + 80 + 220 + 70 + 30 - 10 + 110 3 2 340 + 190 + 140 + 80 + 220 + 70 + 40 - 10 + 110 (1) Automatic Landing correction: if CONF FULL, add 270m. If CONF 3, add 240m. (2) Weight correction: if CONF FULL, subtract 60m per 10T below 190T. If CONF 3, subtract 80m per 10T below 190T. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 1 830 + 140 + 100 + 70 + 200 + 60 + 60 - 40 + 550 3 1 920 + 150 + 110 + 70 + 200 + 70 + 70 - 50 + 670 FULL 1 980 + 140 + 110 + 70 + 200 + 60 + 70 - 50 + 100 3 2 090 + 140 + 110 + 70 + 210 + 70 + 80 - 60 + 110 FULL 2 230 + 170 + 130 + 80 + 220 + 70 + 50 - 10 + 110 3 2 340 + 170 + 140 + 80 + 220 + 80 + 60 - 10 + 110 (1) Automatic Landing correction: if CONF FULL, add 260m. If CONF 3, add 230m. (2) Weight correction: if CONF FULL, subtract 60m per 10T below 190T. If CONF 3, subtract 70m per 10T below 190T. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-D 4/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK 3 - MEDIUM Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 2 030 + 160 + 110 + 80 + 230 + 70 + 90 - 60 + 520 3 2 150 + 160 + 120 + 80 + 240 + 70 + 100 - 60 + 630 FULL 2 170 + 160 + 110 + 80 + 240 + 70 + 100 - 80 + 110 3 2 300 + 160 + 120 + 90 + 240 + 80 + 110 - 90 + 130 FULL 2 310 + 170 + 130 + 90 + 250 + 70 + 90 - 30 + 120 3 2 440 + 170 + 130 + 90 + 250 + 80 + 110 - 50 + 130 (1) Automatic Landing correction: if CONF FULL, add 270m. If CONF 3, add 240m. (2) Weight correction: if CONF FULL, subtract 70m per 10T below 190T. If CONF 3, subtract 80m per 10T below 190T. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 2 350 + 280 + 170 + 130 + 390 + 110 + 140 - 70 + 360 3 2 560 + 310 + 190 + 150 + 420 + 130 + 190 - 90 + 440 FULL 2 410 + 280 + 170 + 140 + 390 + 110 + 150 - 90 + 170 3 2 630 + 310 + 190 + 150 + 420 + 130 + 190 - 110 + 200 FULL 2 460 + 280 + 170 + 140 + 390 + 110 + 150 - 50 + 170 3 2 690 + 310 + 180 + 150 + 430 + 120 + 200 - 80 + 190 (1) Automatic Landing correction: if CONF FULL, add 310m. If CONF 3, add 290m. (2) Weight correction: if CONF FULL, subtract 100m per 10T below 190T. If CONF 3, subtract 130m per 10T below 190T. 1 - POOR Corrections on Landing Distance (m) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF SPD ALT WIND TEMP REF DIST Per 10T (m) for above Per 5kt 190T 190T Per 1000ft above SL Per 5kt TW Per 10°C Per 1% above Down ISA Slope (2) WGT SLOPE REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 3 550 + 290 + 160 + 170 + 570 + 130 + 670 - 220 + 360 3 3 850 + 310 + 180 + 180 + 590 + 150 + 780 - 260 + 440 FULL 3 610 + 290 + 160 + 170 + 570 + 140 + 680 - 230 + 170 3 3 920 + 310 + 180 + 180 + 600 + 150 + 790 - 270 + 200 FULL 3 650 + 290 + 160 + 170 + 570 + 140 + 670 - 230 + 170 3 3 970 + 310 + 180 + 190 + 600 + 150 + 790 - 280 + 190 (1) Automatic Landing correction: if CONF FULL, add 300m. If CONF 3, add 280m. (2) Weight correction: if CONF FULL, subtract 130m per 10T below 190T. If CONF 3, subtract 150m per 10T below 190T. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 1/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-24-00015147.0001001 / 28 FEB 14 Applicable to: ALL Ident.: PER-24-00014126.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 ELECTRICAL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 410 + 130 + 90 + 50 + 130 + 40 + 20 INOP + 640 3 5 1 490 + 140 + 80 + 50 + 140 + 40 + 20 INOP + 740 FULL 0 1 410 + 130 + 90 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 490 + 140 + 80 + 50 + 140 + 40 + 20 - 10 + 740 DC ESS BUS FAULT with FULL Ice Accretion 3 10 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 440 15 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 FULL 10 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 440 3 15 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 3 5 1 490 + 140 + 80 + 50 + 140 + 40 + 20 INOP + 740 REV OVW DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 790 + 190 + 150 + 90 + 250 + 80 + 60 INOP + 400 3 5 1 940 + 210 + 160 + 100 + 270 + 90 + 80 INOP + 480 FULL 0 1 790 + 190 + 150 + 90 + 250 + 80 + 60 - 10 + 400 3 5 1 940 + 210 + 160 + 100 + 270 + 90 + 80 - 20 + 480 DC ESS BUS FAULT with FULL Ice Accretion 3 10 1 860 + 180 + 130 + 90 + 240 + 80 + 50 - 50 + 260 15 2 010 + 200 + 140 + 100 + 250 + 90 + 60 - 60 + 320 FULL 10 1 860 + 180 + 130 + 90 + 240 + 80 + 50 - 50 + 260 3 15 2 010 + 200 + 140 + 100 + 250 + 90 + 60 - 60 + 320 3 5 1 940 + 210 + 160 + 100 + 270 + 90 + 80 INOP + 480 DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 2/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ELECTRICAL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 040 + 140 + 130 + 80 + 220 + 70 + 90 INOP + 490 3 5 2 190 + 140 + 130 + 80 + 230 + 70 + 100 INOP + 590 FULL 0 2 040 + 140 + 130 + 80 + 220 + 70 + 90 - 80 + 490 3 5 2 190 + 140 + 130 + 80 + 230 + 70 + 100 - 100 + 590 DC ESS BUS FAULT with FULL Ice Accretion 3 10 2 060 + 130 + 110 + 70 + 210 + 70 + 70 - 80 + 340 15 2 200 + 140 + 110 + 80 + 210 + 70 + 80 - 100 + 430 FULL 10 2 060 + 130 + 110 + 70 + 210 + 70 + 70 - 80 + 340 3 15 2 200 + 140 + 110 + 80 + 210 + 70 + 80 - 100 + 430 3 5 2 190 + 140 + 130 + 80 + 230 + 70 + 100 INOP + 590 REV OVW DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m 3 - MEDIUM Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 310 + 160 + 140 + 90 + 270 + 80 + 130 INOP + 450 3 5 2 480 + 170 + 150 + 90 + 270 + 90 + 150 INOP + 540 FULL 0 2 310 + 160 + 140 + 90 + 270 + 80 + 130 - 140 + 450 3 5 2 480 + 170 + 150 + 90 + 270 + 90 + 150 - 170 + 540 DC ESS BUS FAULT with FULL Ice Accretion 3 10 2 290 + 150 + 110 + 90 + 240 + 70 + 100 - 110 + 310 15 2 450 + 160 + 120 + 100 + 250 + 80 + 110 - 130 + 390 FULL 10 2 290 + 150 + 110 + 90 + 240 + 70 + 100 - 110 + 310 3 15 2 450 + 160 + 120 + 100 + 250 + 80 + 110 - 130 + 390 3 5 2 480 + 170 + 150 + 90 + 270 + 90 + 150 INOP + 540 DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 3/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ELECTRICAL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 760 + 320 + 220 + 160 + 490 + 140 + 230 INOP + 220 3 5 3 100 + 350 + 250 + 180 + 540 + 170 + 310 INOP + 280 FULL 0 2 760 + 320 + 220 + 160 + 490 + 140 + 230 - 160 + 220 3 5 3 100 + 350 + 250 + 180 + 540 + 170 + 310 - 230 + 280 DC ESS BUS FAULT with FULL Ice Accretion 3 10 2 720 + 280 + 160 + 150 + 410 + 120 + 160 - 150 + 160 15 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 FULL 10 2 720 + 280 + 160 + 150 + 410 + 120 + 160 - 150 + 160 3 15 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 3 5 3 100 + 350 + 250 + 180 + 540 + 170 + 310 INOP + 280 REV OVW DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE DC BUS 1+2 FAULT DC BUS 2 FAULT (2) WGT SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 Landing Distance greater than 6 000 m for all conditions 3 5 Landing Distance greater than 6 000 m for all conditions FULL 0 Landing Distance greater than 6 000 m for all conditions 3 5 Landing Distance greater than 6 000 m for all conditions DC ESS BUS FAULT with FULL Ice Accretion 3 10 3 970 + 280 + 170 + 180 + 590 + 160 + 740 - 430 + 160 15 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 FULL 10 3 970 + 280 + 170 + 180 + 590 + 160 + 740 - 430 + 160 3 15 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 3 5 DC ESS BUS SHED with Ice Accretion EMER CONFIG Landing Distance greater than 6 000 m for all conditions (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 4/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-24-00014126.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 ELECTRICAL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE DC BUS 1+2 FAULT DC BUS 2 FAULT (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 410 + 140 + 90 + 50 + 130 + 50 + 20 INOP + 640 3 5 1 490 + 150 + 80 + 50 + 130 + 40 + 20 INOP + 740 FULL 0 1 410 + 140 + 90 + 50 + 130 + 50 + 20 INOP + 640 5 1 490 + 150 + 80 + 50 + 130 + 40 + 20 INOP + 740 DC ESS BUS FAULT with FULL Ice Accretion 3 10 1 480 + 160 + 80 + 50 + 130 + 50 + 20 - 10 + 440 15 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 FULL 10 1 480 + 160 + 80 + 50 + 130 + 50 + 20 - 10 + 440 3 15 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 3 5 1 490 + 150 + 80 + 50 + 130 + 40 + 20 INOP + 740 REV OVW DC ESS BUS SHED with Ice Accretion EMER CONFIG 3 (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 790 + 210 + 150 + 100 + 250 + 80 + 60 INOP + 400 3 5 1 950 + 230 + 160 + 110 + 280 + 90 + 80 INOP + 470 FULL 0 1 790 + 210 + 150 + 100 + 250 + 80 + 60 INOP + 400 3 5 1 950 + 230 + 160 + 110 + 280 + 90 + 80 INOP + 470 DC ESS BUS FAULT with FULL Ice Accretion 3 10 1 870 + 200 + 130 + 90 + 240 + 80 + 50 - 20 + 260 15 2 030 + 220 + 130 + 110 + 250 + 80 + 60 - 30 + 320 FULL 10 1 870 + 200 + 130 + 90 + 240 + 80 + 50 - 20 + 260 3 15 2 030 + 220 + 130 + 110 + 250 + 80 + 60 - 30 + 320 3 5 1 950 + 230 + 160 + 110 + 280 + 90 + 80 INOP + 470 DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 5/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ELECTRICAL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 040 + 150 + 130 + 80 + 220 + 70 + 90 INOP + 490 3 5 2 180 + 160 + 130 + 80 + 230 + 80 + 100 INOP + 580 FULL 0 2 040 + 150 + 130 + 80 + 220 + 70 + 90 INOP + 490 3 5 2 180 + 160 + 130 + 80 + 230 + 80 + 100 INOP + 580 DC ESS BUS FAULT with FULL Ice Accretion 3 10 2 070 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 340 15 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 FULL 10 2 070 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 340 3 15 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 3 5 2 180 + 160 + 130 + 80 + 230 + 80 + 100 INOP + 580 REV OVW DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m 3 - MEDIUM Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 300 + 170 + 140 + 90 + 260 + 80 + 130 INOP + 450 3 5 2 480 + 180 + 150 + 100 + 280 + 80 + 150 INOP + 540 FULL 0 2 300 + 170 + 140 + 90 + 260 + 80 + 130 INOP + 450 3 5 2 480 + 180 + 150 + 100 + 280 + 80 + 150 INOP + 540 DC ESS BUS FAULT with FULL Ice Accretion 3 10 2 290 + 160 + 120 + 90 + 240 + 80 + 90 - 80 + 310 15 2 460 + 170 + 120 + 100 + 240 + 80 + 110 - 100 + 390 FULL 10 2 290 + 160 + 120 + 90 + 240 + 80 + 90 - 80 + 310 3 15 2 460 + 170 + 120 + 100 + 240 + 80 + 110 - 100 + 390 3 5 2 480 + 180 + 150 + 100 + 280 + 80 + 150 INOP + 540 DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 6/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ELECTRICAL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 740 + 340 + 230 + 170 + 480 + 150 + 230 INOP + 220 3 5 3 100 + 380 + 250 + 200 + 540 + 170 + 310 INOP + 280 FULL 0 2 740 + 340 + 230 + 170 + 480 + 150 + 230 INOP + 220 3 5 3 100 + 380 + 250 + 200 + 540 + 170 + 310 INOP + 280 DC ESS BUS FAULT with FULL Ice Accretion 3 10 2 720 + 290 + 170 + 150 + 400 + 130 + 150 - 120 + 160 15 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 FULL 10 2 720 + 290 + 170 + 150 + 400 + 130 + 150 - 120 + 160 3 15 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 3 5 3 100 + 380 + 250 + 200 + 540 + 170 + 310 INOP + 280 REV OVW DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE DC BUS 1+2 FAULT DC BUS 2 FAULT (2) WGT SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 Landing Distance greater than 6 000 m for all conditions 3 5 Landing Distance greater than 6 000 m for all conditions FULL 0 Landing Distance greater than 6 000 m for all conditions 3 5 Landing Distance greater than 6 000 m for all conditions DC ESS BUS FAULT with FULL Ice Accretion 3 10 3 910 + 300 + 160 + 180 + 580 + 150 + 680 - 340 + 160 15 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 FULL 10 3 910 + 300 + 160 + 180 + 580 + 150 + 680 - 340 + 160 3 15 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 3 5 DC ESS BUS SHED with Ice Accretion EMER CONFIG Landing Distance greater than 6 000 m for all conditions (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 110m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 1/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-27-00014128.0074001 / 28 FEB 14 Applicable to: MSN 0700 FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 1 620 + 180 N/A + 60 + 130 + 50 + 30 - 10 + 690 STAB CTL FAULT with man trim available 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 L/R/L+R ELEV FAULT 2 20 1 620 + 180 N/A + 60 + 130 + 50 + 30 - 10 + 690 RUDDER JAM/ RUDDER FAULT 2 10 1 640 + 240 + 110 + 80 + 180 + 60 + 40 - 10 + 700 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 2 040 + 120 N/A + 90 + 180 + 80 + 50 - 40 + 470 ALTN/DIRECT LAW 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 YAW DAMPER FAULT 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 FULL 0 1 390 + 150 + 80 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 460 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 720 FULL 0 1 410 + 140 + 90 + 50 + 130 + 40 + 20 INOP + 640 3 5 1 490 + 150 + 80 + 50 + 130 + 40 + 20 INOP + 740 3 5 1 610 + 140 + 110 + 60 + 140 + 50 + 30 INOP + 820 FULL 0 1 370 + 150 + 80 + 50 + 120 + 40 + 20 - 10 + 630 3 5 1 450 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 710 FULL 0 1 430 + 140 + 90 + 50 + 130 + 40 + 20 - 10 + 640 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 500 + 150 + 90 + 50 + 130 + 50 + 30 - 10 + 740 FULL 0 1 400 + 140 + 80 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 10 + 730 FULL 0 1 430 + 140 + 90 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 500 + 150 + 90 + 50 + 130 + 50 + 30 - 10 + 740 FULL 0 1 500 + 130 + 100 + 50 + 140 + 40 + 30 - 10 + 680 3 5 1 570 + 140 + 100 + 60 + 140 + 50 + 30 - 20 + 790 FULL 0 1 540 + 130 + 110 + 60 + 140 + 50 + 30 - 20 + 710 3 5 1 610 + 140 + 110 + 60 + 140 + 50 + 30 - 20 + 820 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 20m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 2/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 150 + 240 N/A + 110 + 260 + 90 + 70 - 40 + 410 STAB CTL FAULT with man trim available 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 L/R/L+R ELEV FAULT 2 20 2 150 + 240 N/A + 110 + 260 + 100 + 70 - 40 + 410 RUDDER JAM/ RUDDER FAULT 2 10 2 200 + 300 + 180 + 140 + 320 + 110 + 110 - 50 + 400 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 2 730 + 100 N/A + 160 + 330 + 130 + 130 - 150 + 200 ALTN/DIRECT LAW 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 FULL 0 1 740 + 200 + 140 + 90 + 240 + 70 + 50 - 20 + 410 3 5 1 880 + 220 + 150 + 100 + 260 + 90 + 70 - 30 + 470 FULL 0 1 790 + 210 + 150 + 90 + 250 + 80 + 60 INOP + 410 3 5 1 940 + 230 + 160 + 110 + 270 + 90 + 70 INOP + 480 3 5 2 250 + 310 + 240 + 140 + 330 + 120 + 130 INOP + 570 FULL 0 1 710 + 190 + 130 + 90 + 240 + 70 + 50 - 20 + 400 3 5 1 850 + 210 + 140 + 100 + 250 + 80 + 60 - 30 + 460 FULL 0 1 820 + 210 + 150 + 100 + 260 + 80 + 60 - 30 + 410 3 5 1 970 + 240 + 170 + 110 + 270 + 100 + 80 - 40 + 480 FULL 0 1 770 + 200 + 140 + 90 + 250 + 70 + 50 - 20 + 410 3 5 1 920 + 220 + 150 + 100 + 270 + 80 + 70 - 30 + 470 FULL 0 1 820 + 210 + 150 + 100 + 260 + 80 + 60 - 30 + 410 3 5 1 970 + 240 + 170 + 110 + 270 + 100 + 80 - 40 + 480 FULL 0 1 970 + 250 + 200 + 110 + 280 + 100 + 90 - 40 + 440 3 5 2 130 + 270 + 210 + 120 + 310 + 110 + 110 - 60 + 530 FULL 0 2 080 + 280 + 230 + 120 + 310 + 110 + 110 - 60 + 480 3 5 2 250 + 310 + 240 + 140 + 330 + 120 + 130 - 70 + 570 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 3/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 320 + 150 N/A + 90 + 210 + 70 + 80 - 80 + 560 STAB CTL FAULT with man trim available 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 L/R/L+R ELEV FAULT 2 20 2 320 + 150 N/A + 90 + 210 + 70 + 80 - 80 + 560 RUDDER JAM/ RUDDER FAULT 2 10 2 390 + 220 + 150 + 120 + 270 + 90 + 120 - 90 + 530 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 2 850 + 70 N/A + 130 + 270 + 110 + 130 - 170 + 340 ALTN/DIRECT LAW 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 FULL 0 1 960 + 140 + 120 + 70 + 210 + 70 + 70 - 50 + 500 3 5 2 100 + 150 + 120 + 80 + 220 + 70 + 80 - 60 + 580 FULL 0 2 020 + 150 + 120 + 80 + 220 + 70 + 80 INOP + 500 3 5 2 160 + 160 + 130 + 90 + 220 + 70 + 90 INOP + 590 3 5 2 470 + 190 + 180 + 100 + 250 + 90 + 140 INOP + 680 FULL 0 1 930 + 140 + 110 + 70 + 210 + 60 + 70 - 50 + 490 3 5 2 060 + 150 + 120 + 80 + 210 + 70 + 80 - 60 + 570 FULL 0 2 050 + 150 + 130 + 80 + 220 + 70 + 80 - 60 + 500 3 5 2 190 + 160 + 130 + 90 + 220 + 80 + 90 - 80 + 590 FULL 0 1 990 + 150 + 120 + 80 + 210 + 70 + 80 - 50 + 500 3 5 2 130 + 150 + 120 + 80 + 220 + 70 + 90 - 70 + 580 FULL 0 2 050 + 150 + 130 + 80 + 220 + 70 + 80 - 60 + 500 3 5 2 190 + 160 + 130 + 90 + 220 + 80 + 90 - 80 + 590 FULL 0 2 210 + 170 + 160 + 90 + 230 + 80 + 110 - 90 + 540 3 5 2 350 + 180 + 160 + 100 + 240 + 90 + 120 - 110 + 640 FULL 0 2 330 + 190 + 180 + 100 + 250 + 80 + 120 - 110 + 570 3 5 2 470 + 190 + 180 + 100 + 250 + 90 + 140 - 130 + 680 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 30m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 4/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 590 + 180 N/A + 100 + 250 + 90 + 120 - 110 + 520 STAB CTL FAULT with man trim available 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 L/R/L+R ELEV FAULT 2 20 2 590 + 170 N/A + 100 + 250 + 90 + 120 - 110 + 510 RUDDER JAM/ RUDDER FAULT 2 10 2 660 + 250 + 170 + 130 + 310 + 110 + 170 - 120 + 480 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 3 160 + 80 N/A + 140 + 310 + 120 + 170 - 220 + 300 ALTN/DIRECT LAW 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 FULL 0 2 190 + 160 + 130 + 90 + 240 + 80 + 100 - 80 + 460 3 5 2 350 + 170 + 130 + 90 + 250 + 80 + 120 - 100 + 540 FULL 0 2 260 + 170 + 130 + 90 + 250 + 70 + 110 INOP + 460 3 5 2 430 + 180 + 140 + 100 + 260 + 80 + 130 INOP + 550 3 5 2 820 + 220 + 210 + 120 + 300 + 100 + 210 INOP + 640 FULL 0 2 150 + 160 + 120 + 80 + 240 + 70 + 100 - 70 + 450 3 5 2 310 + 170 + 120 + 90 + 250 + 80 + 110 - 90 + 520 FULL 0 2 290 + 180 + 140 + 90 + 250 + 80 + 120 - 100 + 460 3 5 2 470 + 180 + 140 + 100 + 270 + 80 + 140 - 120 + 550 FULL 0 2 220 + 170 + 130 + 90 + 240 + 80 + 110 - 80 + 460 3 5 2 390 + 180 + 140 + 100 + 260 + 80 + 130 - 110 + 540 FULL 0 2 290 + 180 + 140 + 90 + 250 + 80 + 120 - 100 + 460 3 5 2 470 + 180 + 140 + 100 + 270 + 80 + 140 - 120 + 550 FULL 0 2 500 + 200 + 170 + 110 + 280 + 90 + 150 - 140 + 500 3 5 2 670 + 200 + 180 + 110 + 280 + 100 + 170 - 160 + 600 FULL 0 2 640 + 210 + 200 + 110 + 290 + 100 + 180 - 160 + 530 3 5 2 820 + 220 + 210 + 120 + 300 + 100 + 210 - 180 + 640 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 5/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 3 290 + 350 N/A + 180 + 450 + 160 + 250 - 180 + 280 STAB CTL FAULT with man trim available 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 L/R/L+R ELEV FAULT 2 20 3 290 + 350 N/A + 180 + 450 + 160 + 250 - 180 + 280 RUDDER JAM/ RUDDER FAULT 2 10 3 220 + 440 + 230 + 220 + 520 + 170 + 310 - 180 + 240 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 3 850 + 220 N/A + 230 + 530 + 190 + 340 - 360 + 130 ALTN/DIRECT LAW 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 FULL 0 2 600 + 310 + 190 + 150 + 420 + 130 + 180 - 110 + 250 3 5 2 890 + 350 + 220 + 170 + 450 + 150 + 230 - 140 + 300 FULL 0 2 690 + 330 + 210 + 160 + 440 + 130 + 200 INOP + 250 3 5 3 020 + 370 + 230 + 190 + 480 + 160 + 270 INOP + 310 3 5 3 770 + 510 + 360 + 270 + 630 + 210 + 540 INOP + 390 FULL 0 2 520 + 300 + 180 + 150 + 410 + 120 + 160 - 100 + 240 3 5 2 810 + 330 + 200 + 170 + 440 + 140 + 210 - 130 + 290 FULL 0 2 740 + 340 + 220 + 160 + 450 + 140 + 210 - 130 + 250 3 5 3 080 + 380 + 240 + 190 + 490 + 160 + 280 - 170 + 310 FULL 0 2 640 + 320 + 200 + 160 + 430 + 130 + 190 - 120 + 250 3 5 2 950 + 360 + 220 + 180 + 470 + 150 + 250 - 150 + 300 FULL 0 2 740 + 340 + 220 + 160 + 450 + 140 + 210 - 130 + 250 3 5 3 080 + 380 + 240 + 190 + 490 + 160 + 280 - 170 + 310 FULL 0 3 080 + 400 + 280 + 200 + 520 + 170 + 300 - 180 + 280 3 5 3 470 + 450 + 300 + 230 + 570 + 190 + 410 - 230 + 350 FULL 0 3 340 + 460 + 330 + 230 + 570 + 190 + 390 - 220 + 310 3 5 3 770 + 510 + 360 + 270 + 630 + 210 + 540 - 290 + 390 (1) Automatic Landing correction: add 190m - (2) Weight correction: subtract 90m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 6/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 4 640 + 360 N/A + 220 + 620 + 170 + 890 - 460 + 280 STAB CTL FAULT with man trim available 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 L/R/L+R ELEV FAULT 2 20 4 630 + 360 N/A + 220 + 620 + 180 + 890 - 460 + 280 RUDDER JAM/ RUDDER FAULT 2 10 4 580 + 440 + 210 + 260 + 690 + 190 + 990 - 470 + 240 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 5 160 + 240 N/A + 250 + 650 + 210 + 910 - 700 + 130 ALTN/DIRECT LAW 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 FULL 0 3 890 + 320 + 190 + 190 + 600 + 150 + 770 - 370 + 260 3 5 4 270 + 350 + 200 + 210 + 620 + 170 + 900 - 440 + 300 FULL 0 4 020 + 330 + 200 + 200 + 610 + 160 + 820 INOP + 260 3 5 4 460 + 370 + 220 + 220 + 640 + 180 + 980 INOP + 310 3 5 FULL 0 3 760 + 310 + 170 + 180 + 580 + 140 + 720 - 350 + 240 3 5 4 140 + 330 + 190 + 200 + 610 + 160 + 840 - 410 + 290 FULL 0 4 090 + 340 + 210 + 200 + 610 + 170 + 850 - 420 + 250 3 5 4 540 + 380 + 230 + 230 + 650 + 180 + 1 020 - 500 + 310 FULL 0 3 950 + 330 + 190 + 190 + 600 + 160 + 790 - 390 + 250 Landing Distance greater than 6 000 m for all conditions 3 5 4 350 + 360 + 210 + 220 + 630 + 170 + 930 - 450 + 300 FULL 0 4 090 + 340 + 210 + 200 + 610 + 170 + 850 - 420 + 250 3 5 4 540 + 380 + 230 + 230 + 650 + 180 + 1 020 - 500 + 310 FULL 0 4 620 + 400 + 260 + 240 + 670 + 180 + 1 100 - 530 + 280 3 5 5 110 + 440 + 290 + 270 + 700 + 210 + 1 310 - 630 + 350 FULL 0 5 020 + 440 + 300 + 270 + 710 + 200 + 1 310 - 630 + 310 3 5 5 550 + 480 + 340 + 310 + 740 + 220 + 1 590 - 750 + 390 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 7/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-27-00014128.0068001 / 28 FEB 14 Applicable to: MSN 0968-1118 FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 1 610 + 170 N/A + 60 + 130 + 50 + 30 - 20 + 700 STAB CTL FAULT with man trim available 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 L/R/L+R ELEV FAULT 2 20 1 620 + 170 N/A + 50 + 130 + 50 + 30 - 20 + 690 RUDDER JAM/ RUDDER FAULT 2 10 1 640 + 230 + 110 + 80 + 190 + 60 + 40 - 30 + 700 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 2 040 + 120 N/A + 90 + 180 + 80 + 50 - 60 + 440 ALTN/DIRECT LAW 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 YAW DAMPER FAULT 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 FULL 0 1 380 + 140 + 80 + 50 + 120 + 40 + 20 - 20 + 640 3 5 1 460 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 730 FULL 0 1 410 + 130 + 80 + 50 + 130 + 40 + 20 INOP + 650 3 5 1 480 + 140 + 80 + 50 + 130 + 50 + 20 INOP + 750 3 5 1 600 + 130 + 110 + 60 + 140 + 50 + 30 INOP + 820 FULL 0 1 370 + 140 + 80 + 40 + 130 + 40 + 20 - 10 + 630 3 5 1 440 + 150 + 80 + 50 + 130 + 50 + 20 - 20 + 710 FULL 0 1 420 + 130 + 90 + 50 + 130 + 50 + 20 - 20 + 650 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 500 + 140 + 80 + 50 + 140 + 40 + 20 - 20 + 750 FULL 0 1 400 + 130 + 80 + 50 + 130 + 40 + 20 - 20 + 640 3 5 1 470 + 150 + 80 + 50 + 130 + 50 + 20 - 20 + 740 FULL 0 1 420 + 130 + 90 + 50 + 130 + 50 + 20 - 20 + 650 3 5 1 500 + 140 + 80 + 50 + 140 + 40 + 20 - 20 + 750 FULL 0 1 490 + 120 + 100 + 50 + 140 + 50 + 30 - 30 + 680 3 5 1 560 + 130 + 100 + 50 + 140 + 50 + 30 - 30 + 790 FULL 0 1 540 + 120 + 110 + 50 + 140 + 50 + 30 - 30 + 720 3 5 1 600 + 130 + 110 + 60 + 140 + 50 + 30 - 30 + 820 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 8/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 140 + 230 N/A + 110 + 260 + 100 + 70 - 70 + 420 STAB CTL FAULT with man trim available 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 L/R/L+R ELEV FAULT 2 20 2 140 + 230 N/A + 110 + 260 + 100 + 70 - 70 + 410 RUDDER JAM/ RUDDER FAULT 2 10 2 200 + 290 + 180 + 140 + 330 + 110 + 110 - 80 + 390 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 2 730 + 100 N/A + 160 + 330 + 130 + 130 - 210 + 180 ALTN/DIRECT LAW 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 FULL 0 1 730 + 190 + 140 + 90 + 240 + 80 + 50 - 40 + 420 3 5 1 870 + 200 + 150 + 90 + 250 + 90 + 70 - 50 + 480 FULL 0 1 780 + 190 + 150 + 90 + 250 + 80 + 60 INOP + 420 3 5 1 930 + 210 + 160 + 100 + 270 + 90 + 70 INOP + 490 3 5 2 230 + 280 + 230 + 130 + 330 + 120 + 130 INOP + 570 FULL 0 1 700 + 180 + 130 + 80 + 230 + 70 + 50 - 40 + 400 3 5 1 840 + 200 + 140 + 90 + 250 + 80 + 60 - 50 + 460 FULL 0 1 810 + 200 + 160 + 90 + 250 + 80 + 60 - 50 + 410 3 5 1 960 + 220 + 160 + 100 + 270 + 90 + 80 - 60 + 490 FULL 0 1 760 + 190 + 140 + 90 + 250 + 80 + 60 - 40 + 410 3 5 1 900 + 210 + 150 + 100 + 260 + 90 + 70 - 60 + 480 FULL 0 1 810 + 200 + 160 + 90 + 250 + 80 + 60 - 50 + 410 3 5 1 960 + 220 + 160 + 100 + 270 + 90 + 80 - 60 + 490 FULL 0 1 960 + 230 + 190 + 110 + 280 + 100 + 90 - 70 + 450 3 5 2 120 + 250 + 200 + 120 + 310 + 100 + 100 - 80 + 530 FULL 0 2 070 + 260 + 220 + 120 + 310 + 110 + 110 - 90 + 480 3 5 2 230 + 280 + 230 + 130 + 330 + 120 + 130 - 100 + 570 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 9/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 310 + 140 N/A + 80 + 210 + 80 + 90 - 100 + 570 STAB CTL FAULT with man trim available 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 L/R/L+R ELEV FAULT 2 20 2 310 + 140 N/A + 80 + 210 + 80 + 90 - 100 + 560 RUDDER JAM/ RUDDER FAULT 2 10 2 380 + 210 + 160 + 120 + 270 + 100 + 120 - 120 + 530 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 2 860 + 60 N/A + 130 + 270 + 100 + 130 - 230 + 320 ALTN/DIRECT LAW 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 FULL 0 1 950 + 140 + 120 + 70 + 210 + 70 + 70 - 80 + 500 3 5 2 090 + 140 + 120 + 80 + 220 + 70 + 80 - 90 + 580 FULL 0 2 010 + 140 + 120 + 80 + 210 + 70 + 80 INOP + 500 3 5 2 150 + 150 + 120 + 80 + 220 + 70 + 90 INOP + 600 3 5 2 460 + 170 + 180 + 100 + 250 + 90 + 140 INOP + 690 FULL 0 1 920 + 130 + 110 + 70 + 210 + 60 + 70 - 80 + 490 3 5 2 050 + 140 + 120 + 80 + 210 + 70 + 80 - 90 + 570 FULL 0 2 040 + 140 + 130 + 80 + 220 + 70 + 80 - 100 + 500 3 5 2 180 + 150 + 130 + 80 + 230 + 80 + 90 - 110 + 600 FULL 0 1 980 + 140 + 120 + 70 + 210 + 70 + 80 - 90 + 500 3 5 2 120 + 140 + 120 + 80 + 220 + 70 + 90 - 100 + 590 FULL 0 2 040 + 140 + 130 + 80 + 220 + 70 + 80 - 100 + 500 3 5 2 180 + 150 + 130 + 80 + 230 + 80 + 90 - 110 + 600 FULL 0 2 210 + 160 + 160 + 90 + 240 + 70 + 110 - 120 + 540 3 5 2 340 + 160 + 160 + 90 + 240 + 90 + 120 - 140 + 640 FULL 0 2 320 + 170 + 180 + 90 + 250 + 80 + 130 - 150 + 570 3 5 2 460 + 170 + 180 + 100 + 250 + 90 + 140 - 160 + 690 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 30m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 10/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 590 + 170 N/A + 100 + 250 + 90 + 120 - 150 + 520 STAB CTL FAULT with man trim available 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 L/R/L+R ELEV FAULT 2 20 2 590 + 170 N/A + 100 + 250 + 90 + 120 - 140 + 520 RUDDER JAM/ RUDDER FAULT 2 10 2 660 + 240 + 170 + 130 + 310 + 110 + 170 - 160 + 470 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 3 160 + 80 N/A + 150 + 310 + 120 + 180 - 300 + 280 ALTN/DIRECT LAW 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 FULL 0 2 190 + 150 + 120 + 90 + 250 + 70 + 110 - 120 + 460 3 5 2 340 + 160 + 130 + 90 + 250 + 80 + 120 - 130 + 540 FULL 0 2 250 + 160 + 140 + 90 + 250 + 80 + 120 INOP + 460 3 5 2 420 + 170 + 140 + 100 + 260 + 80 + 130 INOP + 550 3 5 2 810 + 200 + 200 + 120 + 300 + 100 + 210 INOP + 640 FULL 0 2 140 + 150 + 120 + 80 + 240 + 70 + 100 - 110 + 450 3 5 2 300 + 160 + 120 + 90 + 250 + 80 + 110 - 130 + 530 FULL 0 2 290 + 160 + 140 + 90 + 260 + 80 + 120 - 130 + 460 3 5 2 460 + 170 + 140 + 100 + 270 + 80 + 140 - 150 + 550 FULL 0 2 220 + 160 + 130 + 90 + 250 + 80 + 110 - 120 + 460 3 5 2 380 + 170 + 140 + 90 + 260 + 80 + 130 - 140 + 540 FULL 0 2 290 + 160 + 140 + 90 + 260 + 80 + 120 - 130 + 460 3 5 2 460 + 170 + 140 + 100 + 270 + 80 + 140 - 150 + 550 FULL 0 2 490 + 180 + 180 + 100 + 270 + 90 + 160 - 170 + 500 3 5 2 660 + 190 + 180 + 110 + 280 + 100 + 180 - 200 + 600 FULL 0 2 640 + 200 + 200 + 110 + 290 + 100 + 190 - 210 + 530 3 5 2 810 + 200 + 200 + 120 + 300 + 100 + 210 - 230 + 640 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 11/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 3 290 + 340 N/A + 180 + 460 + 160 + 260 - 230 + 270 STAB CTL FAULT with man trim available 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 L/R/L+R ELEV FAULT 2 20 3 290 + 340 N/A + 180 + 470 + 160 + 260 - 230 + 270 RUDDER JAM/ RUDDER FAULT 2 10 3 220 + 430 + 230 + 220 + 550 + 170 + 330 - 230 + 220 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 3 850 + 220 N/A + 230 + 540 + 200 + 350 - 480 + 120 ALTN/DIRECT LAW 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 FULL 0 2 590 + 300 + 200 + 150 + 430 + 130 + 180 - 140 + 250 3 5 2 880 + 330 + 210 + 170 + 470 + 150 + 240 - 180 + 300 FULL 0 2 690 + 320 + 210 + 160 + 450 + 130 + 200 INOP + 240 3 5 3 010 + 350 + 230 + 180 + 500 + 150 + 270 INOP + 310 3 5 3 750 + 480 + 360 + 260 + 660 + 220 + 560 INOP + 390 FULL 0 2 520 + 290 + 180 + 140 + 420 + 120 + 170 - 130 + 240 3 5 2 800 + 320 + 200 + 160 + 450 + 140 + 220 - 170 + 290 FULL 0 2 740 + 320 + 220 + 160 + 460 + 140 + 210 - 170 + 240 3 5 3 060 + 360 + 240 + 190 + 500 + 160 + 290 - 210 + 310 FULL 0 2 640 + 310 + 200 + 150 + 440 + 130 + 190 - 150 + 240 3 5 2 940 + 340 + 220 + 170 + 480 + 150 + 250 - 190 + 300 FULL 0 2 740 + 320 + 220 + 160 + 460 + 140 + 210 - 170 + 240 3 5 3 060 + 360 + 240 + 190 + 500 + 160 + 290 - 210 + 310 FULL 0 3 080 + 390 + 280 + 200 + 540 + 170 + 310 - 220 + 270 3 5 3 450 + 430 + 310 + 230 + 590 + 190 + 420 - 290 + 350 FULL 0 3 340 + 430 + 340 + 230 + 600 + 200 + 410 - 270 + 300 3 5 3 750 + 480 + 360 + 260 + 660 + 220 + 560 - 350 + 390 (1) Automatic Landing correction: add 230m - (2) Weight correction: subtract 90m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 12/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 4 740 + 340 N/A + 220 + 630 + 180 + 990 - 580 + 270 STAB CTL FAULT with man trim available 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 L/R/L+R ELEV FAULT 2 20 4 740 + 340 N/A + 220 + 630 + 180 + 990 - 580 + 270 RUDDER JAM/ RUDDER FAULT 2 10 4 680 + 430 + 220 + 260 + 710 + 200 + 1 100 - 590 + 220 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 5 220 + 240 N/A + 250 + 660 + 210 + 960 - 910 + 120 ALTN/DIRECT LAW 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 YAW DAMPER FAULT PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 FULL 0 3 960 + 300 + 190 + 190 + 610 + 160 + 850 - 470 + 250 3 5 4 340 + 320 + 210 + 210 + 630 + 180 + 990 - 540 + 300 FULL 0 4 110 + 310 + 200 + 200 + 620 + 160 + 920 INOP + 240 3 5 4 550 + 340 + 220 + 220 + 660 + 180 + 1 100 INOP + 310 3 5 FULL 0 3 820 + 290 + 190 + 180 + 590 + 150 + 780 - 430 + 240 3 5 4 200 + 310 + 200 + 200 + 620 + 170 + 920 - 510 + 280 FULL 0 4 180 + 320 + 210 + 200 + 630 + 170 + 950 - 520 + 240 3 5 4 630 + 350 + 230 + 230 + 660 + 180 + 1 130 - 620 + 310 FULL 0 4 030 + 300 + 200 + 190 + 620 + 160 + 880 - 480 + 240 Landing Distance greater than 6 000 m for all conditions 3 5 4 430 + 330 + 210 + 210 + 640 + 180 + 1 030 - 570 + 300 FULL 0 4 180 + 320 + 210 + 200 + 630 + 170 + 950 - 520 + 240 3 5 4 630 + 350 + 230 + 230 + 660 + 180 + 1 130 - 620 + 310 FULL 0 4 750 + 370 + 270 + 240 + 690 + 190 + 1 240 - 680 + 270 3 5 5 240 + 400 + 290 + 260 + 720 + 210 + 1 480 - 800 + 350 FULL 0 5 180 + 400 + 310 + 270 + 720 + 210 + 1 500 - 810 + 300 3 5 5 700 + 440 + 340 + 290 + 760 + 230 + 1 790 - 940 + 390 (1) Automatic Landing correction: add 220m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 13/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-27-00014128.0040001 / 28 FEB 14 Applicable to: MSN 0232-0361 FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 1 610 + 170 N/A + 60 + 130 + 50 + 30 - 20 + 700 STAB CTL FAULT with man trim available 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 L/R/L+R ELEV FAULT 2 20 1 620 + 170 N/A + 50 + 130 + 50 + 30 - 20 + 690 RUD TRV LIM FAULT 2 20 1 610 + 170 N/A + 60 + 130 + 50 + 30 - 20 + 700 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 1 660 + 100 N/A + 50 + 130 + 50 + 30 - 40 + 730 RUDDER JAM 2 20 1 830 + 240 N/A + 80 + 180 + 70 + 50 - 40 + 580 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 1 900 + 150 N/A + 80 + 180 + 60 + 50 - 70 + 610 ALTN/DIRECT LAW 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 YAW DAMPER FAULT 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 FULL 0 1 380 + 140 + 80 + 50 + 120 + 40 + 20 - 20 + 640 3 5 1 460 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 730 FULL 0 1 410 + 130 + 80 + 50 + 130 + 40 + 20 INOP + 650 3 5 1 480 + 140 + 80 + 50 + 130 + 50 + 20 INOP + 750 3 5 1 600 + 130 + 110 + 60 + 140 + 50 + 30 INOP + 820 FULL 0 1 370 + 140 + 80 + 40 + 130 + 40 + 20 - 10 + 630 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 440 + 150 + 80 + 50 + 130 + 50 + 20 - 20 + 710 FULL 0 1 420 + 130 + 90 + 50 + 130 + 50 + 20 - 20 + 650 3 5 1 500 + 140 + 80 + 50 + 140 + 40 + 20 - 20 + 750 FULL 0 1 400 + 130 + 80 + 50 + 130 + 40 + 20 - 20 + 640 3 5 1 470 + 150 + 80 + 50 + 130 + 50 + 20 - 20 + 740 FULL 0 1 420 + 130 + 90 + 50 + 130 + 50 + 20 - 20 + 650 3 5 1 500 + 140 + 80 + 50 + 140 + 40 + 20 - 20 + 750 FULL 0 1 490 + 120 + 100 + 50 + 140 + 50 + 30 - 30 + 680 3 5 1 560 + 130 + 100 + 50 + 140 + 50 + 30 - 30 + 790 FULL 0 1 540 + 120 + 110 + 50 + 140 + 50 + 30 - 30 + 720 3 5 1 600 + 130 + 110 + 60 + 140 + 50 + 30 - 30 + 820 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 14/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 140 + 220 N/A + 110 + 260 + 100 + 70 - 70 + 420 STAB CTL FAULT with man trim available 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 L/R/L+R ELEV FAULT 2 20 2 140 + 220 N/A + 110 + 260 + 100 + 70 - 70 + 410 RUD TRV LIM FAULT 2 20 2 140 + 220 N/A + 110 + 260 + 100 + 70 - 70 + 420 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 2 250 + 100 N/A + 110 + 270 + 100 + 80 - 150 + 420 RUDDER JAM 2 20 2 470 + 300 N/A + 150 + 320 + 120 + 120 - 110 + 290 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 2 620 + 160 N/A + 160 + 350 + 130 + 150 - 240 + 280 ALTN/DIRECT LAW 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 YAW DAMPER FAULT 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 FULL 0 1 730 + 180 + 140 + 90 + 240 + 80 + 50 - 40 + 420 3 5 1 870 + 200 + 150 + 90 + 250 + 90 + 70 - 50 + 480 FULL 0 1 780 + 190 + 150 + 90 + 250 + 80 + 60 INOP + 420 3 5 1 930 + 210 + 160 + 100 + 270 + 90 + 70 INOP + 490 3 5 2 230 + 280 + 230 + 130 + 330 + 120 + 130 INOP + 570 FULL 0 1 700 + 180 + 130 + 80 + 230 + 70 + 50 - 40 + 400 3 5 1 840 + 200 + 140 + 90 + 250 + 80 + 60 - 50 + 460 FULL 0 1 810 + 200 + 160 + 90 + 250 + 80 + 60 - 50 + 410 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 960 + 220 + 160 + 100 + 270 + 90 + 80 - 60 + 490 FULL 0 1 760 + 190 + 140 + 90 + 250 + 80 + 60 - 40 + 410 3 5 1 900 + 210 + 150 + 100 + 260 + 90 + 70 - 60 + 480 FULL 0 1 810 + 200 + 160 + 90 + 250 + 80 + 60 - 50 + 410 3 5 1 960 + 220 + 160 + 100 + 270 + 90 + 80 - 60 + 490 FULL 0 1 960 + 230 + 190 + 110 + 280 + 100 + 90 - 70 + 450 3 5 2 120 + 250 + 200 + 120 + 310 + 100 + 100 - 80 + 530 FULL 0 2 070 + 250 + 220 + 120 + 310 + 110 + 110 - 90 + 480 3 5 2 230 + 280 + 230 + 130 + 330 + 120 + 130 - 100 + 570 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 20m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 15/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 310 + 140 N/A + 80 + 210 + 80 + 90 - 100 + 570 STAB CTL FAULT with man trim available 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 L/R/L+R ELEV FAULT 2 20 2 310 + 140 N/A + 80 + 210 + 80 + 90 - 100 + 560 RUD TRV LIM FAULT 2 20 2 310 + 140 N/A + 80 + 210 + 80 + 90 - 100 + 570 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 2 410 + 60 N/A + 90 + 220 + 80 + 100 - 180 + 580 RUDDER JAM 2 20 2 630 + 210 N/A + 120 + 270 + 100 + 130 - 140 + 430 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 2 780 + 110 N/A + 130 + 280 + 100 + 150 - 270 + 430 ALTN/DIRECT LAW 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 YAW DAMPER FAULT 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 FULL 0 1 950 + 130 + 120 + 70 + 210 + 70 + 70 - 80 + 500 3 5 2 090 + 140 + 120 + 80 + 220 + 70 + 80 - 90 + 580 FULL 0 2 010 + 140 + 120 + 80 + 210 + 70 + 80 INOP + 500 3 5 2 150 + 140 + 120 + 80 + 220 + 70 + 90 INOP + 600 3 5 2 460 + 170 + 180 + 100 + 250 + 90 + 140 INOP + 690 FULL 0 1 920 + 130 + 110 + 70 + 210 + 60 + 70 - 80 + 490 3 5 2 050 + 140 + 120 + 80 + 210 + 70 + 80 - 90 + 570 FULL 0 2 040 + 140 + 130 + 80 + 220 + 70 + 80 - 100 + 500 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 180 + 150 + 130 + 80 + 230 + 80 + 90 - 110 + 600 FULL 0 1 980 + 140 + 120 + 70 + 210 + 70 + 80 - 90 + 500 3 5 2 120 + 140 + 120 + 80 + 220 + 70 + 90 - 100 + 590 FULL 0 2 040 + 140 + 130 + 80 + 220 + 70 + 80 - 100 + 500 3 5 2 180 + 150 + 130 + 80 + 230 + 80 + 90 - 110 + 600 FULL 0 2 210 + 160 + 160 + 90 + 240 + 70 + 110 - 120 + 540 3 5 2 340 + 160 + 160 + 90 + 240 + 90 + 120 - 140 + 640 FULL 0 2 320 + 170 + 180 + 90 + 250 + 80 + 130 - 150 + 570 3 5 2 460 + 170 + 180 + 100 + 250 + 90 + 140 - 160 + 690 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 16/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 590 + 160 N/A + 100 + 250 + 90 + 120 - 150 + 520 STAB CTL FAULT with man trim available 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 L/R/L+R ELEV FAULT 2 20 2 590 + 160 N/A + 100 + 250 + 90 + 120 - 140 + 520 RUD TRV LIM FAULT 2 20 2 590 + 160 N/A + 100 + 250 + 90 + 120 - 150 + 520 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 2 700 + 80 N/A + 100 + 250 + 100 + 140 - 250 + 530 RUDDER JAM 2 20 2 930 + 240 N/A + 140 + 310 + 110 + 180 - 190 + 380 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 3 100 + 130 N/A + 150 + 330 + 120 + 210 - 350 + 380 ALTN/DIRECT LAW 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 YAW DAMPER FAULT 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 FULL 0 2 190 + 150 + 120 + 90 + 250 + 70 + 110 - 120 + 460 3 5 2 340 + 160 + 130 + 90 + 250 + 80 + 120 - 130 + 540 FULL 0 2 250 + 160 + 140 + 90 + 250 + 80 + 120 INOP + 460 3 5 2 420 + 170 + 140 + 100 + 260 + 80 + 130 INOP + 550 3 5 2 810 + 200 + 200 + 120 + 300 + 100 + 210 INOP + 640 FULL 0 2 140 + 150 + 120 + 80 + 240 + 70 + 100 - 110 + 450 3 5 2 300 + 160 + 120 + 90 + 250 + 80 + 110 - 130 + 530 FULL 0 2 290 + 160 + 140 + 90 + 260 + 80 + 120 - 130 + 460 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 460 + 170 + 140 + 100 + 270 + 80 + 140 - 150 + 550 FULL 0 2 220 + 160 + 130 + 90 + 250 + 80 + 110 - 120 + 460 3 5 2 380 + 160 + 140 + 90 + 260 + 80 + 130 - 140 + 540 FULL 0 2 290 + 160 + 140 + 90 + 260 + 80 + 120 - 130 + 460 3 5 2 460 + 170 + 140 + 100 + 270 + 80 + 140 - 150 + 550 FULL 0 2 490 + 180 + 180 + 100 + 270 + 90 + 160 - 170 + 500 3 5 2 660 + 190 + 180 + 110 + 280 + 100 + 180 - 200 + 600 FULL 0 2 640 + 200 + 200 + 110 + 290 + 100 + 190 - 210 + 530 3 5 2 810 + 200 + 200 + 120 + 300 + 100 + 210 - 230 + 640 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 20m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 17/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 3 290 + 340 N/A + 180 + 460 + 160 + 260 - 230 + 270 STAB CTL FAULT with man trim available 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 L/R/L+R ELEV FAULT 2 20 3 290 + 340 N/A + 180 + 470 + 160 + 260 - 230 + 270 RUD TRV LIM FAULT 2 20 3 290 + 340 N/A + 180 + 460 + 160 + 260 - 230 + 270 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 3 500 + 210 N/A + 190 + 490 + 180 + 310 - 470 + 270 RUDDER JAM 2 20 3 570 + 440 N/A + 230 + 550 + 180 + 350 - 280 + 170 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 3 830 + 310 N/A + 250 + 590 + 200 + 430 - 560 + 170 ALTN/DIRECT LAW 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 YAW DAMPER FAULT 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 FULL 0 2 590 + 300 + 200 + 150 + 430 + 130 + 180 - 140 + 250 3 5 2 880 + 330 + 210 + 170 + 470 + 150 + 240 - 180 + 300 FULL 0 2 690 + 310 + 210 + 160 + 450 + 130 + 200 INOP + 240 3 5 3 010 + 350 + 230 + 180 + 500 + 150 + 270 INOP + 310 3 5 3 750 + 470 + 360 + 260 + 660 + 220 + 560 INOP + 390 FULL 0 2 520 + 280 + 180 + 140 + 420 + 120 + 170 - 130 + 240 3 5 2 800 + 310 + 200 + 160 + 450 + 140 + 220 - 170 + 290 FULL 0 2 740 + 320 + 220 + 160 + 460 + 140 + 210 - 170 + 240 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 3 060 + 360 + 240 + 190 + 500 + 160 + 290 - 210 + 310 FULL 0 2 640 + 310 + 200 + 150 + 440 + 130 + 190 - 150 + 240 3 5 2 940 + 340 + 220 + 170 + 480 + 150 + 250 - 190 + 300 FULL 0 2 740 + 320 + 220 + 160 + 460 + 140 + 210 - 170 + 240 3 5 3 060 + 360 + 240 + 190 + 500 + 160 + 290 - 210 + 310 FULL 0 3 080 + 380 + 280 + 200 + 540 + 170 + 310 - 220 + 270 3 5 3 450 + 420 + 310 + 230 + 590 + 190 + 420 - 290 + 350 FULL 0 3 340 + 430 + 340 + 230 + 600 + 200 + 410 - 270 + 300 3 5 3 750 + 470 + 360 + 260 + 660 + 220 + 560 - 350 + 390 (1) Automatic Landing correction: add 230m - (2) Weight correction: subtract 60m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 18/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 4 740 + 330 N/A + 220 + 630 + 180 + 990 - 580 + 270 STAB CTL FAULT with man trim available 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 L/R/L+R ELEV FAULT 2 20 4 740 + 330 N/A + 220 + 630 + 180 + 990 - 580 + 270 RUD TRV LIM FAULT 2 20 4 740 + 330 N/A + 220 + 630 + 180 + 990 - 580 + 270 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 4 970 + 220 N/A + 210 + 610 + 190 + 990 - 940 + 270 RUDDER JAM 2 20 5 030 + 440 N/A + 270 + 700 + 210 + 1 100 - 640 + 180 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 5 310 + 320 N/A + 270 + 690 + 220 + 1 140 - 1 070 + 170 ALTN/DIRECT LAW 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 YAW DAMPER FAULT 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 FULL 0 3 960 + 300 + 190 + 190 + 610 + 160 + 850 - 470 + 250 3 5 4 340 + 320 + 210 + 210 + 630 + 180 + 990 - 540 + 300 FULL 0 4 110 + 310 + 200 + 200 + 620 + 160 + 920 INOP + 240 3 5 4 550 + 340 + 220 + 220 + 660 + 180 + 1 100 INOP + 310 3 5 FULL 0 3 820 + 280 + 190 + 180 + 590 + 150 + 780 - 430 + 240 3 5 4 200 + 310 + 200 + 200 + 620 + 170 + 920 - 510 + 280 FULL 0 4 180 + 310 + 210 + 200 + 630 + 170 + 950 - 520 + 240 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT Landing Distance greater than 6 000 m for all conditions 3 5 4 630 + 340 + 230 + 230 + 660 + 180 + 1 130 - 620 + 310 FULL 0 4 030 + 300 + 200 + 190 + 620 + 160 + 880 - 480 + 240 3 5 4 430 + 330 + 210 + 210 + 640 + 180 + 1 030 - 570 + 300 FULL 0 4 180 + 310 + 210 + 200 + 630 + 170 + 950 - 520 + 240 3 5 4 630 + 340 + 230 + 230 + 660 + 180 + 1 130 - 620 + 310 FULL 0 4 750 + 360 + 270 + 240 + 690 + 190 + 1 240 - 680 + 270 3 5 5 240 + 390 + 290 + 260 + 720 + 210 + 1 480 - 800 + 350 FULL 0 5 180 + 400 + 310 + 270 + 720 + 210 + 1 500 - 810 + 300 3 5 5 700 + 430 + 340 + 290 + 760 + 230 + 1 790 - 940 + 390 (1) Automatic Landing correction: add 220m - (2) Weight correction: subtract 90m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 19/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-27-00014128.0029001 / 28 FEB 14 Applicable to: MSN 0466-0472 FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 1 620 + 180 N/A + 60 + 130 + 50 + 30 - 10 + 690 STAB CTL FAULT with man trim available 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 L/R/L+R ELEV FAULT 2 20 1 620 + 180 N/A + 60 + 130 + 50 + 30 - 10 + 690 RUD TRV LIM FAULT 2 20 1 620 + 180 N/A + 60 + 130 + 50 + 30 - 10 + 690 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 1 650 + 100 N/A + 50 + 130 + 50 + 30 - 20 + 750 RUDDER JAM 2 20 1 830 + 250 N/A + 90 + 180 + 70 + 50 - 20 + 570 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 1 890 + 150 N/A + 80 + 180 + 70 + 50 - 40 + 620 ALTN/DIRECT LAW 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 YAW DAMPER FAULT 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 FULL 0 1 390 + 150 + 80 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 460 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 720 FULL 0 1 410 + 140 + 90 + 50 + 130 + 40 + 20 INOP + 640 3 5 1 490 + 150 + 80 + 50 + 130 + 40 + 20 INOP + 740 3 5 1 610 + 140 + 110 + 60 + 140 + 50 + 30 INOP + 820 FULL 0 1 370 + 150 + 80 + 50 + 120 + 40 + 20 - 10 + 630 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 450 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 710 FULL 0 1 430 + 140 + 90 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 500 + 150 + 90 + 50 + 130 + 50 + 30 - 10 + 740 FULL 0 1 400 + 140 + 80 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 10 + 730 FULL 0 1 430 + 140 + 90 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 500 + 150 + 90 + 50 + 130 + 50 + 30 - 10 + 740 FULL 0 1 500 + 130 + 100 + 50 + 140 + 40 + 30 - 10 + 680 3 5 1 570 + 140 + 100 + 60 + 140 + 50 + 30 - 20 + 790 FULL 0 1 540 + 130 + 110 + 60 + 140 + 50 + 30 - 20 + 710 3 5 1 610 + 140 + 110 + 60 + 140 + 50 + 30 - 20 + 820 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 20/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 150 + 240 N/A + 110 + 260 + 90 + 70 - 40 + 410 STAB CTL FAULT with man trim available 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 L/R/L+R ELEV FAULT 2 20 2 150 + 240 N/A + 110 + 260 + 100 + 70 - 40 + 410 RUD TRV LIM FAULT 2 20 2 150 + 240 N/A + 110 + 260 + 90 + 70 - 40 + 410 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 2 240 + 110 N/A + 110 + 270 + 100 + 80 - 100 + 440 RUDDER JAM 2 20 2 480 + 320 N/A + 150 + 320 + 120 + 120 - 70 + 290 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 2 620 + 160 N/A + 160 + 340 + 130 + 150 - 170 + 300 ALTN/DIRECT LAW 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 YAW DAMPER FAULT 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 FULL 0 1 740 + 200 + 140 + 90 + 240 + 70 + 50 - 20 + 410 3 5 1 880 + 220 + 150 + 100 + 260 + 90 + 70 - 30 + 470 FULL 0 1 790 + 210 + 150 + 90 + 250 + 80 + 60 INOP + 410 3 5 1 940 + 230 + 160 + 110 + 270 + 90 + 70 INOP + 480 3 5 2 250 + 310 + 240 + 140 + 330 + 120 + 130 INOP + 570 FULL 0 1 710 + 190 + 130 + 90 + 240 + 70 + 50 - 20 + 400 3 5 1 850 + 210 + 140 + 100 + 250 + 80 + 60 - 30 + 460 FULL 0 1 820 + 210 + 150 + 100 + 260 + 80 + 60 - 30 + 410 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 1 970 + 240 + 170 + 110 + 270 + 100 + 80 - 40 + 480 FULL 0 1 770 + 200 + 140 + 90 + 250 + 70 + 50 - 20 + 410 3 5 1 920 + 220 + 150 + 100 + 270 + 80 + 70 - 30 + 470 FULL 0 1 820 + 210 + 150 + 100 + 260 + 80 + 60 - 30 + 410 3 5 1 970 + 240 + 170 + 110 + 270 + 100 + 80 - 40 + 480 FULL 0 1 970 + 250 + 200 + 110 + 280 + 100 + 90 - 40 + 440 3 5 2 130 + 270 + 210 + 120 + 310 + 110 + 110 - 60 + 530 FULL 0 2 080 + 280 + 230 + 120 + 310 + 110 + 110 - 60 + 480 3 5 2 250 + 310 + 240 + 140 + 330 + 120 + 130 - 70 + 570 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 20m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 21/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 320 + 150 N/A + 90 + 210 + 70 + 80 - 80 + 560 STAB CTL FAULT with man trim available 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 L/R/L+R ELEV FAULT 2 20 2 320 + 150 N/A + 90 + 210 + 70 + 80 - 80 + 560 RUD TRV LIM FAULT 2 20 2 320 + 150 N/A + 90 + 210 + 70 + 80 - 80 + 560 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 2 400 + 70 N/A + 90 + 220 + 80 + 90 - 130 + 600 RUDDER JAM 2 20 2 640 + 230 N/A + 130 + 270 + 100 + 120 - 110 + 430 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 2 770 + 110 N/A + 130 + 280 + 110 + 150 - 190 + 450 ALTN/DIRECT LAW 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 YAW DAMPER FAULT 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 FULL 0 1 960 + 140 + 120 + 70 + 210 + 70 + 70 - 50 + 500 3 5 2 100 + 150 + 120 + 80 + 220 + 70 + 80 - 60 + 580 FULL 0 2 020 + 150 + 120 + 80 + 220 + 70 + 80 INOP + 500 3 5 2 160 + 160 + 130 + 90 + 220 + 70 + 90 INOP + 590 3 5 2 470 + 190 + 180 + 100 + 250 + 90 + 140 INOP + 680 FULL 0 1 930 + 140 + 110 + 70 + 210 + 60 + 70 - 50 + 490 3 5 2 060 + 150 + 120 + 80 + 210 + 70 + 80 - 60 + 570 FULL 0 2 050 + 150 + 130 + 80 + 220 + 70 + 80 - 60 + 500 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 190 + 160 + 130 + 90 + 220 + 80 + 90 - 80 + 590 FULL 0 1 990 + 150 + 120 + 80 + 210 + 70 + 80 - 50 + 500 3 5 2 130 + 150 + 120 + 80 + 220 + 70 + 90 - 70 + 580 FULL 0 2 050 + 150 + 130 + 80 + 220 + 70 + 80 - 60 + 500 3 5 2 190 + 160 + 130 + 90 + 220 + 80 + 90 - 80 + 590 FULL 0 2 210 + 170 + 160 + 90 + 230 + 80 + 110 - 90 + 540 3 5 2 350 + 180 + 160 + 100 + 240 + 90 + 120 - 110 + 640 FULL 0 2 330 + 190 + 180 + 100 + 250 + 80 + 120 - 110 + 570 3 5 2 470 + 190 + 180 + 100 + 250 + 90 + 140 - 130 + 680 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 22/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 2 590 + 180 N/A + 100 + 250 + 90 + 120 - 110 + 520 STAB CTL FAULT with man trim available 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 L/R/L+R ELEV FAULT 2 20 2 590 + 170 N/A + 100 + 250 + 90 + 120 - 110 + 510 RUD TRV LIM FAULT 2 20 2 590 + 180 N/A + 100 + 250 + 90 + 120 - 110 + 520 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 2 690 + 80 N/A + 100 + 250 + 90 + 140 - 180 + 550 RUDDER JAM 2 20 2 930 + 260 N/A + 140 + 310 + 110 + 170 - 150 + 380 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 3 090 + 130 N/A + 150 + 320 + 120 + 200 - 250 + 400 ALTN/DIRECT LAW 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 YAW DAMPER FAULT 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 FULL 0 2 190 + 160 + 130 + 90 + 240 + 80 + 100 - 80 + 460 3 5 2 350 + 170 + 130 + 90 + 250 + 80 + 120 - 100 + 540 FULL 0 2 260 + 170 + 130 + 90 + 250 + 70 + 110 INOP + 460 3 5 2 430 + 180 + 140 + 100 + 260 + 80 + 130 INOP + 550 3 5 2 820 + 220 + 210 + 120 + 300 + 100 + 210 INOP + 640 FULL 0 2 150 + 160 + 120 + 80 + 240 + 70 + 100 - 70 + 450 3 5 2 310 + 170 + 120 + 90 + 250 + 80 + 110 - 90 + 520 FULL 0 2 290 + 180 + 140 + 90 + 250 + 80 + 120 - 100 + 460 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 2 470 + 180 + 140 + 100 + 270 + 80 + 140 - 120 + 550 FULL 0 2 220 + 170 + 130 + 90 + 240 + 80 + 110 - 80 + 460 3 5 2 390 + 180 + 140 + 100 + 260 + 80 + 130 - 110 + 540 FULL 0 2 290 + 180 + 140 + 90 + 250 + 80 + 120 - 100 + 460 3 5 2 470 + 180 + 140 + 100 + 270 + 80 + 140 - 120 + 550 FULL 0 2 500 + 200 + 170 + 110 + 280 + 90 + 150 - 140 + 500 3 5 2 670 + 200 + 180 + 110 + 280 + 100 + 170 - 160 + 600 FULL 0 2 640 + 210 + 200 + 110 + 290 + 100 + 180 - 160 + 530 3 5 2 820 + 220 + 210 + 120 + 300 + 100 + 210 - 180 + 640 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 20m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 23/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 3 290 + 350 N/A + 180 + 450 + 160 + 250 - 180 + 280 STAB CTL FAULT with man trim available 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 L/R/L+R ELEV FAULT 2 20 3 290 + 350 N/A + 180 + 450 + 160 + 250 - 180 + 280 RUD TRV LIM FAULT 2 20 3 290 + 350 N/A + 180 + 450 + 160 + 250 - 180 + 280 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 3 500 + 210 N/A + 190 + 490 + 170 + 300 - 350 + 290 RUDDER JAM 2 20 3 560 + 460 N/A + 230 + 520 + 180 + 330 - 220 + 190 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 3 830 + 310 N/A + 250 + 580 + 200 + 420 - 420 + 180 ALTN/DIRECT LAW 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 YAW DAMPER FAULT 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 FULL 0 2 600 + 310 + 190 + 150 + 420 + 130 + 180 - 110 + 250 3 5 2 890 + 350 + 220 + 170 + 450 + 150 + 230 - 140 + 300 FULL 0 2 690 + 330 + 210 + 160 + 440 + 130 + 200 INOP + 250 3 5 3 020 + 370 + 230 + 190 + 480 + 160 + 270 INOP + 310 3 5 3 770 + 510 + 360 + 270 + 630 + 210 + 540 INOP + 390 FULL 0 2 520 + 300 + 180 + 150 + 410 + 120 + 160 - 100 + 240 3 5 2 810 + 330 + 200 + 170 + 440 + 140 + 210 - 130 + 290 FULL 0 2 740 + 340 + 220 + 160 + 450 + 140 + 210 - 130 + 250 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT 3 5 3 080 + 380 + 240 + 190 + 490 + 160 + 280 - 170 + 310 FULL 0 2 640 + 320 + 200 + 160 + 430 + 130 + 190 - 120 + 250 3 5 2 950 + 360 + 220 + 180 + 470 + 150 + 250 - 150 + 300 FULL 0 2 740 + 340 + 220 + 160 + 450 + 140 + 210 - 130 + 250 3 5 3 080 + 380 + 240 + 190 + 490 + 160 + 280 - 170 + 310 FULL 0 3 080 + 400 + 280 + 200 + 520 + 170 + 300 - 180 + 280 3 5 3 470 + 450 + 300 + 230 + 570 + 190 + 410 - 230 + 350 FULL 0 3 340 + 460 + 330 + 230 + 570 + 190 + 390 - 220 + 310 3 5 3 770 + 510 + 360 + 270 + 630 + 210 + 540 - 290 + 390 (1) Automatic Landing correction: add 190m - (2) Weight correction: subtract 60m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 24/24 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FLIGHT CONTROLS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 4 640 + 360 N/A + 220 + 620 + 170 + 890 - 460 + 280 STAB CTL FAULT with man trim available 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 L/R/L+R ELEV FAULT 2 20 4 630 + 360 N/A + 220 + 620 + 180 + 890 - 460 + 280 RUD TRV LIM FAULT 2 20 4 640 + 360 N/A + 220 + 620 + 170 + 890 - 460 + 280 RUD TRV LIM FAULT with engine out (Calculated with 160kt min) 2 160kt 4 910 + 220 N/A + 220 + 600 + 190 + 940 - 710 + 290 RUDDER JAM 2 20 4 920 + 460 N/A + 270 + 680 + 200 + 980 - 510 + 190 RUDDER JAM with engine out (Calculated with 160kt min) 2 160kt 5 250 + 320 N/A + 270 + 680 + 220 + 1 080 - 820 + 180 ALTN/DIRECT LAW 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 YAW DAMPER FAULT 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 FULL 0 3 890 + 320 + 190 + 190 + 600 + 150 + 770 - 370 + 260 3 5 4 270 + 350 + 200 + 210 + 620 + 170 + 900 - 440 + 300 FULL 0 4 020 + 330 + 200 + 200 + 610 + 160 + 820 INOP + 260 3 5 4 460 + 370 + 220 + 220 + 640 + 180 + 980 INOP + 310 3 5 FULL 0 3 760 + 310 + 170 + 180 + 580 + 140 + 720 - 350 + 240 3 5 4 140 + 330 + 190 + 200 + 610 + 160 + 840 - 410 + 290 FULL 0 4 090 + 340 + 210 + 200 + 610 + 170 + 850 - 420 + 250 PRIM 1(2)(3)/1+2 FAULT PRIM 1+3/2+3 FAULT PRIM 1+2+3 FAULT SEC 1(2)/1+2 FAULT PRIM 1(2)(3) + SEC 1(2) FAULT PART OF SPOILERS HALF OF SPOILERS MOST OF SPOILERS ALL SPOILERS/ GND SPOILER FAULT Landing Distance greater than 6 000 m for all conditions 3 5 4 540 + 380 + 230 + 230 + 650 + 180 + 1 020 - 500 + 310 FULL 0 3 950 + 330 + 190 + 190 + 600 + 160 + 790 - 390 + 250 3 5 4 350 + 360 + 210 + 220 + 630 + 170 + 930 - 450 + 300 FULL 0 4 090 + 340 + 210 + 200 + 610 + 170 + 850 - 420 + 250 3 5 4 540 + 380 + 230 + 230 + 650 + 180 + 1 020 - 500 + 310 FULL 0 4 620 + 400 + 260 + 240 + 670 + 180 + 1 100 - 530 + 280 3 5 5 110 + 440 + 290 + 270 + 700 + 210 + 1 310 - 630 + 350 FULL 0 5 020 + 440 + 300 + 270 + 710 + 200 + 1 310 - 630 + 310 3 5 5 550 + 480 + 340 + 310 + 740 + 220 + 1 590 - 750 + 390 (1) Automatic Landing correction: add 180m - (2) Weight correction: subtract 100m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 1/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-27A-00014129.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 1 780 + 190 N/A + 60 + 140 + 50 + 30 - 30 + 1 040 1+F≤FLAPS<2 2 15 1 580 + 160 + 80 + 60 + 130 + 40 + 30 - 20 + 950 2≤FLAPS<3 2 10 1 480 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 830 FLAPS=3 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 FLAPS>3 FULL 5 1 420 + 140 + 70 + 50 + 130 + 40 + 20 - 20 + 530 0≤SLATS<1 2 30 1 750 + 180 N/A + 60 + 140 + 50 + 30 - 30 + 560 1≤SLATS<2 2 15 1 550 + 160 + 80 + 60 + 140 + 40 + 30 - 20 + 770 SLATS≥2 3 5 1 430 + 150 + 80 + 50 + 130 + 50 + 20 - 20 + 690 NO FLAPS/NO SLATS 1 50 2 090 + 210 N/A + 70 + 150 + 60 + 40 - 40 + 790 0≤FLAPS<1+F 1 50 2 090 + 210 N/A + 70 + 150 + 60 + 40 - 40 + 790 1+F≤FLAPS<2 2 40 1 940 + 190 N/A + 70 + 140 + 50 + 30 - 40 + 640 2 30 1 750 + 180 N/A + 60 + 140 + 50 + 30 - 30 + 560 FLAPS=3 3 25 1 700 + 170 N/A + 60 + 130 + 50 + 20 - 30 + 400 FLAPS>3 FULL 25 1 690 + 160 N/A + 60 + 130 + 50 + 20 - 30 + 210 0≤FLAPS<1+F 2 30 1 730 + 180 N/A + 60 + 140 + 60 + 30 - 30 + 1 020 1+F≤FLAPS<2 2 20 1 650 + 170 N/A + 60 + 130 + 40 + 30 - 30 + 890 2 15 1 550 + 160 + 80 + 60 + 140 + 40 + 30 - 20 + 770 FLAPS=3 3 10 1 500 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 610 FLAPS>3 FULL 10 1 490 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 430 0≤FLAPS<1+F 2 30 1 730 + 180 N/A + 60 + 140 + 60 + 30 - 30 + 1 020 1+F≤FLAPS<2 2 15 1 580 + 160 + 80 + 60 + 130 + 40 + 30 - 20 + 950 2≤FLAPS<3 2 10 1 480 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 830 FLAPS=3 3 5 1 430 + 150 + 80 + 50 + 130 + 50 + 20 - 20 + 690 FLAPS>3 FULL 0 1 360 + 140 + 80 + 40 + 130 + 40 + 20 - 10 + 620 FLAPS FAULT SLATS FAULT 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 2/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 2 490 + 280 N/A + 130 + 300 + 120 + 110 - 100 + 610 1+F≤FLAPS<2 2 15 2 100 + 230 + 150 + 110 + 270 + 100 + 90 - 70 + 600 2≤FLAPS<3 2 10 1 930 + 210 + 140 + 100 + 260 + 90 + 70 - 50 + 550 FLAPS=3 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 FLAPS>3 FULL 5 1 760 + 180 + 130 + 80 + 230 + 80 + 50 - 40 + 330 0≤SLATS<1 2 30 2 370 + 240 N/A + 120 + 270 + 100 + 80 - 80 + 290 1≤SLATS<2 2 15 2 040 + 220 + 130 + 110 + 260 + 90 + 70 - 60 + 480 SLATS≥2 3 5 1 810 + 190 + 140 + 90 + 240 + 80 + 60 - 40 + 450 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 3 030 + 330 N/A + 170 + 340 + 140 + 140 - 150 + 350 0≤FLAPS<1+F 1 50 3 030 + 330 N/A + 170 + 340 + 140 + 140 - 150 + 350 1+F≤FLAPS<2 2 40 2 720 + 280 N/A + 140 + 300 + 120 + 110 - 120 + 300 2 30 2 370 + 240 N/A + 120 + 270 + 100 + 80 - 80 + 290 FLAPS=3 3 25 2 240 + 220 N/A + 110 + 260 + 90 + 60 - 70 + 200 FLAPS>3 FULL 25 2 180 + 210 N/A + 100 + 240 + 90 + 50 - 70 + 90 0≤FLAPS<1+F 2 30 2 370 + 250 N/A + 130 + 280 + 100 + 90 - 80 + 620 1+F≤FLAPS<2 2 20 2 220 + 240 N/A + 110 + 270 + 100 + 90 - 80 + 530 2 15 2 040 + 220 + 130 + 110 + 260 + 90 + 70 - 60 + 480 FLAPS=3 3 10 1 920 + 200 + 130 + 100 + 250 + 80 + 60 - 50 + 380 FLAPS>3 FULL 10 1 870 + 190 + 130 + 90 + 240 + 80 + 50 - 50 + 250 0≤FLAPS<1+F 2 30 2 370 + 250 N/A + 130 + 280 + 100 + 90 - 80 + 620 1+F≤FLAPS<2 2 15 2 100 + 230 + 150 + 110 + 270 + 100 + 90 - 70 + 600 2≤FLAPS<3 2 10 1 930 + 210 + 140 + 100 + 260 + 90 + 70 - 50 + 550 FLAPS=3 3 5 1 810 + 190 + 140 + 90 + 240 + 80 + 60 - 40 + 450 FLAPS>3 FULL 0 1 670 + 170 + 130 + 80 + 220 + 70 + 50 - 30 + 390 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 3/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 2 610 + 150 N/A + 100 + 220 + 90 + 120 - 130 + 870 1+F≤FLAPS<2 2 15 2 280 + 140 + 120 + 90 + 220 + 80 + 100 - 110 + 770 2≤FLAPS<3 2 10 2 120 + 140 + 110 + 80 + 210 + 80 + 80 - 90 + 690 FLAPS=3 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 FLAPS>3 FULL 5 1 970 + 130 + 110 + 70 + 210 + 70 + 70 - 80 + 410 0≤SLATS<1 2 30 2 500 + 150 N/A + 90 + 220 + 80 + 90 - 120 + 450 1≤SLATS<2 2 15 2 220 + 140 + 110 + 90 + 210 + 70 + 80 - 100 + 630 SLATS≥2 3 5 2 020 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 3 040 + 160 N/A + 110 + 240 + 100 + 130 - 170 + 640 0≤FLAPS<1+F 1 50 3 040 + 160 N/A + 110 + 240 + 100 + 130 - 170 + 640 1+F≤FLAPS<2 2 40 2 800 + 160 N/A + 100 + 230 + 100 + 110 - 150 + 500 2 30 2 500 + 150 N/A + 90 + 220 + 80 + 90 - 120 + 450 FLAPS=3 3 25 2 390 + 140 N/A + 90 + 210 + 80 + 80 - 110 + 300 FLAPS>3 FULL 25 2 340 + 140 N/A + 80 + 210 + 80 + 70 - 100 + 140 0≤FLAPS<1+F 2 30 2 500 + 150 N/A + 90 + 220 + 80 + 100 - 120 + 860 1+F≤FLAPS<2 2 20 2 380 + 150 N/A + 90 + 220 + 80 + 100 - 120 + 720 2 15 2 220 + 140 + 110 + 90 + 210 + 70 + 80 - 100 + 630 FLAPS=3 3 10 2 110 + 140 + 110 + 80 + 210 + 70 + 80 - 90 + 490 FLAPS>3 FULL 10 2 070 + 130 + 110 + 70 + 210 + 70 + 70 - 80 + 340 0≤FLAPS<1+F 2 30 2 500 + 150 N/A + 90 + 220 + 80 + 100 - 120 + 860 1+F≤FLAPS<2 2 15 2 280 + 140 + 120 + 90 + 220 + 80 + 100 - 110 + 770 2≤FLAPS<3 2 10 2 120 + 140 + 110 + 80 + 210 + 80 + 80 - 90 + 690 FLAPS=3 3 5 2 020 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 FLAPS>3 FULL 0 1 890 + 130 + 110 + 70 + 200 + 60 + 60 - 70 + 480 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 4/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 2 950 + 180 N/A + 110 + 270 + 100 + 170 - 190 + 810 1+F≤FLAPS<2 2 15 2 570 + 170 + 130 + 100 + 260 + 90 + 140 - 150 + 710 2≤FLAPS<3 2 10 2 380 + 160 + 130 + 90 + 250 + 90 + 120 - 130 + 640 FLAPS=3 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 FLAPS>3 FULL 5 2 190 + 150 + 120 + 80 + 240 + 70 + 100 - 110 + 370 0≤SLATS<1 2 30 2 800 + 170 N/A + 110 + 250 + 90 + 130 - 160 + 410 1≤SLATS<2 2 15 2 490 + 160 + 120 + 100 + 250 + 80 + 120 - 140 + 580 SLATS≥2 3 5 2 260 + 150 + 120 + 90 + 250 + 80 + 110 - 120 + 510 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 3 420 + 190 N/A + 130 + 280 + 120 + 180 - 230 + 590 0≤FLAPS<1+F 1 50 3 420 + 190 N/A + 130 + 280 + 120 + 180 - 230 + 590 1+F≤FLAPS<2 2 40 3 140 + 180 N/A + 120 + 270 + 110 + 160 - 200 + 450 2 30 2 800 + 170 N/A + 110 + 250 + 90 + 130 - 160 + 410 FLAPS=3 3 25 2 660 + 170 N/A + 100 + 250 + 90 + 120 - 150 + 270 FLAPS>3 FULL 25 2 590 + 160 N/A + 100 + 240 + 80 + 100 - 130 + 120 0≤FLAPS<1+F 2 30 2 810 + 170 N/A + 110 + 260 + 90 + 150 - 160 + 790 1+F≤FLAPS<2 2 20 2 680 + 170 N/A + 100 + 250 + 90 + 140 - 160 + 660 2 15 2 490 + 160 + 120 + 100 + 250 + 80 + 120 - 140 + 580 FLAPS=3 3 10 2 360 + 160 + 120 + 90 + 250 + 80 + 110 - 120 + 450 FLAPS>3 FULL 10 2 300 + 150 + 110 + 90 + 250 + 70 + 100 - 110 + 300 0≤FLAPS<1+F 2 30 2 810 + 170 N/A + 110 + 260 + 90 + 150 - 160 + 790 1+F≤FLAPS<2 2 15 2 570 + 170 + 130 + 100 + 260 + 90 + 140 - 150 + 710 2≤FLAPS<3 2 10 2 380 + 160 + 130 + 90 + 250 + 90 + 120 - 130 + 640 FLAPS=3 3 5 2 260 + 150 + 120 + 90 + 250 + 80 + 110 - 120 + 510 FLAPS>3 FULL 0 2 100 + 150 + 120 + 80 + 240 + 70 + 90 - 100 + 440 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 5/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 3 980 + 400 N/A + 230 + 540 + 190 + 420 - 350 + 430 1+F≤FLAPS<2 2 15 3 290 + 360 + 220 + 190 + 490 + 170 + 310 - 240 + 380 2≤FLAPS<3 2 10 2 990 + 330 + 200 + 170 + 470 + 150 + 250 - 190 + 340 FLAPS=3 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 FLAPS>3 FULL 5 2 580 + 280 + 170 + 140 + 400 + 120 + 160 - 140 + 190 0≤SLATS<1 2 30 3 600 + 350 N/A + 190 + 480 + 170 + 270 - 270 + 200 1≤SLATS<2 2 15 3 140 + 330 + 200 + 180 + 470 + 160 + 250 - 210 + 310 SLATS≥2 3 5 2 730 + 300 + 190 + 150 + 440 + 130 + 200 - 150 + 270 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 4 680 + 430 N/A + 260 + 560 + 220 + 470 - 440 + 310 0≤FLAPS<1+F 1 50 4 680 + 430 N/A + 260 + 560 + 220 + 470 - 440 + 310 1+F≤FLAPS<2 2 40 4 110 + 390 N/A + 220 + 510 + 200 + 350 - 350 + 230 2 30 3 600 + 350 N/A + 190 + 480 + 170 + 270 - 270 + 200 FLAPS=3 3 25 3 300 + 320 N/A + 180 + 440 + 150 + 210 - 220 + 130 FLAPS>3 FULL 25 3 110 + 300 N/A + 160 + 410 + 140 + 160 - 190 + 60 0≤FLAPS<1+F 2 30 3 660 + 360 N/A + 200 + 490 + 180 + 330 - 280 + 440 1+F≤FLAPS<2 2 20 3 460 + 360 N/A + 200 + 490 + 170 + 320 - 260 + 340 2 15 3 140 + 330 + 200 + 180 + 470 + 160 + 250 - 210 + 310 FLAPS=3 3 10 2 870 + 310 + 190 + 160 + 440 + 140 + 200 - 170 + 230 FLAPS>3 FULL 10 2 730 + 280 + 160 + 150 + 410 + 120 + 160 - 150 + 150 0≤FLAPS<1+F 2 30 3 660 + 360 N/A + 200 + 490 + 180 + 330 - 280 + 440 1+F≤FLAPS<2 2 15 3 290 + 360 + 220 + 190 + 490 + 170 + 310 - 240 + 380 2≤FLAPS<3 2 10 2 990 + 330 + 200 + 170 + 470 + 150 + 250 - 190 + 340 FLAPS=3 3 5 2 730 + 300 + 190 + 150 + 440 + 130 + 200 - 150 + 270 FLAPS>3 FULL 0 2 450 + 270 + 180 + 130 + 400 + 120 + 150 - 120 + 220 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 6/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 5 590 + 380 N/A + 260 + 680 + 220 + 1 320 - 760 + 430 1+F≤FLAPS<2 2 15 4 810 + 340 + 210 + 230 + 650 + 190 + 1 120 - 620 + 380 2≤FLAPS<3 2 10 4 430 + 320 + 200 + 210 + 630 + 180 + 990 - 540 + 340 FLAPS=3 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 FLAPS>3 FULL 5 3 840 + 280 + 170 + 180 + 590 + 150 + 740 - 420 + 190 0≤SLATS<1 2 30 5 040 + 340 N/A + 230 + 640 + 200 + 1 000 - 620 + 200 1≤SLATS<2 2 15 4 590 + 330 + 190 + 220 + 640 + 180 + 990 - 560 + 310 SLATS≥2 3 5 4 080 + 300 + 190 + 190 + 610 + 160 + 860 - 470 + 270 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 6 300 + 410 N/A + 290 + 710 + 240 + 1 370 - 860 + 310 0≤FLAPS<1+F 1 50 6 300 + 410 N/A + 290 + 710 + 240 + 1 370 - 860 + 310 1+F≤FLAPS<2 2 40 5 630 + 370 N/A + 260 + 670 + 220 + 1 160 - 730 + 230 2 30 5 040 + 340 N/A + 230 + 640 + 200 + 1 000 - 620 + 200 FLAPS=3 3 25 4 660 + 320 N/A + 210 + 620 + 180 + 870 - 540 + 130 FLAPS>3 FULL 25 4 370 + 300 N/A + 200 + 600 + 170 + 740 - 470 + 60 0≤FLAPS<1+F 2 30 5 150 + 350 N/A + 240 + 650 + 200 + 1 120 - 650 + 440 1+F≤FLAPS<2 2 20 4 980 + 350 N/A + 240 + 650 + 190 + 1 130 - 640 + 340 2 15 4 590 + 330 + 190 + 220 + 640 + 180 + 990 - 560 + 310 FLAPS=3 3 10 4 230 + 300 + 180 + 200 + 610 + 170 + 870 - 490 + 230 FLAPS>3 FULL 10 3 980 + 280 + 170 + 180 + 590 + 160 + 740 - 430 + 150 0≤FLAPS<1+F 2 30 5 150 + 350 N/A + 240 + 650 + 200 + 1 120 - 650 + 440 1+F≤FLAPS<2 2 15 4 810 + 340 + 210 + 230 + 650 + 190 + 1 120 - 620 + 380 2≤FLAPS<3 2 10 4 430 + 320 + 200 + 210 + 630 + 180 + 990 - 540 + 340 FLAPS=3 3 5 4 080 + 300 + 190 + 190 + 610 + 160 + 860 - 470 + 270 FLAPS>3 FULL 0 3 710 + 270 + 170 + 170 + 580 + 150 + 740 - 400 + 230 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 7/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-27A-00014129.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 1 780 + 200 N/A + 60 + 140 + 60 + 40 - 20 + 1 040 1+F≤FLAPS<2 2 15 1 580 + 170 + 80 + 60 + 130 + 50 + 30 - 10 + 950 2≤FLAPS<3 2 10 1 490 + 170 + 80 + 50 + 140 + 40 + 20 - 10 + 830 FLAPS=3 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 FLAPS>3 FULL 5 1 420 + 150 + 80 + 50 + 130 + 40 + 20 - 10 + 520 0≤SLATS<1 2 30 1 750 + 180 N/A + 60 + 140 + 60 + 30 - 10 + 550 1≤SLATS<2 2 15 1 550 + 170 + 80 + 50 + 130 + 50 + 30 - 10 + 760 SLATS≥2 3 5 1 440 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 680 NO FLAPS/NO SLATS 1 50 2 090 + 220 N/A + 70 + 150 + 70 + 40 - 20 + 780 0≤FLAPS<1+F 1 50 2 090 + 220 N/A + 70 + 150 + 70 + 40 - 20 + 780 1+F≤FLAPS<2 2 40 1 940 + 200 N/A + 70 + 140 + 60 + 40 - 20 + 640 2 30 1 750 + 180 N/A + 60 + 140 + 60 + 30 - 10 + 550 FLAPS=3 3 25 1 710 + 170 N/A + 60 + 140 + 50 + 20 - 10 + 390 FLAPS>3 FULL 25 1 700 + 170 N/A + 60 + 130 + 50 + 20 - 10 + 200 0≤FLAPS<1+F 2 30 1 740 + 190 N/A + 60 + 140 + 50 + 30 - 10 + 1 020 1+F≤FLAPS<2 2 20 1 650 + 180 N/A + 60 + 130 + 50 + 30 - 10 + 890 2 15 1 550 + 170 + 80 + 50 + 130 + 50 + 30 - 10 + 760 FLAPS=3 3 10 1 500 + 160 + 80 + 50 + 130 + 50 + 20 - 10 + 600 FLAPS>3 FULL 10 1 490 + 160 + 80 + 50 + 130 + 50 + 20 - 10 + 430 0≤FLAPS<1+F 2 30 1 740 + 190 N/A + 60 + 140 + 50 + 30 - 10 + 1 020 1+F≤FLAPS<2 2 15 1 580 + 170 + 80 + 60 + 130 + 50 + 30 - 10 + 950 2≤FLAPS<3 2 10 1 490 + 170 + 80 + 50 + 140 + 40 + 20 - 10 + 830 FLAPS=3 3 5 1 440 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 680 FLAPS>3 FULL 0 1 360 + 150 + 80 + 50 + 120 + 40 + 20 - 10 + 610 FLAPS FAULT SLATS FAULT 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 8/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 2 490 + 290 N/A + 140 + 290 + 120 + 110 - 70 + 620 1+F≤FLAPS<2 2 15 2 110 + 240 + 150 + 120 + 270 + 100 + 80 - 40 + 600 2≤FLAPS<3 2 10 1 940 + 220 + 140 + 100 + 260 + 80 + 60 - 30 + 550 FLAPS=3 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 FLAPS>3 FULL 5 1 770 + 190 + 130 + 90 + 230 + 80 + 50 - 20 + 320 0≤SLATS<1 2 30 2 380 + 260 N/A + 120 + 270 + 100 + 80 - 60 + 290 1≤SLATS<2 2 15 2 040 + 230 + 140 + 110 + 260 + 90 + 70 - 40 + 480 SLATS≥2 3 5 1 820 + 200 + 140 + 90 + 240 + 80 + 60 - 20 + 440 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 3 020 + 350 N/A + 170 + 330 + 140 + 140 - 110 + 360 0≤FLAPS<1+F 1 50 3 020 + 350 N/A + 170 + 330 + 140 + 140 - 110 + 360 1+F≤FLAPS<2 2 40 2 730 + 300 N/A + 150 + 300 + 120 + 110 - 90 + 300 2 30 2 380 + 260 N/A + 120 + 270 + 100 + 80 - 60 + 290 FLAPS=3 3 25 2 250 + 230 N/A + 110 + 260 + 100 + 70 - 50 + 190 FLAPS>3 FULL 25 2 190 + 220 N/A + 100 + 240 + 90 + 50 - 40 + 80 0≤FLAPS<1+F 2 30 2 380 + 270 N/A + 120 + 280 + 110 + 100 - 60 + 620 1+F≤FLAPS<2 2 20 2 230 + 250 N/A + 120 + 270 + 100 + 90 - 50 + 530 2 15 2 040 + 230 + 140 + 110 + 260 + 90 + 70 - 40 + 480 FLAPS=3 3 10 1 930 + 210 + 140 + 100 + 250 + 80 + 60 - 30 + 370 FLAPS>3 FULL 10 1 880 + 200 + 130 + 90 + 240 + 80 + 50 - 20 + 250 0≤FLAPS<1+F 2 30 2 380 + 270 N/A + 120 + 280 + 110 + 100 - 60 + 620 1+F≤FLAPS<2 2 15 2 110 + 240 + 150 + 120 + 270 + 100 + 80 - 40 + 600 2≤FLAPS<3 2 10 1 940 + 220 + 140 + 100 + 260 + 80 + 60 - 30 + 550 FLAPS=3 3 5 1 820 + 200 + 140 + 90 + 240 + 80 + 60 - 20 + 440 FLAPS>3 FULL 0 1 680 + 180 + 130 + 80 + 230 + 70 + 50 - 20 + 390 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 9/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 2 610 + 160 N/A + 100 + 230 + 80 + 110 - 100 + 870 1+F≤FLAPS<2 2 15 2 290 + 160 + 120 + 90 + 220 + 80 + 100 - 80 + 780 2≤FLAPS<3 2 10 2 130 + 150 + 110 + 80 + 210 + 70 + 80 - 60 + 690 FLAPS=3 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 FLAPS>3 FULL 5 1 980 + 140 + 110 + 80 + 210 + 60 + 60 - 50 + 410 0≤SLATS<1 2 30 2 510 + 160 N/A + 90 + 220 + 80 + 90 - 90 + 440 1≤SLATS<2 2 15 2 220 + 150 + 110 + 80 + 210 + 80 + 80 - 70 + 630 SLATS≥2 3 5 2 030 + 140 + 110 + 80 + 210 + 70 + 80 - 50 + 550 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 3 030 + 170 N/A + 110 + 230 + 100 + 130 - 130 + 640 0≤FLAPS<1+F 1 50 3 030 + 170 N/A + 110 + 230 + 100 + 130 - 130 + 640 1+F≤FLAPS<2 2 40 2 810 + 170 N/A + 110 + 230 + 90 + 110 - 110 + 490 2 30 2 510 + 160 N/A + 90 + 220 + 80 + 90 - 90 + 440 FLAPS=3 3 25 2 410 + 150 N/A + 90 + 210 + 80 + 80 - 80 + 290 FLAPS>3 FULL 25 2 350 + 150 N/A + 80 + 210 + 80 + 70 - 70 + 140 0≤FLAPS<1+F 2 30 2 510 + 160 N/A + 90 + 220 + 80 + 100 - 90 + 860 1+F≤FLAPS<2 2 20 2 390 + 160 N/A + 90 + 220 + 80 + 100 - 90 + 720 2 15 2 220 + 150 + 110 + 80 + 210 + 80 + 80 - 70 + 630 FLAPS=3 3 10 2 120 + 150 + 110 + 80 + 210 + 70 + 80 - 60 + 480 FLAPS>3 FULL 10 2 080 + 140 + 100 + 80 + 210 + 70 + 70 - 50 + 330 0≤FLAPS<1+F 2 30 2 510 + 160 N/A + 90 + 220 + 80 + 100 - 90 + 860 1+F≤FLAPS<2 2 15 2 290 + 160 + 120 + 90 + 220 + 80 + 100 - 80 + 780 2≤FLAPS<3 2 10 2 130 + 150 + 110 + 80 + 210 + 70 + 80 - 60 + 690 FLAPS=3 3 5 2 030 + 140 + 110 + 80 + 210 + 70 + 80 - 50 + 550 FLAPS>3 FULL 0 1 900 + 140 + 100 + 70 + 210 + 60 + 60 - 40 + 470 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 10/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 2 930 + 190 N/A + 110 + 260 + 100 + 160 - 140 + 810 1+F≤FLAPS<2 2 15 2 580 + 180 + 130 + 110 + 260 + 80 + 140 - 120 + 720 2≤FLAPS<3 2 10 2 390 + 170 + 120 + 90 + 250 + 80 + 120 - 100 + 640 FLAPS=3 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 FLAPS>3 FULL 5 2 200 + 160 + 110 + 90 + 240 + 70 + 90 - 70 + 370 0≤SLATS<1 2 30 2 800 + 180 N/A + 110 + 250 + 90 + 130 - 120 + 400 1≤SLATS<2 2 15 2 490 + 170 + 120 + 100 + 250 + 80 + 120 - 110 + 580 SLATS≥2 3 5 2 270 + 160 + 120 + 90 + 250 + 80 + 110 - 80 + 510 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 3 400 + 200 N/A + 130 + 280 + 120 + 180 - 180 + 590 0≤FLAPS<1+F 1 50 3 400 + 200 N/A + 130 + 280 + 120 + 180 - 180 + 590 1+F≤FLAPS<2 2 40 3 140 + 200 N/A + 120 + 270 + 110 + 160 - 160 + 450 2 30 2 800 + 180 N/A + 110 + 250 + 90 + 130 - 120 + 400 FLAPS=3 3 25 2 680 + 180 N/A + 100 + 250 + 80 + 110 - 110 + 260 FLAPS>3 FULL 25 2 600 + 170 N/A + 100 + 240 + 80 + 90 - 100 + 120 0≤FLAPS<1+F 2 30 2 810 + 180 N/A + 110 + 260 + 90 + 140 - 130 + 800 1+F≤FLAPS<2 2 20 2 690 + 180 N/A + 100 + 260 + 90 + 140 - 130 + 660 2 15 2 490 + 170 + 120 + 100 + 250 + 80 + 120 - 110 + 580 FLAPS=3 3 10 2 370 + 170 + 120 + 90 + 250 + 80 + 110 - 90 + 440 FLAPS>3 FULL 10 2 300 + 160 + 120 + 90 + 240 + 80 + 90 - 80 + 300 0≤FLAPS<1+F 2 30 2 810 + 180 N/A + 110 + 260 + 90 + 140 - 130 + 800 1+F≤FLAPS<2 2 15 2 580 + 180 + 130 + 110 + 260 + 80 + 140 - 120 + 720 2≤FLAPS<3 2 10 2 390 + 170 + 120 + 90 + 250 + 80 + 120 - 100 + 640 FLAPS=3 3 5 2 270 + 160 + 120 + 90 + 250 + 80 + 110 - 80 + 510 FLAPS>3 FULL 0 2 110 + 160 + 110 + 80 + 240 + 70 + 90 - 70 + 430 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 11/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 3 940 + 410 N/A + 230 + 520 + 180 + 390 - 270 + 450 1+F≤FLAPS<2 2 15 3 300 + 370 + 210 + 200 + 480 + 160 + 300 - 190 + 400 2≤FLAPS<3 2 10 2 990 + 340 + 190 + 170 + 460 + 150 + 240 - 150 + 350 FLAPS=3 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 FLAPS>3 FULL 5 2 590 + 290 + 170 + 140 + 400 + 120 + 150 - 100 + 200 0≤SLATS<1 2 30 3 590 + 360 N/A + 200 + 460 + 170 + 260 - 210 + 210 1≤SLATS<2 2 15 3 140 + 350 + 190 + 180 + 450 + 150 + 240 - 160 + 310 SLATS≥2 3 5 2 740 + 320 + 190 + 160 + 430 + 130 + 200 - 120 + 280 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 4 610 + 440 N/A + 250 + 530 + 220 + 440 - 340 + 320 0≤FLAPS<1+F 1 50 4 610 + 440 N/A + 250 + 530 + 220 + 440 - 340 + 320 1+F≤FLAPS<2 2 40 4 110 + 400 N/A + 230 + 500 + 190 + 340 - 280 + 230 2 30 3 590 + 360 N/A + 200 + 460 + 170 + 260 - 210 + 210 FLAPS=3 3 25 3 320 + 340 N/A + 180 + 430 + 150 + 210 - 180 + 130 FLAPS>3 FULL 25 3 120 + 310 N/A + 160 + 400 + 140 + 160 - 150 + 60 0≤FLAPS<1+F 2 30 3 660 + 380 N/A + 210 + 480 + 170 + 320 - 220 + 460 1+F≤FLAPS<2 2 20 3 460 + 380 N/A + 200 + 480 + 170 + 310 - 210 + 360 2 15 3 140 + 350 + 190 + 180 + 450 + 150 + 240 - 160 + 310 FLAPS=3 3 10 2 890 + 320 + 180 + 160 + 430 + 140 + 200 - 130 + 240 FLAPS>3 FULL 10 2 730 + 290 + 170 + 150 + 400 + 130 + 150 - 110 + 160 0≤FLAPS<1+F 2 30 3 660 + 380 N/A + 210 + 480 + 170 + 320 - 220 + 460 1+F≤FLAPS<2 2 15 3 300 + 370 + 210 + 200 + 480 + 160 + 300 - 190 + 400 2≤FLAPS<3 2 10 2 990 + 340 + 190 + 170 + 460 + 150 + 240 - 150 + 350 FLAPS=3 3 5 2 740 + 320 + 190 + 160 + 430 + 130 + 200 - 120 + 280 FLAPS>3 FULL 0 2 460 + 280 + 170 + 140 + 400 + 110 + 150 - 90 + 230 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 110m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 12/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page SLATS AND FLAPS SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA 0≤FLAPS<1+F 2 30 5 410 + 410 N/A + 260 + 660 + 210 + 1 160 - 590 + 450 1+F≤FLAPS<2 2 15 4 710 + 370 + 200 + 240 + 640 + 180 + 1 010 - 490 + 400 2≤FLAPS<3 2 10 4 340 + 340 + 190 + 210 + 620 + 170 + 890 - 430 + 350 FLAPS=3 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 FLAPS>3 FULL 5 3 780 + 300 + 160 + 180 + 580 + 140 + 680 - 330 + 200 0≤SLATS<1 2 30 4 930 + 370 N/A + 230 + 630 + 190 + 900 - 480 + 210 1≤SLATS<2 2 15 4 490 + 350 + 180 + 220 + 620 + 170 + 890 - 440 + 310 SLATS≥2 3 5 4 020 + 320 + 190 + 190 + 600 + 160 + 790 - 380 + 280 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 6 090 + 440 N/A + 290 + 690 + 230 + 1 200 - 660 + 320 0≤FLAPS<1+F 1 50 6 090 + 440 N/A + 290 + 690 + 230 + 1 200 - 660 + 320 1+F≤FLAPS<2 2 40 5 510 + 400 N/A + 260 + 660 + 220 + 1 040 - 570 + 240 2 30 4 930 + 370 N/A + 230 + 630 + 190 + 900 - 480 + 210 FLAPS=3 3 25 4 590 + 340 N/A + 210 + 610 + 180 + 790 - 430 + 130 FLAPS>3 FULL 25 4 300 + 320 N/A + 200 + 590 + 160 + 670 - 370 + 60 0≤FLAPS<1+F 2 30 5 040 + 380 N/A + 240 + 640 + 190 + 1 010 - 510 + 460 1+F≤FLAPS<2 2 20 4 870 + 380 N/A + 240 + 640 + 190 + 1 010 - 510 + 360 2 15 4 490 + 350 + 180 + 220 + 620 + 170 + 890 - 440 + 310 FLAPS=3 3 10 4 170 + 330 + 180 + 200 + 610 + 160 + 800 - 390 + 240 FLAPS>3 FULL 10 3 910 + 300 + 170 + 180 + 580 + 160 + 670 - 340 + 160 0≤FLAPS<1+F 2 30 5 040 + 380 N/A + 240 + 640 + 190 + 1 010 - 510 + 460 1+F≤FLAPS<2 2 15 4 710 + 370 + 200 + 240 + 640 + 180 + 1 010 - 490 + 400 2≤FLAPS<3 2 10 4 340 + 340 + 190 + 210 + 620 + 170 + 890 - 430 + 350 FLAPS=3 3 5 4 020 + 320 + 190 + 190 + 600 + 160 + 790 - 380 + 280 FLAPS>3 FULL 0 3 650 + 290 + 170 + 170 + 570 + 140 + 670 - 320 + 230 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-28 1/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-28-00014138.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 FUEL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 440 3 15 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 860 + 180 + 130 + 90 + 240 + 80 + 50 - 50 + 260 3 15 2 010 + 200 + 140 + 100 + 250 + 90 + 60 - 60 + 320 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 060 + 130 + 110 + 70 + 210 + 70 + 70 - 80 + 340 3 15 2 200 + 140 + 110 + 80 + 210 + 70 + 80 - 100 + 430 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-28 2/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FUEL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 290 + 150 + 110 + 90 + 240 + 70 + 100 - 110 + 310 3 15 2 450 + 160 + 120 + 100 + 250 + 80 + 110 - 130 + 390 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 720 + 280 + 160 + 150 + 410 + 120 + 160 - 150 + 160 3 15 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 REV OVW (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 3 970 + 280 + 170 + 180 + 590 + 160 + 740 - 430 + 160 3 15 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 150m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-28 3/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-28-00014138.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 FUEL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 480 + 160 + 80 + 50 + 130 + 50 + 20 - 10 + 440 3 15 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 870 + 200 + 130 + 90 + 240 + 80 + 50 - 20 + 260 3 15 2 030 + 220 + 130 + 110 + 250 + 80 + 60 - 30 + 320 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 070 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 340 3 15 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-28 4/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page FUEL SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 290 + 160 + 120 + 90 + 240 + 80 + 90 - 80 + 310 3 15 2 460 + 170 + 120 + 100 + 240 + 80 + 110 - 100 + 390 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 720 + 290 + 170 + 150 + 400 + 130 + 150 - 120 + 160 3 15 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE T TANK UNUSABLE with CG>aft CG limit shown in QRH ABN-28.06 WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 3 910 + 300 + 160 + 180 + 580 + 150 + 680 - 340 + 160 3 15 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 1/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-29-00014130.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 470 + 110 + 80 + 50 + 140 + 50 + 30 - 20 + 610 3 5 1 550 + 120 + 90 + 50 + 140 + 50 + 30 - 30 + 700 FULL 0 1 400 + 130 + 80 + 50 + 130 + 40 + 20 0 + 640 3 5 1 470 + 150 + 80 + 50 + 130 + 50 + 20 - 10 + 740 FULL 0 1 370 + 140 + 80 + 40 + 130 + 40 + 20 0 + 630 3 5 1 440 + 150 + 80 + 50 + 130 + 50 + 20 0 + 720 B SYS LO PR with G SYS FULL 0 / 140kt 1 890 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 1 980 min) + 220 + 120 + 70 + 190 + 60 + 60 - 50 + 560 + 250 + 130 + 70 + 190 + 70 + 70 - 60 + 670 Y SYS LO PR with G SYS FULL 0 / 140kt 1 570 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 1 640 min) + 100 + 100 + 50 + 150 + 50 + 30 - 10 + 620 + 110 + 100 + 60 + 150 + 50 + 30 - 10 + 730 Y SYS LO PR G+Y G+B B+Y 0≤FLAPS<1+F 2 30 1 950 + 150 N/A + 70 + 150 + 50 + 50 - 10 + 1 080 1+F≤FLAPS<2 2 20 1 860 + 120 N/A + 60 + 140 + 60 + 50 - 10 + 920 2≤FLAPS<3 2 20 1 830 + 130 N/A + 60 + 140 + 60 + 40 - 10 + 740 FLAPS=3 3 15 1 790 + 120 + 100 + 60 + 150 + 60 + 40 - 10 + 570 FLAPS>3 FULL 10 1 710 + 110 + 100 + 60 + 150 + 60 + 40 - 10 + 460 SLATS<1 2 30 2 460 + 310 N/A + 90 + 200 + 80 + 90 - 60 + 570 1≤SLATS<2 2 25 2 360 + 310 N/A + 90 + 200 + 80 + 90 - 60 + 640 SLATS≥2 3 15 2 180 + 260 + 130 + 80 + 200 + 80 + 80 - 50 + 520 2 20 1 700 + 160 N/A + 60 + 130 + 50 + 30 INOP + 770 (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 2/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 840 + 190 + 140 + 90 + 260 + 80 + 60 - 50 + 370 3 5 2 000 + 220 + 160 + 100 + 280 + 90 + 80 - 70 + 440 FULL 0 1 760 + 190 + 140 + 90 + 250 + 80 + 60 - 10 + 410 3 5 1 900 + 210 + 150 + 100 + 260 + 90 + 70 - 10 + 480 FULL 0 1 700 + 180 + 130 + 80 + 230 + 70 + 50 - 10 + 410 3 5 1 840 + 200 + 140 + 90 + 250 + 90 + 60 - 10 + 470 B SYS LO PR with G SYS FULL 0 / 140kt 2 010 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 150 min) + 250 + 160 + 100 + 270 + 90 + 90 - 70 + 420 + 270 + 170 + 110 + 290 + 90 + 100 - 70 + 500 Y SYS LO PR with G SYS FULL 0 / 140kt 2 020 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 170 min) + 220 + 180 + 110 + 290 + 90 + 90 - 80 + 380 + 250 + 180 + 120 + 310 + 100 + 110 - 90 + 460 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 2 770 + 320 N/A + 160 + 340 + 130 + 160 - 90 + 640 1+F≤FLAPS<2 2 20 2 630 + 310 N/A + 150 + 340 + 130 + 150 - 90 + 540 2≤FLAPS<3 2 20 2 560 + 290 N/A + 140 + 330 + 120 + 130 - 80 + 430 FLAPS=3 3 15 2 440 + 270 + 190 + 140 + 320 + 120 + 120 - 70 + 330 FLAPS>3 FULL 10 2 260 + 240 + 180 + 120 + 310 + 100 + 90 - 50 + 250 SLATS<1 2 30 2 800 + 340 N/A + 150 + 320 + 120 + 130 - 90 + 330 1≤SLATS<2 2 25 2 660 + 330 N/A + 140 + 310 + 110 + 130 - 70 + 400 SLATS≥2 3 15 2 400 + 300 + 180 + 120 + 300 + 110 + 110 - 50 + 360 2 20 2 370 + 270 N/A + 130 + 290 + 110 + 100 INOP + 470 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 3/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 930 + 130 + 120 + 70 + 200 + 70 + 70 - 80 + 490 3 5 2 070 + 140 + 120 + 80 + 210 + 70 + 80 - 90 + 580 FULL 0 1 980 + 140 + 120 + 70 + 210 + 70 + 80 - 40 + 500 3 5 2 120 + 140 + 120 + 80 + 220 + 70 + 90 - 50 + 590 FULL 0 1 920 + 130 + 110 + 70 + 210 + 60 + 70 - 30 + 490 3 5 2 060 + 140 + 110 + 80 + 220 + 70 + 80 - 40 + 570 B SYS LO PR with G SYS FULL 0 / 140kt 2 110 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 230 min) + 160 + 140 + 80 + 220 + 70 + 90 - 90 + 510 + 180 + 140 + 90 + 230 + 80 + 100 - 90 + 620 Y SYS LO PR with G SYS FULL 0 / 140kt 2 100 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 220 min) + 140 + 140 + 80 + 220 + 80 + 90 - 90 + 500 + 150 + 140 + 90 + 230 + 80 + 100 - 90 + 600 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 2 670 + 160 N/A + 100 + 230 + 90 + 130 - 90 + 930 1+F≤FLAPS<2 2 20 2 580 + 160 N/A + 100 + 230 + 80 + 130 - 90 + 780 2≤FLAPS<3 2 20 2 520 + 160 N/A + 100 + 230 + 80 + 110 - 80 + 620 FLAPS=3 3 15 2 450 + 160 + 140 + 100 + 230 + 80 + 100 - 80 + 470 FLAPS>3 FULL 10 2 300 + 150 + 140 + 90 + 230 + 80 + 90 - 60 + 360 SLATS<1 2 30 2 770 + 200 N/A + 110 + 230 + 90 + 120 - 100 + 500 1≤SLATS<2 2 25 2 650 + 200 N/A + 100 + 230 + 90 + 120 - 90 + 570 SLATS≥2 3 15 2 450 + 180 + 140 + 100 + 230 + 80 + 110 - 80 + 480 2 20 2 530 + 160 N/A + 100 + 230 + 90 + 110 INOP + 630 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 4/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 160 + 150 + 120 + 80 + 240 + 70 + 100 - 110 + 450 3 5 2 320 + 160 + 130 + 90 + 250 + 80 + 120 - 130 + 530 FULL 0 2 220 + 160 + 130 + 90 + 250 + 80 + 110 - 70 + 460 3 5 2 380 + 160 + 140 + 90 + 260 + 80 + 130 - 90 + 540 FULL 0 2 140 + 150 + 120 + 80 + 240 + 70 + 100 - 60 + 450 3 5 2 300 + 160 + 130 + 90 + 250 + 80 + 120 - 70 + 530 B SYS LO PR with G SYS FULL 0 / 140kt 2 370 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 510 min) + 160 + 150 + 90 + 260 + 80 + 130 - 130 + 470 + 170 + 160 + 100 + 270 + 90 + 150 - 140 + 570 Y SYS LO PR with G SYS FULL 0 / 140kt 2 360 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 510 min) + 160 + 150 + 90 + 260 + 90 + 130 - 130 + 460 + 170 + 150 + 100 + 270 + 90 + 150 - 140 + 560 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 3 020 + 190 N/A + 120 + 270 + 110 + 180 - 140 + 870 1+F≤FLAPS<2 2 20 2 920 + 190 N/A + 120 + 270 + 100 + 180 - 140 + 720 2≤FLAPS<3 2 20 2 850 + 180 N/A + 110 + 270 + 100 + 160 - 130 + 570 FLAPS=3 3 15 2 760 + 180 + 150 + 110 + 270 + 90 + 150 - 120 + 430 FLAPS>3 FULL 10 2 580 + 170 + 150 + 100 + 270 + 90 + 130 - 90 + 330 SLATS<1 2 30 3 120 + 190 N/A + 120 + 280 + 110 + 170 - 160 + 460 1≤SLATS<2 2 25 2 990 + 190 N/A + 120 + 270 + 100 + 170 - 140 + 520 SLATS≥2 3 15 2 760 + 180 + 160 + 110 + 270 + 100 + 160 - 120 + 440 2 20 2 870 + 190 N/A + 110 + 270 + 100 + 160 INOP + 580 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 5/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 540 + 290 + 190 + 140 + 420 + 120 + 170 - 140 + 230 3 5 2 840 + 320 + 210 + 160 + 460 + 150 + 230 - 170 + 290 FULL 0 2 640 + 310 + 200 + 150 + 440 + 130 + 190 - 80 + 240 3 5 2 940 + 340 + 220 + 170 + 480 + 150 + 250 - 130 + 300 FULL 0 2 520 + 290 + 190 + 140 + 410 + 120 + 170 - 70 + 240 3 5 2 810 + 320 + 200 + 160 + 450 + 140 + 220 - 100 + 290 B SYS LO PR with G SYS FULL 0 / 140kt 2 850 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 3 160 min) + 330 + 240 + 170 + 480 + 150 + 240 - 230 + 240 + 370 + 260 + 190 + 530 + 170 + 320 - 290 + 310 Y SYS LO PR with G SYS FULL 0 / 140kt 2 860 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 3 170 min) + 330 + 240 + 170 + 480 + 150 + 240 - 230 + 250 + 380 + 250 + 200 + 530 + 170 + 320 - 290 + 310 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 4 120 + 420 N/A + 250 + 560 + 210 + 480 - 340 + 520 1+F≤FLAPS<2 2 20 3 960 + 430 N/A + 240 + 580 + 200 + 490 - 330 + 390 2≤FLAPS<3 2 20 3 810 + 410 N/A + 230 + 560 + 190 + 400 - 290 + 310 FLAPS=3 3 15 3 540 + 390 + 250 + 210 + 530 + 190 + 340 - 230 + 230 FLAPS>3 FULL 10 3 170 + 350 + 230 + 190 + 490 + 160 + 250 - 150 + 170 SLATS<1 2 30 4 190 + 420 N/A + 240 + 570 + 210 + 430 - 360 + 240 1≤SLATS<2 2 25 3 990 + 420 N/A + 240 + 560 + 210 + 410 - 320 + 270 SLATS≥2 3 15 3 540 + 390 + 240 + 210 + 540 + 180 + 340 - 230 + 230 2 20 3 830 + 410 N/A + 230 + 560 + 200 + 410 INOP + 310 (1) Automatic Landing correction: add 170m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 6/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 3 860 + 290 + 180 + 180 + 600 + 150 + 800 - 440 + 230 3 5 4 280 + 310 + 200 + 200 + 630 + 170 + 960 - 530 + 290 FULL 0 4 030 + 300 + 200 + 190 + 620 + 160 + 880 - 330 + 240 3 5 4 430 + 330 + 210 + 210 + 640 + 180 + 1 030 - 420 + 300 FULL 0 3 830 + 280 + 180 + 180 + 590 + 150 + 790 - 280 + 240 3 5 4 220 + 310 + 200 + 200 + 620 + 170 + 930 - 370 + 290 B SYS LO PR with G SYS FULL 0 / 140kt 4 350 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 4 780 min) + 320 + 230 + 210 + 640 + 180 + 1 010 - 240 + 240 + 360 + 250 + 230 + 670 + 190 + 1 210 - 350 + 310 Y SYS LO PR with G SYS FULL 0 / 140kt 4 370 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 4 790 min) + 320 + 230 + 210 + 650 + 180 + 1 020 - 250 + 250 + 360 + 250 + 230 + 670 + 200 + 1 210 - 360 + 310 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 Landing Distance greater than 6 000 m for all conditions 1+F≤FLAPS<2 2 20 Landing Distance greater than 6 000 m for all conditions 2≤FLAPS<3 2 20 Landing Distance greater than 6 000 m for all conditions FLAPS=3 3 15 Landing Distance greater than 6 000 m for all conditions FLAPS>3 FULL 10 SLATS<1 2 30 Landing Distance greater than 6 000 m for all conditions 1≤SLATS<2 2 25 Landing Distance greater than 6 000 m for all conditions SLATS≥2 3 15 Landing Distance greater than 6 000 m for all conditions 2 20 Landing Distance greater than 6 000 m for all conditions 4 680 + 340 + 220 + 220 + 660 + 190 + 1 030 (1) Automatic Landing correction: add 170m - (2) Weight correction: subtract 60m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE - 180 + 170 PER-29 7/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-29-00014130.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 480 + 120 + 80 + 50 + 140 + 40 + 30 - 10 + 600 3 5 1 560 + 130 + 90 + 50 + 140 + 50 + 30 - 20 + 700 FULL 0 1 400 + 140 + 80 + 50 + 130 + 40 + 20 - 10 + 640 3 5 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 10 + 730 FULL 0 1 370 + 150 + 80 + 50 + 120 + 40 + 20 - 10 + 630 3 5 1 450 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 710 B SYS LO PR with G SYS FULL 0 / 140kt 1 890 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 1 990 min) + 230 + 130 + 70 + 190 + 60 + 60 - 80 + 560 + 260 + 130 + 80 + 190 + 70 + 70 - 80 + 660 Y SYS LO PR with G SYS FULL 0 / 140kt 1 570 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 1 640 min) + 110 + 110 + 60 + 140 + 50 + 30 - 30 + 620 + 120 + 100 + 60 + 150 + 50 + 40 - 30 + 720 Y SYS LO PR G+Y G+B B+Y 0≤FLAPS<1+F 2 30 1 950 + 150 N/A + 70 + 150 + 60 + 50 - 30 + 1 080 1+F≤FLAPS<2 2 20 1 870 + 130 N/A + 60 + 150 + 60 + 50 - 30 + 920 2≤FLAPS<3 2 20 1 840 + 140 N/A + 60 + 140 + 60 + 40 - 30 + 740 FLAPS=3 3 15 1 800 + 120 + 100 + 60 + 150 + 60 + 40 - 30 + 570 FLAPS>3 FULL 10 1 720 + 120 + 100 + 60 + 150 + 50 + 30 - 20 + 460 SLATS<1 2 30 2 470 + 320 N/A + 90 + 200 + 80 + 90 - 90 + 570 1≤SLATS<2 2 25 2 370 + 310 N/A + 90 + 200 + 70 + 90 - 80 + 630 SLATS≥2 3 15 2 200 + 270 + 130 + 90 + 200 + 70 + 80 - 70 + 520 2 20 1 710 + 170 N/A + 60 + 130 + 50 + 30 - 20 + 770 (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 8/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 5 - GOOD Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 850 + 210 + 140 + 100 + 260 + 80 + 60 - 30 + 370 3 5 2 020 + 230 + 150 + 110 + 280 + 90 + 80 - 40 + 430 FULL 0 1 770 + 200 + 140 + 90 + 250 + 70 + 50 - 20 + 410 3 5 1 920 + 220 + 150 + 100 + 270 + 80 + 70 - 30 + 470 FULL 0 1 710 + 190 + 130 + 90 + 240 + 70 + 50 - 20 + 400 3 5 1 850 + 210 + 140 + 100 + 250 + 90 + 60 - 30 + 460 B SYS LO PR with G SYS FULL 0 / 140kt 2 010 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 160 min) + 270 + 170 + 100 + 270 + 90 + 80 - 90 + 420 + 290 + 170 + 110 + 290 + 100 + 100 - 100 + 500 Y SYS LO PR with G SYS FULL 0 / 140kt 2 020 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 180 min) + 240 + 190 + 110 + 290 + 100 + 90 - 100 + 380 + 270 + 190 + 120 + 310 + 110 + 110 - 110 + 460 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 2 780 + 340 N/A + 160 + 340 + 140 + 160 - 110 + 640 1+F≤FLAPS<2 2 20 2 650 + 330 N/A + 150 + 340 + 120 + 150 - 100 + 550 2≤FLAPS<3 2 20 2 570 + 310 N/A + 140 + 320 + 120 + 130 - 90 + 420 FLAPS=3 3 15 2 460 + 290 + 190 + 140 + 320 + 120 + 120 - 90 + 320 FLAPS>3 FULL 10 2 270 + 260 + 180 + 120 + 310 + 100 + 90 - 70 + 250 SLATS<1 2 30 2 800 + 360 N/A + 150 + 320 + 130 + 130 - 110 + 330 1≤SLATS<2 2 25 2 660 + 340 N/A + 140 + 310 + 120 + 130 - 100 + 390 SLATS≥2 3 15 2 420 + 310 + 180 + 130 + 300 + 110 + 110 - 80 + 350 2 20 2 380 + 290 N/A + 130 + 290 + 110 + 100 - 70 + 460 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 9/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 940 + 140 + 110 + 70 + 210 + 70 + 70 - 50 + 490 3 5 2 080 + 150 + 120 + 80 + 210 + 70 + 80 - 60 + 570 FULL 0 1 990 + 150 + 120 + 80 + 210 + 70 + 80 - 50 + 500 3 5 2 130 + 150 + 120 + 80 + 220 + 70 + 90 - 70 + 580 FULL 0 1 930 + 140 + 110 + 70 + 210 + 60 + 70 - 50 + 490 3 5 2 070 + 150 + 110 + 80 + 220 + 70 + 80 - 60 + 570 B SYS LO PR with G SYS FULL 0 / 140kt 2 110 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 240 min) + 180 + 150 + 80 + 220 + 70 + 90 - 110 + 520 + 190 + 140 + 90 + 230 + 80 + 100 - 120 + 620 Y SYS LO PR with G SYS FULL 0 / 140kt 2 110 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 230 min) + 160 + 140 + 80 + 230 + 70 + 90 - 110 + 500 + 160 + 140 + 90 + 230 + 80 + 100 - 120 + 600 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 2 680 + 170 N/A + 100 + 230 + 90 + 120 - 110 + 930 1+F≤FLAPS<2 2 20 2 590 + 170 N/A + 100 + 230 + 80 + 120 - 120 + 780 2≤FLAPS<3 2 20 2 520 + 170 N/A + 100 + 220 + 90 + 110 - 110 + 610 FLAPS=3 3 15 2 460 + 170 + 140 + 100 + 230 + 80 + 100 - 110 + 460 FLAPS>3 FULL 10 2 310 + 160 + 140 + 90 + 230 + 80 + 90 - 90 + 360 SLATS<1 2 30 2 770 + 210 N/A + 110 + 230 + 90 + 120 - 120 + 490 1≤SLATS<2 2 25 2 650 + 210 N/A + 100 + 230 + 90 + 110 - 120 + 560 SLATS≥2 3 15 2 460 + 190 + 140 + 100 + 230 + 90 + 110 - 110 + 480 2 20 2 540 + 170 N/A + 100 + 230 + 80 + 110 - 110 + 620 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 10/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 160 + 160 + 130 + 80 + 240 + 80 + 100 - 70 + 440 3 5 2 330 + 170 + 130 + 90 + 250 + 80 + 120 - 90 + 530 FULL 0 2 220 + 170 + 130 + 90 + 240 + 80 + 110 - 80 + 460 3 5 2 390 + 180 + 140 + 100 + 260 + 80 + 130 - 110 + 540 FULL 0 2 150 + 160 + 120 + 80 + 240 + 70 + 100 - 70 + 450 3 5 2 310 + 170 + 130 + 90 + 250 + 80 + 110 - 90 + 520 B SYS LO PR with G SYS FULL 0 / 140kt 2 360 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 520 min) + 180 + 160 + 90 + 260 + 90 + 130 - 150 + 470 + 190 + 160 + 100 + 270 + 90 + 150 - 160 + 570 Y SYS LO PR with G SYS FULL 0 / 140kt 2 360 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 2 520 min) + 180 + 160 + 100 + 260 + 80 + 130 - 150 + 460 + 190 + 150 + 100 + 270 + 90 + 140 - 160 + 560 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 3 020 + 200 N/A + 120 + 270 + 110 + 180 - 160 + 870 1+F≤FLAPS<2 2 20 2 930 + 200 N/A + 120 + 270 + 100 + 180 - 160 + 730 2≤FLAPS<3 2 20 2 850 + 200 N/A + 110 + 270 + 100 + 160 - 150 + 570 FLAPS=3 3 15 2 770 + 200 + 150 + 120 + 270 + 90 + 150 - 150 + 420 FLAPS>3 FULL 10 2 580 + 190 + 150 + 110 + 260 + 90 + 130 - 130 + 330 SLATS<1 2 30 3 120 + 200 N/A + 130 + 280 + 100 + 170 - 170 + 450 1≤SLATS<2 2 25 2 990 + 200 N/A + 120 + 270 + 100 + 160 - 160 + 510 SLATS≥2 3 15 2 770 + 200 + 160 + 110 + 270 + 100 + 150 - 150 + 430 2 20 2 870 + 200 N/A + 110 + 270 + 100 + 160 - 160 + 570 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 10m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 11/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 540 + 300 + 190 + 140 + 410 + 130 + 170 - 100 + 240 3 5 2 860 + 340 + 210 + 170 + 450 + 140 + 220 - 140 + 300 FULL 0 2 640 + 320 + 200 + 160 + 430 + 130 + 190 - 120 + 250 3 5 2 950 + 360 + 220 + 180 + 470 + 150 + 250 - 150 + 300 FULL 0 2 520 + 300 + 190 + 150 + 400 + 120 + 160 - 100 + 250 3 5 2 820 + 330 + 200 + 170 + 440 + 140 + 210 - 130 + 290 B SYS LO PR with G SYS FULL 0 / 140kt 2 850 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 3 180 min) + 350 + 240 + 180 + 470 + 140 + 230 - 230 + 260 + 400 + 250 + 200 + 510 + 170 + 310 - 270 + 320 Y SYS LO PR with G SYS FULL 0 / 140kt 2 850 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 3 180 min) + 360 + 250 + 180 + 470 + 150 + 230 - 230 + 260 + 400 + 260 + 200 + 510 + 170 + 310 - 270 + 320 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 4 110 + 440 N/A + 250 + 540 + 200 + 460 - 300 + 540 1+F≤FLAPS<2 2 20 3 950 + 450 N/A + 250 + 560 + 200 + 460 - 300 + 420 2≤FLAPS<3 2 20 3 790 + 430 N/A + 230 + 530 + 190 + 380 - 270 + 320 FLAPS=3 3 15 3 560 + 410 + 250 + 220 + 520 + 180 + 330 - 240 + 240 FLAPS>3 FULL 10 3 180 + 370 + 220 + 190 + 480 + 160 + 240 - 180 + 180 SLATS<1 2 30 4 170 + 440 N/A + 250 + 540 + 200 + 400 - 320 + 240 1≤SLATS<2 2 25 3 980 + 440 N/A + 240 + 540 + 190 + 390 - 290 + 280 SLATS≥2 3 15 3 560 + 410 + 240 + 220 + 520 + 180 + 330 - 240 + 230 2 20 3 820 + 430 N/A + 230 + 540 + 190 + 390 - 270 + 320 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 12/12 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page HYDRAULIC SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 1 - POOR Corrections on Landing Distance (m) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR (2) WGT SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 3 790 + 310 + 180 + 180 + 590 + 150 + 730 - 350 + 240 3 5 4 210 + 340 + 200 + 200 + 620 + 170 + 870 - 420 + 300 FULL 0 3 950 + 330 + 190 + 190 + 600 + 160 + 790 - 390 + 250 3 5 4 350 + 360 + 210 + 220 + 630 + 170 + 930 - 450 + 300 FULL 0 3 760 + 310 + 180 + 180 + 580 + 150 + 720 - 350 + 250 3 5 4 150 + 340 + 200 + 200 + 610 + 170 + 840 - 410 + 290 B SYS LO PR with G SYS FULL 0 / 140kt 4 240 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 4 680 min) + 350 + 240 + 210 + 630 + 170 + 900 - 520 + 250 + 390 + 250 + 240 + 660 + 190 + 1 080 - 600 + 320 Y SYS LO PR with G SYS FULL 0 / 140kt 4 260 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 4 700 min) + 360 + 230 + 210 + 630 + 170 + 910 - 520 + 260 + 390 + 240 + 240 + 660 + 190 + 1 100 - 600 + 320 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 5 650 + 430 N/A + 280 + 680 + 230 + 1 280 - 650 + 540 1+F≤FLAPS<2 2 20 5 560 + 440 N/A + 290 + 690 + 210 + 1 340 - 670 + 420 2≤FLAPS<3 2 20 5 340 + 420 N/A + 270 + 670 + 210 + 1 180 - 620 + 320 FLAPS=3 3 15 5 070 + 410 + 240 + 260 + 670 + 200 + 1 100 - 580 + 240 FLAPS>3 FULL 10 4 570 + 370 + 220 + 230 + 640 + 180 + 920 - 480 + 180 SLATS<1 2 30 5 710 + 430 N/A + 290 + 690 + 220 + 1 200 - 660 + 240 1≤SLATS<2 2 25 5 520 + 430 N/A + 280 + 680 + 220 + 1 190 - 640 + 280 SLATS≥2 3 15 5 060 + 400 + 230 + 260 + 670 + 200 + 1 100 - 570 + 230 2 20 5 380 + 420 N/A + 270 + 680 + 210 + 1 200 - 630 + 320 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-30 1/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-30-00014132.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 ANTI ICE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 440 15 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 1 860 + 180 + 130 + 90 + 240 + 80 + 50 - 50 + 260 15 2 010 + 200 + 140 + 100 + 250 + 90 + 60 - 60 + 320 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 2 060 + 130 + 110 + 70 + 210 + 70 + 70 - 80 + 340 15 2 200 + 140 + 110 + 80 + 210 + 70 + 80 - 100 + 430 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-30 2/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ANTI ICE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 2 290 + 150 + 110 + 90 + 240 + 70 + 100 - 110 + 310 15 2 450 + 160 + 120 + 100 + 250 + 80 + 110 - 130 + 390 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 2 720 + 280 + 160 + 150 + 410 + 120 + 160 - 150 + 160 15 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 REV OVW (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 3 970 + 280 + 170 + 180 + 590 + 160 + 740 - 430 + 160 15 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 150m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-30 3/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-30-00014132.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 ANTI ICE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 1 480 + 160 + 80 + 50 + 130 + 50 + 20 - 10 + 440 15 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 1 870 + 200 + 130 + 90 + 240 + 80 + 50 - 20 + 260 15 2 030 + 220 + 130 + 110 + 250 + 80 + 60 - 30 + 320 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 2 070 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 340 15 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-30 4/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ANTI ICE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 2 290 + 160 + 120 + 90 + 240 + 80 + 90 - 80 + 310 15 2 460 + 170 + 120 + 100 + 240 + 80 + 110 - 100 + 390 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 2 720 + 290 + 170 + 150 + 400 + 130 + 150 - 120 + 160 15 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA The following ECAM FULL alerts with Ice Accretion: -WING LO PR 3 -WING VLVE NOT OPEN -WAI SYS FAULT 10 3 910 + 300 + 160 + 180 + 580 + 150 + 680 - 340 + 160 15 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 1/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-32-00014133.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 BRAKE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 750 + 230 + 100 + 60 + 190 + 50 + 60 - 50 + 580 3 5 1 870 + 240 + 110 + 70 + 190 + 70 + 70 - 60 + 660 FULL 0 1 420 + 150 + 80 + 50 + 130 + 50 + 30 - 20 + 590 3 5 1 510 + 160 + 80 + 50 + 150 + 40 + 30 - 20 + 670 FULL 0 1 520 + 170 + 90 + 50 + 150 + 50 + 30 - 30 + 560 3 5 1 610 + 180 + 90 + 60 + 160 + 50 + 40 - 30 + 650 REV OVW (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 830 + 220 + 120 + 80 + 240 + 70 + 60 - 50 + 410 3 5 1 970 + 240 + 130 + 90 + 250 + 80 + 80 - 60 + 470 FULL 0 1 760 + 180 + 130 + 80 + 240 + 80 + 60 - 40 + 380 3 5 1 910 + 200 + 140 + 90 + 260 + 90 + 70 - 60 + 430 FULL 0 1 880 + 200 + 130 + 90 + 270 + 80 + 70 - 60 + 350 3 5 2 050 + 220 + 140 + 100 + 290 + 90 + 80 - 70 + 400 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 2/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page BRAKE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 880 + 180 + 110 + 70 + 200 + 60 + 70 - 70 + 510 3 5 2 020 + 200 + 110 + 80 + 210 + 60 + 80 - 80 + 590 FULL 0 2 000 + 140 + 110 + 70 + 220 + 70 + 80 - 90 + 460 3 5 2 150 + 140 + 110 + 80 + 230 + 70 + 90 - 100 + 540 FULL 0 2 150 + 150 + 120 + 80 + 250 + 70 + 100 - 110 + 430 3 5 2 310 + 160 + 120 + 90 + 250 + 80 + 120 - 130 + 510 REV OVW (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m 3 - MEDIUM Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 090 + 150 + 120 + 80 + 230 + 80 + 100 - 100 + 460 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 540 FULL 0 2 230 + 160 + 120 + 90 + 260 + 70 + 110 - 120 + 420 3 5 2 400 + 170 + 130 + 90 + 270 + 80 + 130 - 140 + 490 FULL 0 2 390 + 170 + 130 + 90 + 280 + 90 + 150 - 150 + 390 3 5 2 590 + 180 + 130 + 100 + 300 + 90 + 170 - 170 + 460 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 3/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page BRAKE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 440 + 270 + 180 + 140 + 390 + 120 + 150 - 120 + 240 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 FULL 0 2 580 + 290 + 180 + 140 + 430 + 120 + 180 - 140 + 220 3 5 2 870 + 320 + 190 + 160 + 470 + 140 + 230 - 180 + 260 FULL 0 2 730 + 300 + 190 + 150 + 450 + 140 + 210 - 170 + 200 3 5 3 050 + 340 + 200 + 170 + 500 + 150 + 280 - 210 + 240 REV OVW (1) Automatic Landing correction: add 160m - (2) Weight correction: subtract 110m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 3 700 + 270 + 180 + 170 + 580 + 150 + 730 - 400 + 240 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 FULL 0 3 910 + 280 + 180 + 190 + 640 + 160 + 950 - 450 + 210 3 5 4 320 + 310 + 190 + 210 + 680 + 170 + 1 130 - 530 + 260 FULL 0 4 160 + 290 + 180 + 200 + 720 + 170 + 1 340 - 520 + 200 3 5 Landing Distance greater than 6 000 m for all conditions (1) Automatic Landing correction: add 160m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 4/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-32-00014133.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 BRAKE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 750 + 230 + 100 + 60 + 180 + 60 + 60 - 30 + 580 3 5 1 880 + 250 + 110 + 70 + 190 + 70 + 70 - 30 + 660 FULL 0 1 430 + 160 + 80 + 50 + 140 + 40 + 20 - 10 + 580 3 5 1 510 + 170 + 80 + 50 + 140 + 50 + 30 - 10 + 670 FULL 0 1 520 + 180 + 90 + 50 + 150 + 50 + 30 - 20 + 550 3 5 1 620 + 190 + 90 + 60 + 160 + 50 + 30 - 20 + 640 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 830 + 230 + 130 + 80 + 230 + 70 + 60 - 30 + 410 3 5 1 980 + 250 + 130 + 90 + 250 + 80 + 80 - 40 + 470 FULL 0 1 770 + 200 + 130 + 90 + 250 + 70 + 50 - 20 + 370 3 5 1 920 + 220 + 140 + 100 + 260 + 90 + 70 - 30 + 430 FULL 0 1 890 + 210 + 130 + 90 + 270 + 80 + 70 - 30 + 350 3 5 2 060 + 230 + 150 + 110 + 290 + 90 + 90 - 50 + 400 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 5/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page BRAKE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 1 890 + 190 + 110 + 70 + 200 + 60 + 70 - 40 + 500 3 5 2 030 + 210 + 110 + 80 + 210 + 60 + 80 - 50 + 580 FULL 0 2 010 + 150 + 110 + 80 + 220 + 70 + 80 - 60 + 460 3 5 2 160 + 150 + 110 + 80 + 230 + 70 + 90 - 70 + 540 FULL 0 2 150 + 160 + 120 + 80 + 240 + 80 + 100 - 70 + 430 3 5 2 320 + 170 + 120 + 90 + 250 + 80 + 120 - 90 + 510 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 60m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m 3 - MEDIUM Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 100 + 160 + 120 + 80 + 230 + 70 + 90 - 70 + 460 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 530 FULL 0 2 230 + 170 + 120 + 90 + 260 + 80 + 110 - 80 + 420 3 5 2 410 + 180 + 130 + 100 + 270 + 80 + 130 - 100 + 490 FULL 0 2 390 + 180 + 130 + 100 + 280 + 90 + 140 - 110 + 390 3 5 2 590 + 190 + 140 + 110 + 300 + 90 + 170 - 130 + 460 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 6/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page BRAKE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 2 450 + 280 + 170 + 140 + 390 + 120 + 150 - 90 + 240 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 290 FULL 0 2 580 + 300 + 170 + 150 + 420 + 120 + 170 - 110 + 220 3 5 2 880 + 330 + 190 + 170 + 460 + 140 + 230 - 140 + 260 FULL 0 2 730 + 320 + 180 + 150 + 440 + 130 + 210 - 130 + 210 3 5 3 050 + 360 + 200 + 180 + 490 + 150 + 270 - 170 + 240 REV OVW (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 110m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE ANTISKID FAULT ONE BRK RELEASED TWO BRK RELEASED WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 3 640 + 290 + 170 + 170 + 570 + 150 + 670 - 320 + 240 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 290 FULL 0 3 840 + 310 + 170 + 180 + 630 + 150 + 870 - 360 + 220 3 5 4 240 + 340 + 190 + 210 + 660 + 170 + 1 020 - 430 + 270 FULL 0 4 070 + 320 + 170 + 200 + 700 + 160 + 1 220 - 420 + 210 3 5 4 500 + 350 + 210 + 240 + 800 + 200 + 1 030 - 490 + 240 (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 1/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-34-00014134.0068001 / 01 DEC 14 Applicable to: MSN 0968-1118 NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 ALL ADR OFF 3 N/A 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 ADR/IR DISAGREE 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 ALL ADR OFF 3 N/A 2 010 + 200 + 140 + 100 + 250 + 90 + 60 - 60 + 320 ADR/IR DISAGREE 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 ALL ADR OFF 3 N/A 2 200 + 140 + 110 + 80 + 210 + 70 + 80 - 100 + 430 ADR/IR DISAGREE 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 2/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 ALL ADR OFF 3 N/A 2 450 + 160 + 120 + 100 + 250 + 80 + 110 - 130 + 390 ADR/IR DISAGREE 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 REV OVW (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 ALL ADR OFF 3 N/A 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 ADR/IR DISAGREE 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 REV OVW (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 130m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 ALL ADR OFF 3 N/A 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 ADR/IR DISAGREE 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 150m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 3/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-34-00014134.0065001 / 28 FEB 14 Applicable to: MSN 0700 NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 ALL ADR OFF 3 N/A 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 ADR/IR DISAGREE 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 60m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 ALL ADR OFF 3 N/A 2 030 + 220 + 130 + 110 + 250 + 80 + 60 - 30 + 320 ADR/IR DISAGREE 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 ALL ADR OFF 3 N/A 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 ADR/IR DISAGREE 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 4/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 ALL ADR OFF 3 N/A 2 460 + 170 + 120 + 100 + 240 + 80 + 110 - 100 + 390 ADR/IR DISAGREE 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 ALL ADR OFF 3 N/A 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 ADR/IR DISAGREE 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 ALL ADR OFF 3 N/A 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 ADR/IR DISAGREE 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 150m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 5/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-34-00014134.0045001 / 01 DEC 14 Applicable to: MSN 0232-0361 NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 3 15 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 2 010 + 200 + 140 3 5 1 810 + 190 3 15 2 010 + 200 3 5 1 810 + 190 + 100 + 250 + 90 + 60 - 60 + 320 + 130 + 90 + 250 + 80 + 50 - 40 + 460 + 140 + 100 + 250 + 90 + 60 - 60 + 320 + 130 + 90 + 250 + 80 + 50 - 40 + 460 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 2 200 + 140 + 110 + 80 + 210 + 70 + 80 3 5 2 010 + 130 + 110 + 80 + 210 + 70 3 15 2 200 + 140 + 110 + 80 + 210 + 70 3 5 2 010 + 130 + 110 + 80 + 210 + 70 - 100 + 430 + 70 - 80 + 560 + 80 - 100 + 430 + 70 - 80 + 560 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 6/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 2 450 + 160 + 120 3 5 2 250 + 150 3 15 2 450 + 160 3 5 2 250 + 150 + 100 + 250 + 80 + 110 - 130 + 390 + 120 + 90 + 240 + 80 + 110 - 120 + 520 + 120 + 100 + 250 + 80 + 110 - 130 + 390 + 120 + 90 + 240 + 80 + 110 - 120 + 520 REV OVW (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 15 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 DOUBLE ADR/IR FAULT 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 TRIPLE ADR FAULT 3 15 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 ADR/IR DISAGREE 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 REV OVW (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 130m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 15 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 DOUBLE ADR/IR FAULT 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 TRIPLE ADR FAULT 3 15 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 ADR/IR DISAGREE 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 (1) Automatic Landing correction: add 150m - (2) Weight correction: subtract 150m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 7/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-34-00014134.0032001 / 01 DEC 14 Applicable to: MSN 0466-0472 NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 3 15 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 60m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 2 030 + 220 + 130 3 5 1 820 + 200 3 15 2 030 + 220 3 5 1 820 + 200 + 110 + 250 + 80 + 60 - 30 + 320 + 130 + 90 + 250 + 80 + 60 - 20 + 450 + 130 + 110 + 250 + 80 + 60 - 30 + 320 + 130 + 90 + 250 + 80 + 60 - 20 + 450 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 3 15 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 8/8 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page NAVIGATION SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 DOUBLE ADR/IR FAULT TRIPLE ADR FAULT ADR/IR DISAGREE 15 2 460 + 170 + 120 3 5 2 260 + 160 3 15 2 460 + 170 3 5 2 260 + 160 + 100 + 240 + 80 + 110 - 100 + 390 + 120 + 90 + 240 + 80 + 120 + 100 + 240 + 80 + 110 - 80 + 510 + 110 - 100 + 390 + 120 + 90 + 240 + 80 + 110 - 80 + 510 REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 15 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 DOUBLE ADR/IR FAULT 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 TRIPLE ADR FAULT 3 15 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 ADR/IR DISAGREE 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA UNRELIABLE SPEED INDICATION 3 15 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 DOUBLE ADR/IR FAULT 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 TRIPLE ADR FAULT 3 15 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 ADR/IR DISAGREE 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 150m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-36 1/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-36-00014137.0055001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 BLEED SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 480 + 150 + 80 + 50 + 130 + 40 + 20 - 20 + 440 3 15 1 550 + 160 + 80 + 50 + 130 + 50 + 30 - 20 + 540 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 860 + 180 + 130 + 90 + 240 + 80 + 50 - 50 + 260 3 15 2 010 + 200 + 140 + 100 + 250 + 90 + 60 - 60 + 320 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 060 + 130 + 110 + 70 + 210 + 70 + 70 - 80 + 340 3 15 2 200 + 140 + 110 + 80 + 210 + 70 + 80 - 100 + 430 (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-36 2/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page BLEED SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 290 + 150 + 110 + 90 + 240 + 70 + 100 - 110 + 310 3 15 2 450 + 160 + 120 + 100 + 250 + 80 + 110 - 130 + 390 REV OVW (1) Automatic Landing correction: add 120m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 720 + 280 + 160 + 150 + 410 + 120 + 160 - 150 + 160 3 15 3 010 + 310 + 180 + 170 + 440 + 140 + 210 - 190 + 200 REV OVW (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 3 970 + 280 + 170 + 180 + 590 + 160 + 740 - 430 + 160 3 15 4 370 + 310 + 170 + 200 + 620 + 170 + 870 - 510 + 210 (1) Automatic Landing correction: add 140m - (2) Weight correction: subtract 150m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-36 3/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-36-00014137.0051001 / 28 FEB 14 Applicable to: MSN 0466-0700 BLEED SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 480 + 160 + 80 + 50 + 130 + 50 + 20 - 10 + 440 3 15 1 560 + 170 + 80 + 50 + 130 + 50 + 20 - 10 + 540 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 1 870 + 200 + 130 + 90 + 240 + 80 + 50 - 20 + 260 3 15 2 030 + 220 + 130 + 110 + 250 + 80 + 60 - 30 + 320 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 070 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 340 3 15 2 210 + 150 + 110 + 80 + 210 + 70 + 80 - 70 + 420 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-36 4/4 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page BLEED SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 3 - MEDIUM Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 290 + 160 + 120 + 90 + 240 + 80 + 90 - 80 + 310 3 15 2 460 + 170 + 120 + 100 + 240 + 80 + 110 - 100 + 390 REV OVW (1) Automatic Landing correction: add 100m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 2 720 + 290 + 170 + 150 + 400 + 130 + 150 - 120 + 160 3 15 3 030 + 330 + 180 + 170 + 430 + 140 + 200 - 150 + 210 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE The following ECAM alerts with Ice Accretion: -WING LEAK -ENG BLEED LEAK -ABNORM BLEED CONFIG -BLEED LO TEMP WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 3 910 + 300 + 160 + 180 + 580 + 150 + 680 - 340 + 160 3 15 4 300 + 330 + 180 + 210 + 600 + 170 + 790 - 410 + 210 (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 1/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-70-00014135.0063001 / 28 FEB 14 Applicable to: MSN 0232-0361, 0968-1118 ENGINE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 1 450 + 140 + 80 + 50 + 130 + 50 + 20 - 20 + 730 SHUTDOWN with damage but no Ice Accretion 3 5 1 450 + 140 + 80 + 50 + 130 + 50 + 20 - 20 + 730 SHUTDOWN with damage and Ice Accretion 3 15 1 590 + 150 + 90 + 50 + 130 + 50 + 30 - 30 + 570 THR LEVER FAULT/ DISAGREE 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 10 + 700 REV UNLOCKED with buffet 2 25 1 680 + 170 N/A + 60 + 140 + 50 + 30 - 30 + 630 REV UNLOCKED without buffet 3 5 1 430 + 150 + 70 + 50 + 130 + 40 + 20 - 20 + 700 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 1 870 + 210 + 150 + 100 + 260 + 80 + 70 - 60 + 460 SHUTDOWN with damage but no Ice Accretion 3 5 1 870 + 210 + 150 + 100 + 260 + 80 + 70 - 60 + 460 SHUTDOWN with damage and Ice Accretion 3 15 2 100 + 220 + 150 + 110 + 260 + 100 + 80 - 80 + 320 THR LEVER FAULT/ DISAGREE 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 60 - 10 + 460 REV UNLOCKED with buffet 2 25 2 260 + 230 N/A + 120 + 270 + 90 + 70 - 70 + 350 REV UNLOCKED without buffet 3 5 1 810 + 190 + 130 + 90 + 250 + 80 + 50 - 40 + 460 (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 2/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ENGINE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 2 080 + 140 + 120 + 80 + 210 + 70 + 80 - 110 + 570 SHUTDOWN with damage but no Ice Accretion 3 5 2 080 + 140 + 120 + 80 + 210 + 70 + 80 - 110 + 570 SHUTDOWN with damage and Ice Accretion 3 15 2 290 + 150 + 120 + 90 + 220 + 70 + 90 - 120 + 440 THR LEVER FAULT/ DISAGREE 3 5 2 030 + 130 + 110 + 70 + 210 + 70 + 80 - 60 + 560 REV UNLOCKED with buffet 2 25 2 410 + 150 N/A + 90 + 220 + 70 + 90 - 110 + 510 REV UNLOCKED without buffet 3 5 2 010 + 130 + 110 + 80 + 210 + 70 + 70 - 80 + 560 REV OVW (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 820m 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 2 330 + 170 + 140 + 90 + 250 + 80 + 120 - 150 + 530 SHUTDOWN with damage but no Ice Accretion 3 5 2 330 + 170 + 140 + 90 + 250 + 80 + 120 - 150 + 530 SHUTDOWN with damage and Ice Accretion 3 15 2 560 + 170 + 130 + 100 + 250 + 90 + 130 - 180 + 400 THR LEVER FAULT/ DISAGREE 3 5 2 280 + 150 + 120 + 90 + 250 + 80 + 110 - 100 + 520 REV UNLOCKED with buffet 2 25 2 690 + 170 N/A + 100 + 250 + 90 + 130 - 150 + 460 REV UNLOCKED without buffet 3 5 2 250 + 150 + 120 + 90 + 240 + 80 + 110 - 120 + 520 (1) Automatic Landing correction: add 130m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 3/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ENGINE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 2 850 + 330 + 220 + 160 + 460 + 150 + 240 - 210 + 280 SHUTDOWN with damage but no Ice Accretion 3 5 2 850 + 330 + 220 + 160 + 460 + 150 + 240 - 210 + 280 SHUTDOWN with damage and Ice Accretion 3 15 3 190 + 350 + 210 + 180 + 470 + 150 + 250 - 270 + 200 THR LEVER FAULT/ DISAGREE 3 5 2 760 + 300 + 190 + 160 + 450 + 130 + 210 - 130 + 270 REV UNLOCKED with buffet 2 25 3 450 + 350 N/A + 190 + 470 + 160 + 260 - 250 + 230 REV UNLOCKED without buffet 3 5 2 720 + 300 + 190 + 150 + 430 + 130 + 200 - 150 + 280 REV OVW (1) Automatic Landing correction: add 160m - (2) Weight correction: subtract 130m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 340m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 4 240 + 350 + 210 + 190 + 590 + 170 + 870 - 640 + 280 SHUTDOWN with damage but no Ice Accretion 3 5 4 240 + 350 + 210 + 190 + 590 + 170 + 870 - 640 + 280 SHUTDOWN with damage and Ice Accretion 3 15 4 570 + 360 + 200 + 200 + 590 + 180 + 880 - 700 + 200 THR LEVER FAULT/ DISAGREE 3 5 4 340 + 270 + 190 + 180 + 680 + 170 + 1 230 - 690 + 270 REV UNLOCKED with buffet 2 25 4 890 + 340 N/A + 230 + 640 + 190 + 990 - 600 + 230 REV UNLOCKED without buffet 3 5 4 080 + 300 + 180 + 190 + 610 + 160 + 870 - 470 + 280 (1) Automatic Landing correction: add 160m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 4/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Ident.: PER-70-00014135.0055001 / 28 FEB 14 Applicable to: MSN 0466-0700 ENGINE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 6 - DRY Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 1 450 + 150 + 80 + 50 + 130 + 50 + 20 - 10 + 740 SHUTDOWN with damage but no Ice Accretion 3 5 1 450 + 150 + 80 + 50 + 130 + 50 + 20 - 10 + 740 SHUTDOWN with damage and Ice Accretion 3 15 1 590 + 160 + 90 + 50 + 130 + 50 + 30 - 10 + 590 THR LEVER FAULT/ DISAGREE 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 REV UNLOCKED with buffet 2 25 1 690 + 180 N/A + 60 + 140 + 50 + 30 - 10 + 620 REV UNLOCKED without buffet 3 5 1 430 + 160 + 80 + 50 + 130 + 40 + 20 - 10 + 690 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 70m - (2) Weight correction: subtract 40m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 310m 5 - GOOD Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 1 870 + 220 + 150 + 100 + 250 + 90 + 70 - 30 + 470 SHUTDOWN with damage but no Ice Accretion 3 5 1 870 + 220 + 150 + 100 + 250 + 90 + 70 - 30 + 470 SHUTDOWN with damage and Ice Accretion 3 15 2 110 + 240 + 150 + 110 + 270 + 90 + 70 - 50 + 340 THR LEVER FAULT/ DISAGREE 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 REV UNLOCKED with buffet 2 25 2 270 + 250 N/A + 120 + 270 + 90 + 70 - 50 + 350 REV UNLOCKED without buffet 3 5 1 820 + 200 + 130 + 90 + 250 + 80 + 60 - 20 + 450 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 600m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 5/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ENGINE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 4 - GOOD TO MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 2 080 + 150 + 120 + 80 + 210 + 70 + 80 - 70 + 580 SHUTDOWN with damage but no Ice Accretion 3 5 2 080 + 150 + 120 + 80 + 210 + 70 + 80 - 70 + 580 SHUTDOWN with damage and Ice Accretion 3 15 2 290 + 160 + 120 + 90 + 220 + 80 + 90 - 90 + 450 THR LEVER FAULT/ DISAGREE 3 5 2 030 + 140 + 110 + 80 + 210 + 70 + 80 - 60 + 560 REV UNLOCKED with buffet 2 25 2 410 + 150 N/A + 90 + 210 + 80 + 90 - 80 + 500 REV UNLOCKED without buffet 3 5 2 020 + 140 + 110 + 80 + 210 + 70 + 70 - 50 + 560 TEMP SLOPE REV OVW (1) Automatic Landing correction: add 80m - (2) Weight correction: subtract 70m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 1 830m 3 - MEDIUM Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 2 330 + 180 + 140 + 90 + 250 + 90 + 120 - 110 + 530 SHUTDOWN with damage but no Ice Accretion 3 5 2 330 + 180 + 140 + 90 + 250 + 90 + 120 - 110 + 530 SHUTDOWN with damage and Ice Accretion 3 15 2 560 + 180 + 140 + 100 + 250 + 90 + 130 - 130 + 410 THR LEVER FAULT/ DISAGREE 3 5 2 280 + 160 + 120 + 90 + 250 + 80 + 110 - 100 + 510 REV UNLOCKED with buffet 2 25 2 700 + 180 N/A + 100 + 250 + 90 + 120 - 120 + 460 REV UNLOCKED without buffet 3 5 2 260 + 160 + 120 + 90 + 240 + 80 + 110 - 80 + 510 (1) Automatic Landing correction: add 90m - (2) Weight correction: subtract 80m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 030m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 6/6 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK Continued from the previous page ENGINE SYSTEM The Reference Distance (REF DIST) considers : Sea Level (SL), ISA, no wind, no slope, no engine reverse thrust, manual (1) landing , maximum manual braking, VAPP = VREF+ΔVREF without APPR COR. 2 - MEDIUM TO POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE REV OVW FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 2 870 + 350 + 220 + 170 + 460 + 140 + 240 - 160 + 280 SHUTDOWN with damage but no Ice Accretion 3 5 2 870 + 350 + 220 + 170 + 460 + 140 + 240 - 160 + 280 SHUTDOWN with damage and Ice Accretion 3 15 3 210 + 370 + 210 + 180 + 460 + 160 + 250 - 210 + 210 THR LEVER FAULT/ DISAGREE 3 5 2 760 + 320 + 200 + 160 + 450 + 140 + 210 - 140 + 270 REV UNLOCKED with buffet 2 25 3 440 + 360 N/A + 190 + 460 + 160 + 250 - 190 + 240 REV UNLOCKED without buffet 3 5 2 730 + 320 + 190 + 160 + 420 + 130 + 190 - 120 + 280 REV OVW (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 120m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 2 350m 1 - POOR Corrections on Landing Distance (m) FAILURE WGT (2) SPD ALT WIND TEMP SLOPE FLAPS REF Per Per Per Per 1% Per Thrust If OVW LEVER DIST 10T 1000ft Per 10°C ΔVREF Per 5kt Down Reverser PROC for (m) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 4 220 + 370 + 210 + 190 + 580 + 170 + 840 - 500 + 280 SHUTDOWN with damage but no Ice Accretion 3 5 4 220 + 370 + 210 + 190 + 580 + 170 + 840 - 500 + 280 SHUTDOWN with damage and Ice Accretion 3 15 4 560 + 380 + 200 + 210 + 590 + 170 + 850 - 550 + 210 THR LEVER FAULT/ DISAGREE 3 5 4 260 + 310 + 190 + 190 + 660 + 170 + 1 100 - 580 + 270 REV UNLOCKED with buffet 2 25 4 780 + 360 N/A + 230 + 620 + 190 + 890 - 470 + 240 REV UNLOCKED without buffet 3 5 4 020 + 320 + 180 + 190 + 600 + 150 + 790 - 380 + 280 (1) Automatic Landing correction: add 110m - (2) Weight correction: subtract 140m per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 3 550m TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 PER-E 1/8 IN FLIGHT PERFORMANCE 01 DEC 14 QUICK REFERENCE HANDBOOK CEILINGS Ident.: PER-E-00010707.0011001 / 11 FEB 11 Applicable to: MSN 0466-0700 ONE ENGINE OUT GROSS CEILING at LONG RANGE and GREEN DOT SPEEDS Pack Flow Hi – Anti ice OFF CORRECTIONS ENGINE ANTI ICE ON TOTAL ANTI ICE ON LONG RANGE -700 ft -1 800 ft GREEN DOT -400 ft -1 500 ft TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 PER-E 2/8 IN FLIGHT PERFORMANCE 01 DEC 14 QUICK REFERENCE HANDBOOK CEILINGS Ident.: PER-E-00010707.0024001 / 11 FEB 11 Applicable to: MSN 0232-0361, 0968-1118 ONE ENGINE OUT GROSS CEILING at LONG RANGE and GREEN DOT SPEEDS Pack Flow Hi – Anti ice OFF CORRECTIONS ENGINE ANTI ICE ON TOTAL ANTI ICE ON LONG RANGE -800 ft -1 800 ft GREEN DOT -500 ft -1 200 ft TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-E 3/8 01 DEC 14 GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED Ident.: PER-E-00010708.0015001 / 11 FEB 11 Applicable to: MSN 0232-0361, 0968-1118 ONE ENGINE OUT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-E 4/8 01 DEC 14 GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED Ident.: PER-E-00010708.0018001 / 11 FEB 11 Applicable to: MSN 0466-0700 ONE ENGINE OUT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK CRUISE AT LONG RANGE CRUISE SPEED Ident.: PER-E-00010709.0018001 / 11 FEB 11 Applicable to: MSN 0466-0700 ONE ENGINE OUT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-E 5/8 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK CRUISE AT LONG RANGE CRUISE SPEED Ident.: PER-E-00010709.0015001 / 11 FEB 11 Applicable to: MSN 0232-0361, 0968-1118 ONE ENGINE OUT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-E 6/8 01 DEC 14 IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK IN CRUISE QUICK CHECK LONG RANGE Ident.: PER-E-00010710.0018001 / 16 MAR 11 Applicable to: MSN 0466-0700 ONE ENGINE OUT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-E 7/8 01 DEC 14 IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK IN CRUISE QUICK CHECK LONG RANGE Ident.: PER-E-00010710.0015001 / 16 MAR 11 Applicable to: MSN 0232-0361, 0968-1118 ONE ENGINE OUT TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-E 8/8 01 DEC 14 PER-G 1/10 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK OPTIMUM & MAXIMUM ALTITUDES Ident.: PER-G-00010713.0008001 / 01 OCT 12 Applicable to: MSN 0466-0700 ALL ENGINES CORRECTIONS ENGINE ANTI ICE ON TOTAL ANTI ICE ON PACK FLOW HI OR/AND CARGO COOL ON ≤ ISA + 9 -100 ft -300 ft -400 ft ISA + 15 -1 100 ft -1 300 ft -600 ft ISA + 20 -1 300 ft -1 700 ft -1 200 ft TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-G 2/10 IN FLIGHT PERFORMANCE A330 01 DEC 14 QUICK REFERENCE HANDBOOK OPTIMUM & MAXIMUM ALTITUDES Ident.: PER-G-00010713.0011001 / 01 OCT 12 Applicable to: MSN 0232-0361, 0968-1118 ALL ENGINES CORRECTIONS ENGINE ANTI ICE ON TOTAL ANTI ICE ON PACK FLOW HI OR/AND CARGO COOL ON ≤ ISA + 11 -1 000 ft -2 000 ft -400 ft ISA + 15 -2 000 ft -2 700 ft -1 200 ft ISA + 20 -3 000 ft -3 600 ft -1 800 ft TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-G 3/10 01 DEC 14 IN CRUISE QUICK CHECK AT A GIVEN MACH NUMBER Ident.: PER-G-00010714.0018001 / 11 FEB 11 Applicable to: MSN 0466-0700 ALL ENGINES Note: THE"*" (IF ANY) MEANS THAT A STEP CLIMB OF 4 000 ft MUST BE FLOWN TO REACH THE CORRESPONDING FLIGHT LEVEL. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-G 4/10 01 DEC 14 IN CRUISE QUICK CHECK AT A GIVEN MACH NUMBER Ident.: PER-G-00010714.0015001 / 11 FEB 11 Applicable to: MSN 0232-0361, 0968-1118 ALL ENGINES TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-G 5/10 01 DEC 14 COST INDEX FOR LONG RANGE CRUISE SPEED Ident.: PER-G-00010715.0001001 / 08 FEB 13 Applicable to: MSN 0232-0361, 0968-1118 ALL ENGINES For a quick determination of the CILRC, use: ‐ CILRC = 30 kg/min in the FMGC, for aircraft in metric units. or ‐ CILRC= 40 (100 lb/h) in the FMGC, for aircraft in US units. COST INDEX FOR LONG RANGE CRUISE SPEED Ident.: PER-G-00010715.0005001 / 08 FEB 13 Applicable to: MSN 0466-0700 ALL ENGINES For a quick determination of the CILRC, use: ‐ CILRC = 40 kg/min in the FMGC, for aircraft in metric units. or ‐ CILRC = 53 (100 lb/h) in the FMGC, for aircraft in US units. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK STANDARD DESCENT Ident.: PER-G-00010716.0015001 / 11 FEB 11 Applicable to: MSN 0232-0361, 0968-1118 ALL ENGINES TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-G 6/10 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK STANDARD DESCENT Ident.: PER-G-00010716.0019001 / 11 FEB 11 Applicable to: MSN 0466-0700 ALL ENGINES TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-G 7/10 01 DEC 14 IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK QUICK DETERMINATION TABLE OF ALTERNATE FLIGHT PLANNING Ident.: PER-G-00010717.0015001 / 11 FEB 11 Applicable to: MSN 0232-0361, 0968-1118 ALL ENGINES TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-G 8/10 01 DEC 14 IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK QUICK DETERMINATION TABLE OF ALTERNATE FLIGHT PLANNING Ident.: PER-G-00010717.0018001 / 11 FEB 11 Applicable to: MSN 0466-0700 ALL ENGINES TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-G 9/10 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-G 10/10 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-H 1/2 01 DEC 14 IN CRUISE QUICK CHECK FL 100 LONG RANGE Ident.: PER-H-00010718.0015001 / 11 FEB 11 Applicable to: MSN 0232-0361, 0968-1118 FLIGHT WITHOUT CAB PRESS TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-H 2/2 01 DEC 14 IN CRUISE QUICK CHECK FL 100 LONG RANGE Ident.: PER-H-00010718.0018001 / 11 FEB 11 Applicable to: MSN 0466-0700 FLIGHT WITHOUT CAB PRESS TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-I 1/6 01 DEC 14 GROUND DISTANCE / AIR DISTANCE CONVERSION Ident.: PER-I-00010719.0001001 / 01 OCT 12 Applicable to: ALL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK IAS / MACH CONVERSION Ident.: PER-I-00010720.0001001 / 01 OCT 12 Applicable to: ALL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 2/6 01 DEC 14 IN FLIGHT PERFORMANCE A330 QUICK REFERENCE HANDBOOK ISA TEMPERATURE AND PRESSURE ALTITUDE CORRECTION Ident.: PER-I-00015042.0001001 / 28 FEB 14 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 3/6 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Applicable to: ALL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 4/6 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK WIND COMPONENT Ident.: PER-I-00014336.0001001 / 16 MAY 12 Applicable to: ALL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 5/6 01 DEC 14 A330 IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 6/6 01 DEC 14 A330 QUICK REFERENCE HANDBOOK OPERATIONAL DATA TABLE OF CONTENTS OPS 1/2 01 DEC 14 Severe Turbulence ........................................................................ OPS.01A Hydraulic Architecture.....................................................................OPS.02A Flight Controls Architecture............................................................ OPS.03A Required Equipment for CAT2 and CAT3...................................... OPS.04A TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK OPERATIONAL DATA TABLE OF CONTENTS Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS 2/2 01 DEC 14 OPS.01A OPERATIONAL DATA A330 01 DEC 14 QUICK REFERENCE HANDBOOK SEVERE TURBULENCE Ident.: OPS-00012057.0017001 / 21 NOV 11 Applicable to: MSN 0466-0700 Speed and Thrust Setting (N1) for Turbulence Speed FLIGHT LEVEL SPD or Mach 120 GROSS WEIGHT (1 000 kg) 130 140 150 160 170 180 190 200 210 220 230 240 410 0.8 89.2 90.1 91.1 92.1 93.5 95.2 - - - - - - - 390 0.8 88.2 88.9 89.7 90.6 91.6 92.6 94.0 95.7 - - - - - 370 0.8 87.3 87.9 88.6 89.3 90.1 91.0 91.9 92.9 94.3 95.9 - - - 350 260 85.2 85.9 86.6 87.4 88.2 89.0 90.0 90.9 91.9 93.1 94.6 96.1 - 330 260 83.9 84.5 85.2 85.9 86.7 87.6 88.5 89.4 90.4 91.4 92.4 93.7 95.0 310 260 82.4 83.1 83.8 84.5 85.2 86.0 86.8 87.8 88.8 89.8 90.8 91.9 92.9 290 260 81.0 81.6 82.2 83.0 83.7 84.5 85.3 86.1 87.1 88.1 89.1 90.1 91.2 270 260 79.8 80.3 80.9 81.5 82.2 83.0 83.8 84.7 85.5 86.4 87.4 88.4 89.5 250 260 78.2 78.7 79.4 80.1 80.8 81.4 82.2 83.0 83.9 84.9 85.8 86.7 87.7 200 240 71.4 72.1 72.9 73.7 74.5 75.5 76.5 77.5 78.5 79.6 80.8 81.8 83.0 150 240 67.5 68.2 68.9 69.6 70.5 71.4 72.3 73.3 74.2 75.2 76.3 77.5 78.5 100 240 63.4 64.1 64.9 65.6 66.5 67.4 68.4 69.3 70.2 71.1 72.1 73.2 74.3 50 240 59.4 60.2 60.9 61.6 62.4 63.3 64.2 65.2 66.1 67.1 68.1 69.2 70.3 SIGNS......................................................................................................................ON AUTO PILOT................................................................................................ KEEP ON A/THR (when thrust changes become excessive)................................ DISCONNECT DESCENT.................................................................................................. CONSIDER Consider descending to or below OPT FL in order to increase the margin to buffet FOR APPROACH: A/THR in managed speed................................................................................USE SEVERE TURBULENCE Ident.: OPS-00012057.0014001 / 21 NOV 11 Applicable to: MSN 0232-0361, 0968-1118 Speed and Thrust Setting (N1) for Turbulence Speed GROSS WEIGHT (1 000 kg) FLIGHT LEVEL SPD or Mach 120 130 140 150 160 170 180 190 200 210 220 230 240 410 0.8 78.0 78.8 79.8 80.8 81.8 83.4 85.4 - - - - - - 390 0.8 76.9 77.7 78.5 79.4 80.3 81.2 82.3 83.8 85.8 - - - - 370 0.8 76.0 76.6 77.4 78.1 78.9 79.7 80.6 81.5 82.5 84.0 - - - 350 260 74.2 74.8 75.5 76.3 77.1 78.0 78.8 79.7 80.6 81.7 82.9 84.3 - 330 260 72.9 73.5 74.1 74.8 75.6 76.5 77.4 78.3 79.2 80.1 81.1 82.2 83.5 310 260 71.3 72.1 72.9 73.6 74.3 75.0 75.9 76.8 77.7 78.7 79.7 80.6 81.7 290 260 69.8 70.5 71.3 72.2 73.0 73.8 74.5 75.4 76.3 77.2 78.2 79.3 80.2 270 260 68.7 69.3 70.0 70.7 71.6 72.5 73.2 74.1 75.0 75.9 76.7 77.6 78.8 250 260 67.3 67.8 68.4 69.1 69.9 70.7 71.6 72.5 73.4 74.3 75.2 76.0 76.9 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.01B OPERATIONAL DATA A330 01 DEC 14 QUICK REFERENCE HANDBOOK SEVERE TURBULENCE (Cont'd) Speed and Thrust Setting (N1) for Turbulence Speed GROSS WEIGHT (1 000 kg) FLIGHT LEVEL SPD or Mach 120 130 140 150 160 170 180 190 200 210 220 230 240 200 240 62.0 62.7 63.4 64.1 64.9 65.7 66.5 67.4 68.3 69.3 70.3 71.4 72.6 150 240 58.5 59.2 59.9 60.7 61.4 62.2 63.0 63.8 64.6 65.4 66.3 67.2 68.2 100 240 54.6 55.3 56.0 56.8 57.6 58.5 59.4 60.3 61.2 62.1 62.9 63.7 64.6 50 240 51.2 51.8 52.5 53.2 54.0 54.8 55.7 56.6 57.6 58.7 59.8 60.8 61.6 SIGNS......................................................................................................................ON AUTO PILOT................................................................................................ KEEP ON A/THR (when thrust changes become excessive)................................ DISCONNECT DESCENT.................................................................................................. CONSIDER Consider descending to or below OPT FL in order to increase the margin to buffet FOR APPROACH: A/THR in managed speed................................................................................USE TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPERATIONAL DATA A330 QUICK REFERENCE HANDBOOK HYDRAULIC ARCHITECTURE Ident.: OPS-00010722.0012001 / 01 DEC 14 Applicable to: MSN 0968-1118 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.02A 01 DEC 14 OPERATIONAL DATA A330 QUICK REFERENCE HANDBOOK HYDRAULIC ARCHITECTURE Ident.: OPS-00010722.0010001 / 01 DEC 14 Applicable to: MSN 0232-0361 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.02B 01 DEC 14 OPERATIONAL DATA A330 QUICK REFERENCE HANDBOOK HYDRAULIC ARCHITECTURE Ident.: OPS-00010722.0009001 / 01 DEC 14 Applicable to: MSN 0700 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.02C 01 DEC 14 OPERATIONAL DATA A330 QUICK REFERENCE HANDBOOK HYDRAULIC ARCHITECTURE Ident.: OPS-00010722.0008001 / 01 DEC 14 Applicable to: MSN 0466-0472 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.02D 01 DEC 14 OPERATIONAL DATA A330 QUICK REFERENCE HANDBOOK FLIGHT CONTROLS ARCHITECTURE Ident.: OPS-00010723.0001001 / 01 OCT 12 Applicable to: MSN 0232-0472 P = PRIM computers S = SEC computers → Arrows indicate the control reconfiguration priorities G B Y indicates the hydraulic source for each servo control MLA = Manoeuver load alleviation TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.03A 01 DEC 14 OPERATIONAL DATA A330 QUICK REFERENCE HANDBOOK FLIGHT CONTROLS ARCHITECTURE Ident.: OPS-00010723.0004001 / 01 OCT 12 Applicable to: MSN 0700-1118 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.03B 01 DEC 14 OPS.04A OPERATIONAL DATA A330 01 DEC 14 QUICK REFERENCE HANDBOOK REQUIRED EQUIPMENT FOR CAT2 AND CAT3 Ident.: OPS-00012527.0008001 / 01 DEC 14 Applicable to: MSN 0700-1118 CAPABILITY→ CAT 2 CAT 3 SINGLE CAT 3 DUAL 1 AP ENGAGED 1 AP ENGAGED 2 AP ENGAGED AUTO THRUST 0 1 1 FMA 1 2 2 ELECTRICALLY POWER SUPPLY SPLIT 0 0 1 PRIM 1 1 (N°1+N°2) or (N°1+N°3) SEC 1 1 2 RUDDER TRIM 1 1 2 HYDRAULIC CIRCUIT 2 2 3 PFD 2 2 2 DMC 2 2 2 1 1 2 1(1) 1(1) 1 ANTISKID 1(1) 1(1) 1 NOSEWHEEL STEERING 1(1) 1(1) 1 EQUIPMENT↓ AP FMGS FLIGHT WARNING MONITORED COMPUTER FOR FMA LDG BSCU CHANNEL CAPABILITY RADIO ALTIMETERS 1 (displayed on both sides) 2 2 ILS RECEIVER 2 2 2 GLS (2) RECEIVER (for GLS approach) 2 N/A N/A ATTITUDE INDICATION (PFD1/PFD2) N°1+N°2 N°1+N°2 N°1+N°2 2/2 2/2 3/3 1 for PM 2 2 ADR/IR BEAM EXCESSIVE DEVIATION TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.04B OPERATIONAL DATA A330 01 DEC 14 QUICK REFERENCE HANDBOOK CAPABILITY→ CAT 2 CAT 3 SINGLE CAT 3 DUAL AP DISCONNECT PB 2 2 2 "AP OFF" ECAM WARNING 1 1 2 "A/THR OFF" ECAM CAUTION 0 1 1 "AUTOLAND" LIGHT 1 1 1 EQUIPMENT↓ WINDSHIELD HEAT (L or NOT FMGS R windshield) MONITORED FOR FMA LDG WINDSHIELD WIPERS OR RAIN REPELLENT (if CAPABILITY activated) ND AUTO CALLOUT FUNCTION ATTITUDE INDICATION (STBY) 1 for PF 1 for PF 1 2 2 one is required for autoland 1 1 1 1 1 DH INDICATION 1 for PM (1) For automatic rollout , one is required. For autoland without automatic rollout, none is required. (2) GLS autoland is certified for CAT I minima, but the FMGES monitors the same equipments as for CAT2. Note: Flight crews are not expected to check the equipment list before approach. When an ECAM or local caution occurs, the crew should use the list to confirm the landing capability. On ground, the equipment list determines which approach category the aircraft will be able to perform at the next landing. Electrical power supply split: This ensures that each FMGEC is powered by an independent electrical source (AC and DC). Failure of antiskid and/or nosewheel steering mechanical parts are not monitored for landing capability. The DH will be displayed on the FMA, and the "Hundred Above" and "Minimum " auto callouts will be announced, provided that the DH value has been entered on the MCDU. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.04C OPERATIONAL DATA A330 01 DEC 14 QUICK REFERENCE HANDBOOK REQUIRED EQUIPMENT FOR CAT2 AND CAT3 Ident.: OPS-00012527.0001001 / 01 DEC 14 Applicable to: MSN 0232-0472 CAPABILITY→ CAT 2 CAT 3 SINGLE CAT 3 DUAL 1 AP ENGAGED 1 AP ENGAGED 2 AP ENGAGED AUTO THRUST 0 1 1 FMA 1 2 2 ELECTRICALLY POWER SUPPLY SPLIT 0 0 1 PRIM 1 1 (N°1+N°2) or (N°1+N°3) SEC 1 1 2 YAW DAMPER/RUDDER TRIM 1/1 1/1 2/2 HYDRAULIC CIRCUIT 2 2 3 PFD 2 2 2 DMC 2 2 2 1 1 2 1(1) 1(1) 1 ANTISKID 1(1) 1(1) 1 NOSEWHEEL STEERING 1(1) 1(1) 1 1 (displayed on both sides) 2 2 ILS RECEIVER 2 2 2 GLS (2) RECEIVER 2 N/A N/A N°1+N°2 N°1+N°2 N°1+N°2 2/2 2/2 3/3 1 for PM 2 2 EQUIPMENT↓ AP FMGS FLIGHT WARNING MONITORED COMPUTER FOR FMA LDG CAPABILITY BSCU CHANNEL RADIO ALTIMETERS (for GLS approach) ATTITUDE INDICATION (PFD1/PFD2) ADR/IR BEAM EXCESSIVE DEVIATION TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.04D OPERATIONAL DATA A330 01 DEC 14 QUICK REFERENCE HANDBOOK CAPABILITY→ CAT 2 CAT 3 SINGLE CAT 3 DUAL AP DISCONNECT PB 2 2 2 "AP OFF" ECAM WARNING 1 1 2 "A/THR OFF" ECAM CAUTION 0 1 1 "AUTOLAND" LIGHT 1 1 1 EQUIPMENT↓ RUDDER TRAVEL LIMIT SYSTEM NOT FMGS MONITORED WINDSHIELD HEAT (L or R windshield) FOR FMA LDG CAPABILITY WINDSHIELD WIPERS 1 required only for autoland with crosswind greater than 12 kt 1 for PF OR RAIN REPELLENT (if activated) ND AUTO CALLOUT FUNCTION ATTITUDE INDICATION (STBY) 1 for PF 1 2 2 one is required for autoland 1 1 1 1 1 DH INDICATION 1 for PM (1) For automatic rollout , one is required. For autoland without automatic rollout, none is required. (2) GLS autoland is certified for CAT I minima, but the FMGES monitors the same equipments as for CAT2. Note: Flight crews are not expected to check the equipment list before approach. When an ECAM or local caution occurs, the crew should use the list to confirm the landing capability. On ground, the equipment list determines which approach category the aircraft will be able to perform at the next landing. Electrical power supply split: This ensures that each FMGEC is powered by an independent electrical source (AC and DC). Failure of antiskid and/or nosewheel steering mechanical parts are not monitored for landing capability. The DH will be displayed on the FMA, and the "Hundred Above" and "Minimum " auto callouts will be announced, provided that the DH value has been entered on the MCDU. TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK OPERATIONS ENGINEERING BULLETINS LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN Identification OEB26 Issue 2 Title OEBPROC 1/2 01 DEC 14 Erroneous Radio Altimeter (RA) Height Indication ECAM Entry None Applicable to: ALL OEB33 Pack Flow Monitoring Issue 1 ECAM Entry None Applicable to: MSN 0232-0259, 0472-0700 OEB34 NAV ADR 1+2+3 FAULT ECAM Warning Undue Activation Issue 1 ECAM Entry NAV ADR 1+2+3 FAULT Applicable to: MSN 0232-0472 OEB47 ELEC EMER CONFIG Issue 1 ECAM Entry ELEC EMER CONFIG Applicable to: ALL OEB49 Abnormal V Alpha Prot Issue 2 ECAM Entry None Applicable to: ALL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK OPERATIONS ENGINEERING BULLETINS LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE OEBPROC 2/2 01 DEC 14 A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK 26.01A 01 DEC 14 RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB ERRONEOUS RADIO ALTIMETER (RA) HEIGHT INDICATION Ident.: OEBPROC-26-00013371.0001001 / 08 APR 14 Applicable to: ALL ECAM ENTRY None PROCEDURE: This bulletin is issued to remind operators of the possible consequences of an erroneous Radio Altimeter (RA) height indication. Erroneous RA height indication may have on aircraft systems, any of the effects listed in the OEB N°26. This OEB PROC is issued to provide flight crews with the following recommendations: During all phases of flight, the flight crew must monitor and crosscheck all primary flight parameters and FMA indications. During an ILS (or GLS) approach with AP engaged: In the event of an early/untimely FLARE and THR IDLE mode engagement (possibly associated with AUTOLAND warning and/or RETARD callout), the flight crew must: ‐ Immediately perform an automatic go-around (thrust levers set to TOGA), OR ‐ Immediately disconnect AP and set both FDs to OFF. If external visual references are sufficient, the approach may be continued manually. In case of Go-Around (automatic or manual), when climb gradient is established, reduce thrust without delay (thrust levers set to CLB detent). Note: ‐ If the flight crew does not immediately react, the angle-of-attack will increase and may reach the stall value. ‐ The auto-trim function may be inhibited. Reducing the thrust increases the pitch down authority. A significant longitudinal sidestick input may be required. During go-around: If SRS and GA TRK modes remain engaged and other guidance modes cannot be selected or engaged as expected: Note: ‐ At the thrust reduction altitude, LVR CLB will not be displayed on the FMA, ‐ ALT* and ALT will not engage at the FCU altitude. Disconnect APs. Set both FDs to OFF then ON. FDs revert to basic modes (HDG - V/S). Re-engage guidance modes as appropriate. For the approach that follows the go-around: Do not arm the G/S mode. Flight crews must report, in the technical logbook, any of the consequences of an erroneous RA height listed in the OEB N°26. END OF OEB26 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 OPERATIONS ENGINEERING BULLETINS A330 33.01A QUICK REFERENCE HANDBOOK 01 DEC 14 PACK FLOW MONITORING Ident.: OEBPROC-33-00013540.0001001 / 18 MAR 11 Applicable to: MSN 0232-0259, 0472-0700 ECAM ENTRY None PROCEDURE Apply the following paper procedures if flying in suspected icing conditions above FL 300: IF SUSPECTED ICING CONDITIONS ABOVE FL 300: PACK FLOW (A330 and A340-200/-300)..................................................NORM AIR FLOW (A340-500/-600)...................................................................... NORM ECAM BLEED PAGE............................................................................. SELECT PACK 1 and PACK 2 FLOW............................................................... MONITOR IF PACK 1 AND PACK 2 FLOW INDICATION BELOW 90 %: 90 % flow corresponds to 11 o'clock position on the display SPEED............................................................... TEMPORARILY INCREASE CABIN TEMPERATURE.................................... TEMPORARILY INCREASE Increase cabin temperature by 2 °C to 3 °C. IF PACK 1 AND PACK 2 FLOW INDICATION AMBER XX: CABIN ALTITUDE.......................................................................... MONITOR CABIN VERTICAL SPEED.............................................................MONITOR IF CABIN ALTITUDE INCREASES: FLIGHT LEVEL REDUCTION................................................. CONSIDER WHEN CABIN ALTITUDE IS STABILIZED: PACK CONTROLLER 1 AND 2................................................RESET Reset the pack controllers, one at a time, using the reset pb on the overhead panel, to clear the amber XX. IF "AIR PACK 1 REGUL FAULT" AND "AIR PACK 2 REGUL FAULT" ECAM CAUTIONS ARE DISPLAYED WITH THE LINE "PACK 1 (2) IN BYPASS MODE": CABIN ALTITUDE.......................................................................... MONITOR CABIN VERTICAL SPEED.............................................................MONITOR IF CABIN ALTITUDE INCREASES: FLIGHT LEVEL REDUCTION................................................. CONSIDER WHEN CABIN ALTITUDE IS STABILIZED: PACK CONTROLLER 1 AND 2................................................RESET Reset the pack controllers, one at a time, using the reset pb on the overhead panel, to clear the "AIR PACK 1 REGUL FAULT" and "AIR PACK 2 REGUL FAULT" ECAM cautions. END OF OEB33 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK 34.01A 01 DEC 14 NAV ADR 1+2+3 FAULT ECAM WARNING UNDUE ACTIVATION Ident.: OEBPROC-34-00013552.0009001 / 18 MAR 11 Applicable to: MSN 0232-0472 ECAM ENTRY NAV ADR 1+2+3 FAULT PROCEDURE In the case of a NAV ADR 1+2+3 FAULT ECAM warning, apply the ADR 1+2+3 FAULT procedure. Refer to ABN-34 ADR 1+2+3 FAULT. END OF OEB34 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK 47.01A 01 DEC 14 RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB ELEC EMER CONFIG Ident.: OEBPROC-47-00015425.0001001 / 17 NOV 14 Applicable to: ALL ECAM ENTRY ELEC EMER CONFIG PROCEDURE Apply the ELEC EMER CONFIG ECAM procedure. For slats extension, before setting the LAND RECOVERY pb-sw to ON, press the RAT MAN ON pb to extend the RAT and resume application of the ELEC EMER CONFIG ECAM procedure. END OF OEB47 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 OPERATIONS ENGINEERING BULLETINS 49.01A QUICK REFERENCE HANDBOOK 01 DEC 14 RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB ABNORMAL V ALPHA PROT Ident.: OEBPROC-49-00015964.0001001 / 01 DEC 14 Applicable to: ALL ECAM ENTRY None PROCEDURE CAUTION Monitor the Alpha Prot strip when it is visible When the Mach increases, if the Alpha Prot strip (black and amber) continuously increases and exceeds Green Dot (GD) speed in a stabilized wings-level flight path (without an increase in load factor): ONE ADR .........................................................................................KEEP ON TWO ADRs.................................................................................................OFF CAUTION RISK OF ERRONEOUS DISPLAY OF THE VSW STRIP (RED AND BLACK) AND RISK OF UNDUE STALL WARNING SPEED.............................................................................DO NOT INCREASE FPV USE........................................................................................ CONSIDER CAPT (F/O) EFIS DMC ................................................................... AS RQRD When at or above Safety altitude: ALTITUDE...................................................................DO NOT INCREASE AT ANY TIME, with a speed above VLS, if the aircraft goes to a CONTINUOUS NOSE DOWN PITCH RATE that cannot be stopped with backward sidestick inputs, IMMEDIATELY APPLY: ONE ADR ...................................................................................... KEEP ON TWO ADRs.............................................................................................. OFF END OF OEB49 TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES C2 01 DEC 14 EMERGENCY EVACUATION Ident.: 00010643.0001001 / 08 FEB 13 Applicable to: MSN 0232-0472 AIRCRAFT/PARKING BRK.......................................................................... STOP/ON ATC (VHF 1)....................................................................................................NOTIFY CABIN CREW (PA)........................................................................................... ALERT ΔP (only if MAN CAB PR has been used)............................................ CHECK ZERO If not zero, MODE SEL on MAN, V/S CTL FULL UP. ENG MASTERS (ALL)...........................................................................................OFF FIRE Pushbuttons (ALL: ENG and APU)........................................................... PUSH AGENTS (ENG and APU)............................................................................AS RQRD If evacuation required: EVACUATION........................................................................................... INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . If evacuation not required: CABIN CREW and PASSENGERS (PA)................................................... NOTIFY EMERGENCY EVACUATION Ident.: 00010643.0002001 / 08 FEB 13 Applicable to: MSN 0700-1118 AIRCRAFT/PARKING BRK.......................................................................... STOP/ON ATC (VHF1)..................................................................................................... NOTIFY CABIN CREW (PA)........................................................................................... ALERT ΔP (only if MAN CAB PR has been used)............................................ CHECK ZERO If not zero, MODE SEL on MAN, V/S CTL FULL UP. ENG MASTERS (ALL)...........................................................................................OFF FIRE Pushbuttons (ALL: ENG and APU)........................................................... PUSH AGENTS (ENG and APU)............................................................................AS RQRD If evacuation required: EVACUATION........................................................................................... INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb . ALL BATs......................................................................................................... OFF If evacuation not required: CABIN CREW and PASSENGERS (PA)................................................... NOTIFY TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 01 DEC 14 C3 NORMAL PROCEDURES A330 01 DEC 14 QUICK REFERENCE HANDBOOK BEFORE START APPROACH Ident.: 00010684.0001001 / 22 MAY 13 Applicable to: ALL Ident.: 00010692.0001001 / 18 NOV 14 Applicable to: ALL COCKPIT PREP..................... COMPLETED (BOTH) GEAR PINS and COVERS.......................REMOVED SIGNS.........................................................ON/AUTO ADIRS ............................................................... NAV FUEL QUANTITY....................................... _____KG TO DATA............................................................. SET BARO REF.................................. _____SET (BOTH) WINDOWS/DOORS........................CLOSED (BOTH) BEACON................................................................ON THR LEVERS .................................................... IDLE PARKING BRAKE...................................... AS RQRD BRIEFING............................................. CONFIRMED ECAM STATUS.........................................CHECKED SEAT BELTS.........................................................ON BARO REF.................................. _____SET (BOTH) MINIMUM.................................... _____SET (BOTH) ENG START SEL ......................................AS RQRD AFTER START Ident.: 00010686.0001001 / 07 AUG 13 Applicable to: ALL ANTI ICE.................................................... AS RQRD PACK 2...................................................... AS RQRD ECAM STATUS ........................................CHECKED PITCH TRIM............................................. _____SET RUDDER TRIM ............................................... ZERO GROUND EQUIPMENT............................REMOVED BEFORE TAKEOFF Ident.: 00010687.0001001 / 01 DEC 14 Applicable to: ALL FLIGHT CONTROLS................... CHECKED (BOTH) FLT INST .................................... CHECKED (BOTH) BRIEFING............................................. CONFIRMED FLAP SETTING....................... CONF _____ (BOTH) V1. VR. V2/FLX TEMP ...................... _____ (BOTH) ATC .....................................................................SET ECAM MEMO....................................... TO NO BLUE ‐ ‐ ‐ ‐ SIGNS ON SPLRS ARMED CABIN READY FLAPS TO ‐ AUTO BRK MAX ‐ TO CONFIG NORM TAKEOFF RWY................. _____CONFIRM (BOTH) CABIN CREW ............................................ADVISED TCAS ...............................................................TA/RA ENGINE START SEL ................................AS RQRD PACKS.................................................................OFF AFTER TAKEOFF / CLIMB Ident.: 00010689.0001001 / 01 DEC 14 Applicable to: ALL LDG GEAR............................................................ UP FLAPS...................................................RETRACTED PACKS...................................................................ON BARO REF.................................. _____SET (BOTH) LANDING Ident.: 00010694.0001001 / 18 NOV 14 Applicable to: ALL CABIN CREW............................................. ADVISED A/THR ....................................................SPEED/OFF AUTOBRAKE............................................. AS RQRD ECAM MEMO.................................... LDG NO BLUE ‐ SIGNS ON ‐ CABIN READY ‐ LDG GEAR DN ‐ FLAPS LDG ‐ SPLRS ARMED AFTER LANDING Ident.: 00010695.0002001 / 22 MAY 13 Applicable to: ALL FLAPS...................................................RETRACTED SPOILERS............................................... DISARMED APU ................................................................START RADAR...................................................... OFF/STBY PREDICTIVE WINDSHEAR SYSTEM................ OFF Consider ONE ENGINE TAXI PARKING Ident.: 00010696.0001001 / 20 MAY 13 Applicable to: ALL APU BLEED.......................................................... ON ENGINES.............................................................OFF SEAT BELTS.......................................................OFF EXT LT ......................................................AS RQRD FUEL PUMPS......................................................OFF PARK BRK AND CHOCKS........................ AS RQRD SECURING THE AIRCRAFT Ident.: 00010697.0001001 / 22 MAY 13 Applicable to: ALL ADIRS .................................................................OFF OXYGEN..............................................................OFF APU BLEED ....................................................... OFF EMER EXIT LT ...................................................OFF SIGNS..................................................................OFF APU AND BAT.................................................... OFF Consider COLD WEATHER TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE A330 NORMAL PROCEDURES QUICK REFERENCE HANDBOOK TAKEOFF CG / TRIM POS Ident.: 00012519.0001001 / 14 MAR 12 Applicable to: ALL TAM A330 FLEET AS PER AIRCRAFT ALLOCATION TABLE C3 01 DEC 14
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