A330 QRH

QUICK REFERENCE HANDBOOK 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE Intentionally left blank A330-243F TRANSMITTAL LETTER QUICK REFERENCE HANDBOOK 1/2 06 MAR 17 Issue date: 06 MAR 17 This is the QUICK REFERENCE HANDBOOK major event publication at issue date 06 MAR 17 for the A330-243F and replacing last issue dated 18 JAN 17 QRH PAGE GEN.02A PROVIDES ADDITIONAL GUIDANCE TO MANAGE THE QRH UPDATES. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F TRANSMITTAL LETTER QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 06 MAR 17 1/2 FILING INSTRUCTIONS A330-243F 06 MAR 17 QUICK REFERENCE HANDBOOK Please incorporate this major event revision as follow: Localization Subsection Title * * PLP-LESS LIST OF EFFECTIVE SECTIONS/SUBSECTIONS PLP-LEDU LIST OF EFFECTIVE DOCUMENTARY UNITS ABN-PLP-TOC TABLE OF CONTENTS ABN-PLP-SOH SUMMARY OF HIGHLIGHTS ABN-80 Miscellaneous C2 Back-cover page interior * Preliminary pages that may be removed from the QRH binder TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE Remove Insert Rev. Date ALL 06 MAR 17 ALL 06 MAR 17 ALL 06 MAR 17 ALL 06 MAR 17 ALL 06 MAR 17 ALL 06 MAR 17 A330-243F FILING INSTRUCTIONS QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 06 MAR 17 A330-243F QUICK REFERENCE HANDBOOK (1) M R R Localization PLP-LESS PLP-LETDU GEN ABN-22 ABN-24 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 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 1/2 06 MAR 17 Rev. Date 06 MAR 17 05 NOV 13 30 JUN 15 30 JUN 15 30 JUN 15 06 DEC 16 06 DEC 16 18 JAN 17 18 JAN 17 06 DEC 16 19 MAR 13 18 JAN 17 06 DEC 16 18 JAN 17 18 JAN 17 06 MAR 17 06 DEC 16 06 DEC 16 05 MAR 14 07 JUN 16 18 JAN 17 05 MAR 14 05 MAR 14 05 MAR 14 30 JUN 15 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 05 MAR 14 06 DEC 16 18 JAN 17 A330-243F QUICK REFERENCE HANDBOOK PRELIMINARY PAGES LIST OF EFFECTIVE SECTIONS/SUBSECTIONS Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 06 MAR 17 A330-243F QUICK REFERENCE HANDBOOK M (1) PRELIMINARY PAGES LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS Localization DU Title DU identification 1/2 05 NOV 13 DU date ABN-31 Display Unit Failure 00014692.0002001 12 MAR 13 Criteria: S30653, A330 Applicable to: ALL Impacted DU: 00010550 Display Unit Failure Reason for issue: The "Display Unit Failure" procedure is amended to introduce a temporary procedure and its associated corrective action in the case of Display Unit (DU ) brightness reduction to the minimum. Due to an issue with the backlight monitoring function of the Enhanced Display Unit (EDU) a DU might have its brightness spuriously set to the minimum. To recover the display, the flight crew has to set the affected DU brightness knob to OFF then ON. 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 System 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK PRELIMINARY PAGES LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 05 NOV 13 A330-243F QUICK REFERENCE HANDBOOK PRELIMINARY PAGES AIRCRAFT ALLOCATION TABLE 1/2 06 JAN 15 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 1368 N330QT 330-243F 1380 N331QT 330-243F 1428 N332QT 330-243F 1448 N334QT 330-243F 1534 N335QT 330-243F (1) Evolution code : N=New, R=Revised TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK PRELIMINARY PAGES AIRCRAFT ALLOCATION TABLE Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 2/2 06 JAN 15 A330-243F QUICK REFERENCE HANDBOOK (1) M MODIFICATION D40487 1/4 PRELIMINARY PAGES LIST OF MODIFICATIONS Linked SB Incorp. Date 18 JAN 17 Title 19 MAR 13 Applicable to: ALL D42829 FUEL - APU FUEL PUMP SYSTEM - PREVENT AN ELECTRICAL ESS NETWORK "OVERLOAD" (A330) 19 MAR 13 Applicable to: ALL D45352 COMMUNICATIONS - GENERAL - BASIC PROVISIONS FOR IN FLIGHT ENTERTAINMENT SYSTEM A330/A340-200/300 19 MAR 13 Applicable to: ALL D48233 EQUIPMENT/FURNISHINGS-MIS. EMER. EQPT.- INSTALL HONEYWELL ELT WITH REMOTE CONTROL PANEL IN THE COCKPIT 19 MAR 13 Applicable to: ALL D48352 COMMUNICATIONS - CIDS - INTRODUCE THE COMMUNAL DIRECTOR FOR LONG RANGE PAX AND FREIGHTER A/C'S WITH INTEGRATED SDF 19 MAR 13 Applicable to: ALL H13959 E/F.: COURIER AREA - DEFINE FLEXIBLE LAYOUT DEFINITION IN ADDITION TO THE TYPE CERTIFICATE FOR A330-200F 19 MAR 13 ICE AND RAIN PROTECTION - WING ICE PROTECTION RELOCATE OUTBOARD VALVE TO INBOARD POSITION 19 MAR 13 FUEL - FCMS - INSTALL FCMC STAGE 9.0 19 MAR 13 GENERAL-DESIGN WEIGHTS-CERTIFY A330-200 WV050 MTOW 230T, MLW 180T, MZFW 168T WITH REVISED A/C DESIGN SERVICE GOAL 19 MAR 13 FUEL-TANKS- REMOVE OF THE CENTRE TANK CAPABILITY 21 SEP 15 AUTOFLIGHT-DEFINE QFE/QNH SETTING 19 MAR 13 Applicable to: ALL S12358 INDICATING/RECORDING SYSTEMS-FMGEC- REPLACE METERS BY FEET 19 MAR 13 Applicable to: ALL S12410 FLIGHT CONTROLS - CHANGE WIRING OF FCPC1 AND FCSC1 FAULT INDICATOR LIGHTS 19 MAR 13 Applicable to: ALL S12968 ENGINE FUEL AND CONTROL - GENERAL - PROVIDE DERATED TAKE OFF FACILITY FOR R.R. ENGINES 19 MAR 13 Applicable to: ALL S13133 NAVIGATION - WEATHER RADAR SYSTEM - ACTIVATE DUAL PREDICTIVE WINDSHEAR RADAR SYSTEM, COLLINS 19 MAR 13 Applicable to: ALL S13217 ICE AND RAIN PROTECTION - WINDSHIELD RAIN PROTECTION - DEACTIVATE RAIN REPELLENT SYSTEM 19 MAR 13 Applicable to: ALL S13313 FUEL - DISTRIBUTION - INSTALL STRUCTURE AND SYSTEM PROVISIONS FOR ACTIVATION OF CENTER TANK (A330-200) 19 MAR 13 Applicable to: ALL S13455 FLIGHT CONTROLS - GENERAL - ADAPT FLIGHT CONTROLS FOR ST7 21 SEP 15 Applicable to: ALL S13661 AUTO FLIGHT-FLIGHT CONTROL UNIT- ACTIVATE AUTOMATIC ENGAGEMENT OF FLIGHT DIRECTOR WITH CROSS BARS IN GO AROUND 19 MAR 13 Applicable to: ALL S13893 NAVIGATION - MMR - INSTALL COLLINS MULTI-MODE RECEIVERS PROVIDING ILS (FM IMMUNE) AND GPS PRIMARY FUNCTION 19 MAR 13 Applicable to: ALL S13916 OXYGEN - CREW OXYGEN - INSTALL A 115 CU.FT COMPOSITE OXYGEN CYLINDER 19 MAR 13 ICE AND RAIN PROTECTION - WINDSHIELD RAIN PROTECTION - REACTIVATE THE RAIN REPELLENT SYSTEM Applicable to: ALL H14027 Applicable to: ALL H15264 Applicable to: ALL H16147 Applicable to: ALL S10053 Applicable to: ALL S11135 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK (1) M 2/4 PRELIMINARY PAGES LIST OF MODIFICATIONS 18 JAN 17 Continued from the previous page MODIFICATION S14135 Linked SB Incorp. Date Title 19 MAR 13 INDICATING/RECORDING SYSTEMS - EIS - DISPLAY MANAGEMENT COMPUTER - INSTALL NEW DMC SOFTWARE V510X 19 MAR 13 NAVIGATION - GPWS - ACTIVATE ENHANCED GPWS 19 MAR 13 Applicable to: ALL S14327 AUTO FLIGHT - FMGEC - INSTALL FMGEC P1-CD7 FOR RR OR PW ENGINES 19 MAR 13 Applicable to: ALL S14521 INDICATING/RECORDING SYSTEMS-CENTRAL WARNING SYSTEMS-PROVIDE NEW AUTO CALL-OUT CALLED "V1" 19 MAR 13 Applicable to: ALL S14562 NAVIGATION-TCAS-INSTALL ALLIED SIGNAL CHANGE 7 P/N 066-50000-2220 19 MAR 13 Applicable to: ALL S14649 AUTO FLIGHT - FMGEC - INSTALL A NEW STANDARD FMGEC L9CD6 19 MAR 13 Applicable to: ALL S14786 NAVIGATION - MMR - INSTALL COLLINS MULTI-MODE RECEIVERS P/N 822-1152-121 19 MAR 13 Applicable to: ALL S14859 NAVIGATION-STANDBY NAVIGATION SYSTEMS- INSTALL SEXTANT AVIONICS INTEGRATED STANDBY INSTRUMENT SYSTEM (ISIS) 19 MAR 13 Applicable to: ALL S15891 INDICATING/RECORDING SYSTEMS-ELECTRONIC INSTRUMENT SYSTEM - INSTALL NEW DISPLAY SYSTEM (EIS2) EQTS (DMC/DU/DISKETTES) 19 MAR 13 Applicable to: ALL S16107 NAVIGATION - EGPWS - USE LATERAL GPS POSITION WITH AUTOMATIC DESELECTION 19 MAR 13 INFORMATION SYSTEMS - GENERAL - CERTIFY FANS A CONFIGURATIONS 19 MAR 13 NAVIGATION - EGPWS - ACTIVATE OBSTACLE FUNCTION 19 MAR 13 Applicable to: ALL S16286 FLIGHT CONTROLS - ELECTRICAL FLIGHT CONTROL SYSTEM (EFCS) - INSTALL RUDDER FLY-BY WIRE ON A330/A340 19 MAR 13 Applicable to: ALL S16318 INDICATING/RECORDING SYSTEMS - FWC - INSTALL NEW STANDARD K7 19 MAR 13 Applicable to: ALL S16354 ELECTICAL POWER - GENERAL - INSTALL EMERGENCY POWER CENTER 743 VU IN SECT 11/12 19 MAR 13 Applicable to: ALL S16606 INDICATING/RECORDING SYSTEMS - FWC - REPLACE THE EXISTING STANDARD FWC BY A NEW STD K6 FOR A330 FAR 121-344 19 MAR 13 Applicable to: ALL S16646 INDICATING/RECORDING SYSTEMS - EIS - INTALL NEW EIS2 STANDARD L4 ON A330/A340 ENHANCED 19 MAR 13 Applicable to: ALL S16983 NAVIGATION - WEATHER RADAR SYSTEM - INSTALL COLLINS DUAL CONTROL PANEL CAPABLE OF MULTISCAN FUNCTION 19 MAR 13 Applicable to: ALL S16985 INFORMATION SYSTEMS - GENERAL - CERTIFY FANS A+ CONFIGURATIONS (OVERALL MODIFICATION) 19 MAR 13 GENERAL-TECHNICAL INFO ,WEIGHT AND GC - INCREASE MAXIMUM OPERATING ALTITUDE FROM 41100 TO 41450 FEET Applicable to: ALL S14218 Applicable to: ALL S14275 Applicable to: ALL S16262 Applicable to: ALL S16279 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK (1) M 3/4 PRELIMINARY PAGES LIST OF MODIFICATIONS 18 JAN 17 Continued from the previous page MODIFICATION S17494 Linked SB Incorp. Date Title 19 MAR 13 Applicable to: ALL S18094 INDICATING/RECORDING SYSTEM - EIS - INSTALL NEW EIS2 STANDARD L3-1 (DMC, DU AND DISKS) 19 MAR 13 Applicable to: ALL S18144 FLIGHT CONTROL - FLIGHT CONTROL PRIMARY COMPUTER (FCPC) - INTRODUCE TRIM SETTING AUTOMATIC FUNCTION 19 MAR 13 NAVIGATION-ADIRS-INTRODUCE AIR DATA MONITORING FUNCTION 06 JAN 15 AUTO FLIGHT - FMGEC - INSTALL FMGEC P4HJ1 WITH GENEPI HARDWARE AND FMS HONEYWELL RELEASE 1A ON A330 WITH PW/RR 19 MAR 13 AUTO-FLIGHT - MCDU - INSTALL 3 LCD MCDU HONEYWELL 19 MAR 13 Applicable to: ALL S18711 NAVIGATION - SWITCHING AND INDICATING - REMOVE DDRMI INDICATORS 19 MAR 13 Applicable to: ALL S18882 AUTO-FLIGHT - MCDU - INSTALL NEW MCDU LCD HONEYWELL (REBOND STANDARD) 19 MAR 13 Applicable to: ALL S19417 NAVIGATION - DME - RELOCATE DME1 POWER SUPPLY TO PROVIDE POWER IN EMERGENCY FOR A330 19 MAR 13 Applicable to: ALL S19547 INDICATING / RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) - INSTALL FWC STANDARD T2-0. 21 SEP 15 Applicable to: ALL S30154 AUTO FLIGHT-FMGEC-REPLACE FMGEC T3HJ0 HARDWARE GENEPI WITH P3HJ0 ON A330-200F WITH PW/RR ENGINES 19 MAR 13 Applicable to: ALL S30373 FUSELAGE - NOSE FORWARD FUSELAGE ADAPT NLG DOORS FOR A330-200F 19 MAR 13 Applicable to: ALL S30653 NAVIGATION - TCAS - INSTALL TCAS HONEYWELL TPA-100B CHANGE 7.1 CAPABLE OF ATSAW 19 MAR 13 Applicable to: ALL S30672 INDICATING/RECORDING SYSTEMS - DMC - INSTALL ENHANCED DU INSTEAD OF EIS2 LCDU 19 MAR 13 Applicable to: ALL S30806 INDICATING/RECORDING SYSTEMS - FWC - INSTALL FWC STANDARD T3-0 ON LR A/C 21 SEP 15 Applicable to: ALL S30934 AUTO FLIGHT-FLIGHT MANAGEMENT-ACTIVATE "NO PROFILE INVALIDATION AT MDA - 50FT IN FINAL APP" FUNCTION IN FMS RELEASE 1 30 MAY 13 Applicable to: ALL S30958 NAVIGATION - GENERAL - FLIGHT MANUAL EXTENSION TO RNP AR 0.3 CAPABILITY - A330 CONFIGURATION 19 MAR 13 Applicable to: ALL S30973 INDICATING/RECORDING SYSTEMS - FWC - INTRODUCE NEW FWC STANDARD T4 ON LR A/C 30 MAY 13 Applicable to: ALL S31353 INDICATING/RECORDING SYSTEM - EIS - ACTIVATE LAT DEV SCALE DISPLAY FUNCTION 19 MAR 13 INDICATING RECORDING SYSTEMS - FWC - ACTIVATE MONITORING OF ATC/XPDR FAULTS Applicable to: ALL S18160 22-3125 04 Applicable to: ALL S18168 Applicable to: ALL S18222 Applicable to: ALL S32159 31-3200 01 06 JAN 15 Applicable to: ALL S32258 INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) - INTRODUCE NEW FWC STANDARD T5 34-3288 01 06 JAN 15 NAV- W/R SYST - INSTALL COLLINS WXR CAPABLE MULTISCAN WITH TRANSCEIVER WRT-2100 (P/N 822-1710-214) Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK (1) M 4/4 PRELIMINARY PAGES LIST OF MODIFICATIONS 18 JAN 17 Continued from the previous page MODIFICATION 22-3147 01 Applicable to: ALL 31-3232 00 Linked SB Incorp. Date Title 21 SEP 15 AUTO FLIGHT - FMGEC - INSTALL FMGEC P4HJ1A CAPABLE OF NAV MODE KEPT IN GO AROUND ON A330 WITH PW/RR ENGINES 07 JUN 16 INDICATING/RECORDING SYSTEMS - FLIGHT WARNING COMPUTER (FWC) - INTRODUCE FWC STD T7 Applicable to: ALL (1) Evolution code : N=New, R=Revised, E=Effectivity TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK GENERAL TABLE OF CONTENTS GEN 1/2 30 JUN 15 Important.........................................................................................GEN.01A General Information........................................................................GEN.02A TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK GENERAL TABLE OF CONTENTS Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE GEN 2/2 30 JUN 15 A330-243F GENERAL QUICK REFERENCE HANDBOOK GEN.01A 30 JUN 15 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 / 23 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 / 12 MAY 15 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 this height). The flight crew can stop the procedure if the conditions for the application of the QRH procedure disappear. Ident.: GEN-A-00010468.0001001 / 23 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE GENERAL A330-243F QUICK REFERENCE HANDBOOK GEN.02A 30 JUN 15 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 / 16 MAR 15 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS ABN 1/4 06 MAR 17 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 Fire Protection ABN-26 SMOKE/FUMES/AVNCS/MD 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................................................................ 27.02A Sidestick / Rudder Pedals Stiff.......................................................... 27.03A Rudder Jam/Rudder Pedal Jam.........................................................27.04A Rudder Trim Runaway....................................................................... 27.05A Fuel ABN-28 FUEL IMBALANCE............................................................................ 28.01A FUEL LEAK........................................................................................28.02A FUEL LOSS REDUCTION................................................................. 28.03A 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 Indicating / Recording Systems ABN-31 Display Unit Failure............................................................................31.01A ECAM Single Display.........................................................................31.02A EIS DISPLAY DISCREPANCY.......................................................... 31.03A TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS ABN 2/4 06 MAR 17 Continued from the previous page 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 NAV FM / GPS POS DISAGREE...................................................... 34.05A IR Alignment in ATT Mode................................................................ 34.06A EGPWS Warnings............................................................................ 34.07A EGPWS Cautions...............................................................................34.08A TCAS Warnings................................................................................ 34.09A Pneumatic ABN-36 AIR ENG 1+2 BLEED RESET (APU BLEED AVAILABLE)................36.02A AIR ENG 1+2 BLEED RESET (APU BLEED NOT AVAILABLE)....... 36.03A Engines ABN-70 ALL ENGINES FAILURE.................................................................. 70.01A ENG RELIGHT (IN FLIGHT)..............................................................70.06A ENG 1(2) STALL................................................................................70.07A ENG Tailpipe Fire.............................................................................. 70.08A HIGH ENGINE VIBRATION............................................................... 70.09A Suspected ENG Fuel Sys Contamination .........................................70.10A ENG Fuel Sys Contamination............................................................ 70.10A 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 Overspeed Recovery..........................................................................80.06A Overweight Landing........................................................................... 80.07A Stall Recovery.................................................................................. 80.08A Stall Warning at Liftoff.................................................................... 80.08A Tailstrike............................................................................................. 80.09A TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS ABN 3/4 06 MAR 17 Continued from the previous page 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 Emer Landing ALL ENG FAILURE........................................................ C2 Emergency Evacuation...........................................................................C2 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES TABLE OF CONTENTS Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABN 4/4 06 MAR 17 ABNORMAL AND EMERGENCY PROCEDURES SUMMARY OF HIGHLIGHTS A330-243F QUICK REFERENCE HANDBOOK Localization Title ABN-80 Emer Landing ALL ENG FAILURE Page ID 80.C2 1 ABN 1/2 06 MAR 17 Reason Documentation update: Addition of "Emer Landing ALL ENG FAILURE" documentary unit TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES SUMMARY OF HIGHLIGHTS Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABN 2/2 06 MAR 17 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 22.01A 30 JUN 15 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 22.02A 30 JUN 15 MCDU 1(2)(3) FAILURE Ident.: ABN-22-00010479.0002001 / 08 FEB 13 Applicable to: ALL 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK 24.01A ABNORMAL AND EMERGENCY PROCEDURES 30 JUN 15 ELEC EMER CONFIG SYS-REMAINING 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 Applicable to: ALL 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 Ident.: ABN-24-SYN-00010488.0001001 / 17 NOV 14 Applicable to: ALL FCU Ident.: ABN-24-SYN-00010489.0001001 / 17 NOV 14 Applicable to: ALL COM Ident.: ABN-24-SYN-00010491.0002001 / 17 NOV 14 Applicable to: ALL CARGO SMOKE DET FIRE 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 - - - Norm APU AUTO EXT. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01B ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 30 JUN 15 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) 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 Norm Norm Norm Norm 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 Norm Norm Norm Norm AFT APU PUMP Norm (a) Norm (a) Norm (a) Norm (a) APU LP VALVE Norm Norm Norm Norm 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 Norm inop inop inop STBY AOA/PITOT Norm (f) inop inop inop RAIN REPEL  Capt Capt Capt Capt Ident.: ABN-24-SYN-00010492.0004001 / 17 MAR 15 Applicable to: ALL FLT CTL RUDD TRAVEL Ident.: ABN-24-SYN-00010493.0002001 / 17 NOV 14 Applicable to: ALL FUEL XFR , ISOL VALVES Ident.: ABN-24-SYN-00010494.0001001 / 17 NOV 14 Applicable to: ALL HYD Ident.: ABN-24-SYN-00010495.0001001 / 17 NOV 14 Applicable to: ALL ICE & RAIN WHC 1 CAPT AOA TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01C ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 30 JUN 15 Continued from the previous page BAT ONLY SUPPLIED BY ENG HYD PUMPS SUPPLIED BY RAT ONLY IN FLT ON GND (IAS < 50 kt) 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 SDAC 1, FWC 1, 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 IR 1 and 3 Norm Norm Norm Norm 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 ATC 1 only inop inop inop RADAR 1 only inop inop inop ISIS Norm Norm Norm Norm Ident.: ABN-24-SYN-00010496.0001001 / 17 NOV 14 Applicable to: ALL EIS Ident.: ABN-24-SYN-00010497.0001001 / 08 DEC 14 Applicable to: ALL LGCIU L/G AUTO BRK/ANTI SKID PARK BRK Ident.: ABN-24-SYN-00010498.0001001 / 17 NOV 14 Applicable to: ALL LIGHTS L LDG LT Ident.: ABN-24-SYN-00010499.0026001 / 17 NOV 14 Applicable to: ALL NAV Ident.: ABN-24-SYN-00010500.0001001 / 17 NOV 14 Applicable to: ALL OXYGEN Crew OXY valve CTL Norm inop inop inop PAX OXY Norm Norm Norm Norm BMC 2 inop BMC 2 inop BMC 2 inop BMC 2 inop man only man only man only man only Ident.: ABN-24-SYN-00010501.0001001 / 17 NOV 14 Applicable to: ALL PNEU ENG BLEED X BLEED TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ELEC EMER CONFIG SYS REMAINING 24.01D ABNORMAL AND EMERGENCY PROCEDURES EMER GEN RUNNING 30 JUN 15 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 Norm Norm Norm Norm FADEC's A+B A+B A+B A+B IGNITION Ident.: ABN-24-SYN-00010502.0001001 / 17 NOV 14 Applicable to: ALL APU Ident.: ABN-24-SYN-00010503.0001001 / 17 NOV 14 Applicable to: ALL DOORS SLIDES ARM WARN Ident.: ABN-24-SYN-00010504.0003001 / 17 NOV 14 Applicable to: ALL PWR PLT A only A only A only A only 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 VOR 1 or ADF 1 (as selected on the FCU) is available at a time. (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). TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 24.02A 30 JUN 15 ELEC EMER CONFIG SUMMARY Ident.: ABN-24-SUM-00010480.0015001 / 09 APR 15 Applicable to: ALL 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: ILS 1, GLS1  , DME 1, VOR 1, GPS1 only COM: HF 1, VHF 1, ATC 1, RMP1 only For Landing Performance assessment, Refer to QRH PER-C, or use the LDG PERF application of FlySmart with Airbus. Ident.: ABN-24-SUM-00010483.0006001 / 17 NOV 14 Applicable to: ALL 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 Applicable to: ALL 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 Applicable to: ALL GO-AROUND NO GEAR RETRACTION FUEL: Increased fuel consumption (Refer to QRH PER-B) TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 30 JUN 15 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01A 06 DEC 16 SMOKE/FUMES/AVNCS/MD SMOKE Ident.: ABN-26-A-00010507.0004001 / 20 SEP 13 Applicable to: ALL LAND ASAP APPLY IMMEDIATELY  IF REQUIRED: CREW OXY MASKS................... USE/100%/EMERG CAB FANS................................................................OFF GALLEY & LAV FAN................................................ OFF GALLEY.................................................................... OFF CKPT/CAB COM.......................................... ESTABLISH CAB TO CRG DOORS........................................ CLOSE SIGNS.........................................................................ON  IF SMOKE SOURCE IMMEDIATELY OBVIOUS, ACCESSIBLE AND EXTINGUISHABLE: FAULTY EQPT.............................................ISOLATE  IF SMOKE SOURCE NOT IMMEDIATELY ISOLATED: DIVERSION.................................................. INITIATE DESCENT.....................................................INITIATE Descent to FL 200, 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01B 06 DEC 16 SMOKE/FUMES/AVNCS/MD SMOKE (Cont'd)  At ANY TIME of the procedure, if situation becomes UNMANAGEABLE: IMMEDIATE LANDING............................CONSIDER Ident.: ABN-26-A-00013661.0003001 / 27 NOV 12 Applicable to: ALL  IF SMOKE MD SMOKE ECAM ALERT, COMPLETE ECAM ACTIONS, THEN: CREW OXY MASKS................................. USE/100% CAB OXY MASKS........................................MAN ON VENT EXTRACT................................. CHECK AUTO MD ISOL VALVES............................................... OFF ALL LOWER CRG ISOL VALVES....................... OFF CAB................................................................ NOTIFY EMER EXIT LT...................................................... ON COMMERCIAL..................................................... OFF CAB PR MODE SEL...........................................MAN MAN VALVE SEL............................................... FWD MAN V/S CTL.....................................+ 4 000 FT/MN MAN ALT TGT........................................... 20 000 FT ATC................................................................ NOTIFY RECOMMENDED CRUISE ALT......................FL 200  When A/C and CAB ALT at 20 000 ft: MAN V/S CTL..........................................FULL UP CREW OXY MASKS........................NORMAL MODE OXY PRESS...............................................MONITOR TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01C 06 DEC 16 SMOKE/FUMES/AVNCS/MD SMOKE (Cont'd) MINIMUM OXY PRESS FOR 2 CREW AT FL 200 (NORMAL MODE) Remaining Flight Time 30 60 90 120 150 180 210 to Landing (min) MIN OXY PRESS 165 240 315 390 465 540 610 (PSI)  If remaining OXY PRESS close to minimum: DESCENT (FL 140/MEA, min obstacle clearance altitude)................................................ CONSIDER  At or below FL 140: CAB SUPPLY..............................CONSIDER OFF 3RD AND 4TH CREW OXY MASKS..................... .......................................... CONSIDER STOWING REMOVAL OF SMOKE/FUMES.............. CONSIDER Ident.: ABN-26-A-00010510.0016001 / 27 NOV 12 Applicable to: ALL  If AIR COND SMOKE SUSPECTED: APU BLEED.........................................................OFF VENT EXTRACT................................. CHECK AUTO MD ISOL VALVES............................................... OFF ALL LOWER CRG ISOL VALVES....................... OFF PACK 1................................................................ OFF  If smoke continues: PACK 1............................................................. ON PACK 2........................................................... OFF TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01D 06 DEC 16 SMOKE/FUMES/AVNCS/MD SMOKE (Cont'd)  If smoke still continues: PACK 2........................................................ ON PACK 1.......................................................OFF REMOVAL OF SMOKE/FUMES.............. CONSIDER  IF CAB EQUIPMENT SMOKE SUSPECTED:  If smoke continues : VENT EXTRACT..........................................OVRD EMER EXIT LT................................................. ON COMMERCIAL................................................ OFF SMOKE DISSIPATION.............................. CHECK  If smoke still continues : VENT EXTRACT..................................... AUTO REMOVAL OF SMOKE/FUMES.............. CONSIDER Ident.: ABN-26-A-00010511.0005001 / 27 NOV 12 Applicable to: ALL  IF SMOKE SOURCE CANNOT BE DETERMINED AND STILL CONTINUES OR AVNCS/ELECTRICAL SMOKE SUSPECTED: VENT EXTRACT...............................................OVRD  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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01E 06 DEC 16 SMOKE/FUMES/AVNCS/MD SMOKE (Cont'd)  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 EMER ELEC CONFIG..............................CONSIDER Ident.: ABN-26-A-00010512.0012001 / 21 MAR 11 Applicable to: ALL 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.01F 06 DEC 16 SMOKE/FUMES/AVNCS/MD 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.02A 06 DEC 16 REMOVAL OF SMOKE/FUMES Ident.: ABN-26-00010506.0005001 / 23 DEC 14 Applicable to: ALL CREW OXY MASKS...................................... USE/100% EMER EXIT LIGHT.................................................... ON CAB.....................................................................NOTIFY CAB OXY MASKS.............................................MAN ON CAB PR MODE SEL................................................MAN MAN VALVE SEL.................................................... FWD MAN V/S CTL..........................................+ 4 000 FT/MN CAB ALT TGT.................................................20 000 FT DESCENT (FL 200, or MEA -MORA, or minimum obstacle clearance altitude)...............................INITIATE ATC..................................................................... NOTIFY SMOKE/FUMES/AVNCS/MD SMOKE PROC................. .......................................................................CONTINUE While descending, continue applying the appropriate steps of the SMOKE/FUMES/AVNCS /MD SMOKE paper procedure depending on the suspected smoke source.  At FL 200 or MEA-MORA: PACK 1................................................................ OFF PACK 2.................................................... CHECK ON MAN V/S CTL.............................................. FULL UP  If smoke persists, cockpit window opening: MAX SPEED................................................... 230 KT COCKPIT DOOR.............................................. OPEN HEADSET.............................................................. ON PM COCKPIT WINDOW...................................OPEN  When window is open: VISUAL WARNINGS (noisy CKPT)........... MONITOR TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.02B 06 DEC 16 REMOVAL OF SMOKE/FUMES (Cont'd) SMOKE/FUMES/ AVNCS/MD SMOKE PROC........... ..................................................................CONTINUE OXY PRESS................................................... MONITOR  If low OXY PRESS: DESCENT (FL 100, or MEA -MORA).......CONSIDER CAB SUPPLY.................................. CONSIDER OFF 3RD AND 4TH CREW OXY MASKS.......................... ............................................... CONSIDER STOWING TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 26.03A 06 DEC 16 SMOKE/FIRE FROM LITHIUM BATTERY Ident.: ABN-26-00015935.0003001 / 18 JUN 15 Applicable to: ALL If necessary, transfer control to the flight crew member seated on the opposite side of the fire  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: CKPT/CAB COM.............................................................................ESTABLISH DEVICE..............................................................TRANSFER TO CABIN AREA RECEPTACLE.................. FILL WITH WATER OR NON-ALCOHOLIC LIQUID DEVICE..............................................................................................IMMERSE RECEPTACLE...................................................... STORE IN THE LAVATORY RECEPTACLE................................................................................... MONITOR  AT ANY TIME of the procedure, if SMOKE becomes the GREATEST THREAT: REMOVAL OF SMOKE/FUMES procedure........................................ CONSIDER  AT ANY TIME of the procedure, if situation becomes UNMANAGEABLE: IMMEDIATE LANDING........................................................................CONSIDER TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 06 DEC 16 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.01A 06 DEC 16 LANDING WITH SLATS OR FLAPS JAMMED Ident.: ABN-27-00010513.0001001 / 09 APR 15 Applicable to: ALL LANDING CONF......................................................................................DETERMINE Refer to QRH PER-27A Landing Distance with Slats and Flaps System Failure, or use the LDG PERF application of FlySmart with Airbus.  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 CONF 1, 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 27.01B ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 06 DEC 16 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.02A 06 DEC 16 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 CONF 1, 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.03A 06 DEC 16 SIDESTICK / RUDDER PEDALS STIFF Ident.: ABN-27-00010515.0001001 / 23 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 27.04A 06 DEC 16 RUDDER JAM/RUDDER PEDAL JAM Ident.: ABN-27-00010516.0004001 / 03 JUN 14 Applicable to: ALL 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 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 27.05A 06 DEC 16 RUDDER TRIM RUNAWAY Ident.: ABN-27-00010517.0002001 / 08 FEB 13 Applicable to: ALL 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 28.01A 18 JAN 17 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 28.02A 18 JAN 17 FUEL LEAK Ident.: ABN-28-00010522.0010001 / 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 fuel spray is observed 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). 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 Trim tank, or the APU/Trim feeding line (Case 2). WING X FEED.....................................................................MAINTAIN CLOSED Crossfeed valve must remain closed to prevent the leak from affecting both sides. 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. 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.  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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 28.02B 18 JAN 17 FUEL LEAK (Cont'd) 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 Trim tank or the APU/Trim feeding line may be suspected. APU (if ON).............................................................................................. OFF T TANK FEED...................................................................... MAINTAIN ISOL This prevents additional fuel loss through the APU/Trim feeding line. FOR LANDING CAUTION Do not use reversers. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 28.03A 18 JAN 17 FUEL LOSS REDUCTION Ident.: ABN-28-00010523.0005001 / 21 MAR 11 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 a leak from the wing : ‐ A manual Trim tank transfer can be done, to symmetrically transfer fuel to both inner tanks, and avoid an automatic fuel transfer to only the least full inner tank.  If Trim Tank not empty: T TANK FEED............................................................................................... AUTO T TANK MODE................................................................................................FWD  When Trim Tank empty: T TANK MODE.........................................................................................AUTO T TANK FEED............................................................................................ISOL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 28.04A 18 JAN 17 ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 28.05A 18 JAN 17 GRVTY FUEL FEEDING Ident.: ABN-28-00010525.0006001 / 08 FEB 13 Applicable to: ALL 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) Flight time from takeoff less than 30 min (Fuel non-deaerated) 20 000 ft 15 000 ft 7 000 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 28.06A 18 JAN 17 TRIM TANK FUEL UNUSABLE Ident.: ABN-28-00010526.0001001 / 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 MAXIMUM FLIGHT TIME........................................................................4 HOURS After 4 h, depending on the fuel distribution, the aft CG limit may be reached. FOR LANDING  If CG > 39 %: 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 18 JAN 17 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.01A 18 JAN 17 HYD B+Y SYS LO PR SUMMARY Ident.: ABN-29-SUM1-00010527.0001001 / 09 APR 15 Applicable to: ALL 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, or use the LDG PERF application of FlySmart with Airbus. Ident.: ABN-29-SUM1-00010531.0001001 / 08 FEB 13 Applicable to: ALL 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 Applicable to: ALL 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 Applicable to: ALL GO-AROUND NO GEAR RETRACTION FUEL: Increased fuel consumption (Refer to QRH PER-B) TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.02A 18 JAN 17 HYD G+B SYS LO PR SUMMARY Ident.: ABN-29-SUM2-00010528.0001001 / 09 APR 15 Applicable to: ALL 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, or use the LDG PERF application of FlySmart with Airbus. Ident.: ABN-29-SUM2-00010537.0001001 / 08 FEB 13 Applicable to: ALL 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 Applicable to: ALL 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 Applicable to: ALL GO-AROUND NO GEAR RETRACTION  For circuit: MAINTAIN SLATS/FLAPS CONFIGURATION Recommended speed: MAX SPD - 10 kt / 200 kt  For diversion: SELECT CLEAN CONFIGURATION TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES GO-AROUND  If Slats jammed at zero: Normal operating speeds (MAX SPD 200 kt)  If Slats jammed above zero: Recommended speed: 200 kt FUEL: Increased fuel consumption (Refer to QRH PER-B) TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 29.02B 18 JAN 17 Continued from the previous page A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 29.03A 18 JAN 17 HYD G+Y SYS LO PR SUMMARY Ident.: ABN-29-SUM3-00010529.0001001 / 09 APR 15 Applicable to: ALL 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, or use the LDG PERF application of FlySmart with Airbus. Ident.: ABN-29-SUM3-00010543.0004001 / 04 AUG 15 Applicable to: ALL APPROACH CAT 2 INOP SLATS SLOW / FLAPS JAMMED GPWS FLAP MODE (If Flaps < 3 or 3 < Flaps < FULL)......................................................................... 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 Applicable to: ALL 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 Applicable to: ALL 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES GO-AROUND Normal operating speeds (MAX SPD= 200 kt)  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) TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 29.03B 18 JAN 17 Continued from the previous page A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 18 JAN 17 ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 30.01A 06 DEC 16 DOUBLE AOA HEAT FAILURE Ident.: ABN-30-00010548.0002001 / 21 OCT 16 Applicable to: ALL In the case of double failure of alpha probe heaters, the choice made by the computers among the 3 ADR values may be erroneous. One of affected ADRs........................................................................................... OFF NAV ADR 1(2)(3) FAULT In the case of disagreement between the two remaining ADR s, the NAV ADR DISAGREE ECAM caution will trigger. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 06 DEC 16 ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 31.01A 19 MAR 13 DISPLAY UNIT FAILURE Ident.: TDU / ABN-31-00014692.0002001 / 12 MAR 13 Applicable to: ALL  DU is blank (with or without a large letter "F" in amber), or the display is distorted, or DU brightness reduces to the minimum: DU (affected) brightness knob ..........................................................OFF then ON The display will recover after 10 s.  If unsuccessful: 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  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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 31.01B 19 MAR 13 DISPLAY UNIT FAILURE (Cont'd)  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 E/WD and SD: ECAM UPPER DISPLAY................................................................OFF THEN ON The action on the ECAM DMC SWITCHING selector produces the same effect. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 31.02A 19 MAR 13 ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 31.03A 19 MAR 13 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 32.01A 18 JAN 17 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 32.02A 18 JAN 17 ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 32.03A 18 JAN 17 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 32.04A 18 JAN 17 LANDING WITH ABNORMAL L/G Ident.: ABN-32-00010556.0008001 / 22 APR 16 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 OCCUPANTS................................................................................... NOTIFY ATC............................................................................................................... NOTIFY Consider fuel reduction to a safe minimum.  If one MAIN L/G abnormal: FUEL IMBALANCE............................................................................CONSIDER Open all fuel XFEED 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 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. 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 32.04B 18 JAN 17 LANDING WITH ABNORMAL L/G (Cont'd) 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 PARK BRK........................................................................................................... ON 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 ALL BATs...................................................................................................... OFF  If Evacuation not required: CABIN OCCUPANTS (PA)......................................................................NOTIFY Ensure that all the landing gears are secured before initiating the disembarkation of the aircraft (before switching OFF the SEAT BELTS signs). TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 18 JAN 17 ABNORMAL AND EMERGENCY PROCEDURES A330-243F 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 34.01A 06 DEC 16 A330-243F QUICK REFERENCE HANDBOOK 34.02A ABNORMAL AND EMERGENCY PROCEDURES 06 DEC 16 ADR CHECK PROC Ident.: ABN-34-00015215.0001001 / 30 NOV 15 Applicable to: ALL Apply the UNRELIABLE SPEED INDICATION procedure. UNRELIABLE SPEED INDICATION Ident.: ABN-34-D-00017854.0001001 / 30 NOV 15 Applicable to: ALL  If the safe conduct of the flight is impacted: 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 Ident.: ABN-34-D-00017855.0001001 / 30 NOV 15 Applicable to: ALL  To level off: AP/FD............................................................................................................... OFF A/THR............................................................................................................... OFF SPEEDBRAKES...................................................................CHECK RETRACTED PITCH/THRUST TABLE...............................................................................APPLY Ident.: ABN-34-D-00017858.0008001 / 30 NOV 15 Applicable to: ALL PITCH / THRUST FOR LEVEL OFF 240 t 200 t 160 t 120 t 530 000 lb 440 000 lb 350 000 lb 260 000 lb SLATS / FLAPS EXTENDED CONF PITCH THRUST % N1 (Resultant speed) 3 7.5° 64% (170 kt) 60% (155 kt) 54% (135 kt) 50% (120 kt) 2 7.5° 62% (180 kt) 58% (165 kt) 54% (145 kt) 48% (125 kt) 1+F 6.5° 62% (205 kt) 58% (190 kt) 52% (170 kt) 46% (145 kt) 1 9.5° 60% (200 kt) 56% (185 kt) 52% (165 kt) 46% (140 kt) PITCH FL 4° at or below FL250 100 62% (285 kt) 58% (255 kt) 52% (225 kt) 48% (195 kt) 200 68% (280 kt) 64% (255 kt) 58% (225 kt) 52% (195 kt) CLEAN THRUST % N1 (Resultant speed) TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK 34.02B ABNORMAL AND EMERGENCY PROCEDURES 06 DEC 16 UNRELIABLE SPEED INDICATION (Cont'd) PITCH / THRUST FOR LEVEL OFF 240 t 3° above FL250 200 t 160 t 120 t 530 000 lb 440 000 lb 350 000 lb 260 000 lb 300 76% (295 kt) 72% (275 kt) 68% (245 kt) 62% (215 kt) 350 / 76% (270 kt) 70% (245 kt) 64% (210 kt) 400 / / 76% (235 kt) 70% (210 kt) FLYING TECHNIQUE TO STABILIZE SPEED Stabilize the altitude. When altitude is stabilized: ‐ If the pitch is above the target pitch, increase the thrust and maintain the altitude. ‐ If the pitch is below the target pitch, decrease the thrust and maintain the altitude. When the pitch reaches the target pitch, adjust the thrust to keep this target pitch. Ident.: ABN-34-D-00017882.0001001 / 30 NOV 15 Applicable to: ALL  When flight path is stabilized: AP/FD............................................................................................................... OFF A/THR............................................................................................................... OFF SPEEDBRAKES...................................................................CHECK RETRACTED FLIGHT PATH.......................................................................... KEEP STABILIZED Respect Stall Warning and disregard “RISK OF UNDUE STALL WARNING” STATUS message if displayed on ECAM. Ident.: ABN-34-D-00017911.0002001 / 28 SEP 16 Applicable to: ALL AFFECTED ADR IDENTIFICATION PROBE/WINDOW HEAT......................................................................................ON ALL SPEED INDICATIONS.......................................................................X CHECK ADR3 and STBY speeds use the data of the same probe.  If at least one ADR is confirmed reliable: RELIABLE AIR DATA................................................................................... USE UNRELIABLE ADR P/B(s)............................................................................ OFF  If affected ADR(s) cannot be identified or all ADRs are affected:  When above FL 250: ONE ADR........................................................................................KEEP ON TWO ADR P/B(s)..................................................................................... OFF This prevents the flight control laws from using two coherent but unreliable ADR data. For flight continuation, Refer to Pitch/Thrust Tables.  When below FL 250, if speed still unreliable: ALL ADR P/B(s)....................................................................................... OFF SPD.................................................................................... FLY THE GREEN NAV ADR 1+2+3 FAULT Procedure................................................... APPLY TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 34.02C ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 06 DEC 16 UNRELIABLE SPEED INDICATION (Cont'd) Ident.: ABN-34-D-00017888.0008001 / 30 NOV 15 Applicable to: ALL CLIMB CLIMB IN CLEAN CONFIGURATION THRUST 240 t 200 t 160 t 120 t 530 000 lb 440 000 lb 350 000 lb 260 000 lb FL CLB PITCH (Resultant speed) 50 9° (280 kt) 10° (255 kt) 13° (220 kt) 17° (185 kt) 100 8° (280 kt) 9° (255 kt) 12° (220 kt) 16° (185 kt) 200 6° (280 kt) 7° (255 kt) 9° (225 kt) 12° (190 kt) 300 5° (275 kt) 5° (250 kt) 6° (225 kt) 8° (190 kt) 400 / / 5° (220 kt) 6° (190 kt) CRUISE FLYING TECHNIQUE TO STABILIZE SPEED Stabilize the altitude. When altitude is stabilized: ‐ If the pitch is above the target pitch, increase the thrust and maintain the altitude. ‐ If the pitch is below the target pitch, decrease the thrust and maintain the altitude. When the pitch reaches the target pitch, adjust the thrust to keep this target pitch. LEVEL FLIGHT IN CLEAN CONFIGURATION 240 t 200 t 160 t 120 t 530 000 lb 440 000 lb 350 000 lb 260 000 lb PITCH FL 4° at or below FL250 100 62% (285 kt) 58% (255 kt) 52% (225 kt) 48% (195 kt) 200 68% (280 kt) 64% (255 kt) 58% (225 kt) 52% (195 kt) 300 76% (295 kt) 72% (275 kt) 68% (245 kt) 62% (215 kt) 350 / 76% (270 kt) 70% (245 kt) 64% (210 kt) 400 / / 76% (235 kt) 70% (210 kt) 3° above FL250 Note: THRUST % N1 (Resultant speed) If the failure is due to radome destruction, the drag will increase and therefore N1 must be increased by 3% in cruise and 1.5% in approach. Fuel flow will increase by about 10%. DESCENT DESCENT IN CLEAN CONFIGURATION THRUST PITCH IDLE 2° 240 t 200 t 530 000 lb 440 000 lb 160 t 120 t 350 000 lb 260 000 lb Resultant speed 275 kt 250 kt INITIAL / INTERMEDIATE APPROACH Apply the FLYING TECHNIQUE TO STABILIZE SPEED TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 225 kt 195 kt 34.02D ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 06 DEC 16 UNRELIABLE SPEED INDICATION (Cont'd) LEVEL FLIGHT WITH LANDING GEAR UP 240 t 200 t 160 t 120 t 530 000 lb 440 000 lb 350 000 lb 260 000 lb WITH LANDING GEAR UP CONF PITCH THRUST % N1 (Resultant speed) 0 5° 58% (250 kt) 54% (225 kt) 50% (200 kt) 46% (180 kt) 1 9.5° 60% (200 kt) 56% (185 kt) 52% (165 kt) 46% (140 kt) 1+F 6.5° 62% (205 kt) 58% (190 kt) 52% (170 kt) 46% (145 kt) 2 7.5° 62% (180 kt) 58% (165 kt) 54% (145 kt) 48% (125 kt) 58% (140 kt) 52% (120 kt) 160 t 120 t 350 000 lb 260 000 lb WITH LANDING GEAR DOWN 3 7.5° 68% (170 kt) 64% (155 kt) FINAL APPROACH AT -3° DESCENT FLIGHT PATH APPROACH IN CONF 3 AND L/G EXTENDED CONF PITCH 3 4° 240 t 200 t 530 000 lb 440 000 lb THRUST (% N1) 50% 48% TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 42% 38% A330-243F QUICK REFERENCE HANDBOOK 34.03A ABNORMAL AND EMERGENCY PROCEDURES 06 DEC 16 ALL ADR OFF Ident.: ABN-34-B-00019415.0032001 / 17 MAR 16 Applicable to: ALL 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. 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 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  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 / 17 MAR 16 Applicable to: ALL STATUS INOP SYS The list of Inoperative Systems is displayed on the ECAM. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.03B 06 DEC 16 ALL ADR OFF (Cont'd) Other INOP SYS RAT automatic extension NWS FLAP AUTO RETRACT FLAP LOAD RELIEF ALPHA LOCK L/G RETRACT TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 34.04A 06 DEC 16 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.05A 06 DEC 16 NAV FM / GPS POS DISAGREE Ident.: ABN-34-00010562.0001001 / 08 FEB 13 Applicable to: ALL 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 34.06A 06 DEC 16 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.07A 06 DEC 16 EGPWS WARNINGS Ident.: ABN-34-00017173.0004001 / 17 MAR 16 Applicable to: ALL  "PULL UP" - "TERRAIN AHEAD PULL UP" - "OBSTACLE AHEAD PULL UP" Simultaneously: L2 L1 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.08A 06 DEC 16 EGPWS CAUTIONS Ident.: ABN-34-00019414.0004001 / 17 MAR 16 Applicable to: ALL  "TERRAIN TERRAIN" - "TOO LOW TERRAIN" - "TERRAIN AHEAD" "OBSTACLE AHEAD"  During night or IMC: Simultaneously: AP............................................................................................................... OFF PITCH.................................................................................................PULL UP L2 Pull to full backstick and maintain in that position. THRUST LEVERS...................................................................................TOGA SPEED BRAKE lever.....................................................CHECK RETRACTED BANK.....................................................................WINGS LEVEL or ADJUST L1 Note:  L2 L1 L2 "SINK RATE"  Above 1 000 ft AAL in IMC or above 500 ft AAL in VMC: FLIGHT PATH..................................................................................... ADJUST   L2 L2 For some airports, the operator may define a specific procedure. Adjust pitch and thrust to silence the alert. L1 L1 During daylight and VMC with terrain and obstacles clearly in sight: FLIGHT PATH..................................................................................... ADJUST Adjust pitch, bank and thrust to silence the alert. Note:  For some airports, the operator may define a specific procedure. Below 1 000 ft AAL in IMC or below 500 ft AAL in VMC: GO-AROUND..................................................................................CONSIDER "DON'T SINK" FLIGHT PATH.......................................................................................... ADJUST Adjust pitch and thrust to silence the alert.  "TOO LOW GEAR" - "TOO LOW FLAPS" GO-AROUND........................................................................................PERFORM  "GLIDE SLOPE"  Above 1 000 ft AAL in IMC or above 500 ft AAL in VMC: FLIGHT PATH..................................................................................... ADJUST Adjust pitch and thrust to reduce the vertical deviation from the glideslope. L1   When conditions require a deliberate approach below glideslope: G/S MODE............................................................................................ OFF Below 1 000 ft AAL in IMC or below 500 ft AAL in VMC: GO-AROUND..................................................................................CONSIDER TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 34.09A 06 DEC 16 TCAS WARNINGS Ident.: ABN-34-00010565.0048001 / 07 JUN 16 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 ″LEVEL OFF, LEVEL OFF″ or ″MONITOR VERTICAL SPEED″ type messages: AP (if engaged)................................................................................................ OFF BOTH FDs........................................................................................................ OFF Respond promptly and smoothly to a 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 a 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 06 DEC 16 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 36.01A 18 JAN 17 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 36.02A 18 JAN 17 AIR ENG 1+2 BLEED RESET (APU BLEED AVAILABLE) Ident.: ABN-36-00014556.0002001 / 04 AUG 15 Applicable to: ALL Apply this procedure when both engine bleed supply systems are failed and after the completion of the AIR ENG 1+2 BLEED FAULT ECAM procedure and when the APU Bleed supplies the aircraft. CABIN PRESSURE MONITOR MAX FL 220 AVOID ICING CONDITIONS  If no message associated with AIR ENG 1+2 BLEED FAULT and If no ENG BLEED lost due to ENG FIRE or Start Air Valve failed open: PACK 1............................................................................................................... On PACK 2............................................................................................................... On ENG 1 BLEED....................................................................................................ON ENG 2 BLEED....................................................................................................ON APU BLEED..................................................................................................... OFF  If no ENG BLEED recovered: APU BLEED.................................................................................................. ON  If PACK 1 available: PACK 2.................................................................................................. OFF ENG 1 BLEED.............................................................................................OFF ENG 2 BLEED.............................................................................................OFF  If RIGHT LEAK message associated with AIR ENG 1+2 BLEED FAULT or If ENG 2 BLEED lost due to ENG 2 FIRE or Start Air Valve 2 failed open: PACK 1............................................................................................................... On ENG 1 BLEED....................................................................................................ON APU BLEED..................................................................................................... OFF  If no ENG BLEED recovered: APU BLEED.................................................................................................. ON ENG 1 BLEED.............................................................................................OFF TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 36.03A 18 JAN 17 AIR ENG 1+2 BLEED RESET (APU BLEED NOT AVAILABLE) Ident.: ABN-36-00014557.0001001 / 04 AUG 15 Applicable to: ALL Apply this procedure when both engine bleed supply systems are failed and after the completion of the AIR ENG 1+2 BLEED FAULT ECAM procedure and if no APU Bleed is available to supply the aircraft. MAX FL 100/MEA-MORA AVOID ICING CONDITIONS  If no message associated with AIR ENG 1+2 BLEED FAULT and If no ENG BLEED lost due to ENG FIRE or Start Air Valve failed open or APU leak fed by engine: PACK 1............................................................................................................... On PACK 2............................................................................................................... On ENG 1 BLEED....................................................................................................ON ENG 2 BLEED....................................................................................................ON  If no ENG BLEED recovered: ENG 1 BLEED.............................................................................................OFF ENG 2 BLEED.............................................................................................OFF  If only LEFT LEAK message associated with AIR ENG 1+2 BLEED FAULT or If ENG 1 BLEED lost due to ENG 1 FIRE or Start Air Valve 1 failed open or APU leak fed by engine: PACK 2............................................................................................................... On ENG 2 BLEED....................................................................................................ON  If no ENG BLEED recovered: ENG 2 BLEED.............................................................................................OFF  If only RIGHT LEAK message associated with AIR ENG 1+2 BLEED FAULT or If only ENG 2 BLEED lost due to ENG 2 FIRE or Start Air Valve 2 failed open: PACK 1............................................................................................................... On ENG 1 BLEED....................................................................................................ON  If no ENG BLEED recovered: ENG 1 BLEED.............................................................................................OFF  If both LEFT LEAK and RIGHT LEAK messages associated with AIR ENG 1+2 BLEED FAULT or If both ENG BLEEDs lost due to ENG FIRE or Start Air Valve failed open or APU leak fed by engine: No ENG BLEED can be recovered. Consider unsuccessful. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 36.03B 18 JAN 17 AIR ENG 1+2 BLEED RESET (APU BLEED NOT AVAILABLE) (Cont'd)  If unsuccessful (no ENG BLEED recovered):  When DIFF PR < 1 PSI RAM AIR....................................................................................................... ON  If severe ice accretion: MIN SPD.................................................................................VLS+10 / G DOT MANEUVER WITH CARE  If severe ice accretion during approach: APPR SPD.......................................................................................VLS+10 KT LDG DIST PROC....................................................................................APPLY TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 70.01A ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 18 JAN 17 ALL ENGINES FAILURE Ident.: ABN-70-01-00015499.0003001 / 04 AUG 15 Applicable to: ALL First apply the following actions of the ENG ALL ENGINES FAILURE ECAM procedure (if not already applied): LAND ASAP RAT................................................................................................................ MAN ON EMER ELEC PWR.........................................................................................MAN ON OPTIMUM RELIGHT SPEED......................................................................... 300/0.82 Ident.: ABN-70-01-00016584.0012001 / 04 AUG 15 Applicable to: ALL In the case of a speed indication failure due to volcanic ash, the pitch attitude for the optimum relight speed is: WEIGHT Pitch (°) At or below 150 000 kg -2.0 170 000 kg -1.5 190 000 kg -1.0 APU (below FL 250)......................................................................................... START THR LEVERS....................................................................................................... IDLE GLIDING DISTANCE: 2 NM / 1000 FT AT 300 KT: 2 NM / 1000 FT (500 FT/NM) NO WIND Flight Level Distance (NM) FL 200 FL 300 FL 400 40 60 80 DIVERSION....................................................................................................INITIATE Check if there is an accessible runway, or determine the most appropriate area for a forced landing or ditching. .......................................................................................................................................................................... Then, as long as none of the engines relights, apply the following paper procedure. If there is sufficient time, clear all ECAM alerts, and clear the ECAM STATUS page. VHF1......................................................................................................................USE ATC.................................................................................................................. NOTIFY CABIN OCCUPANTS...................................................................................... NOTIFY SIGNS......................................................................................................................ON CREW OXY MASK (FL > 100)............................................................................. USE FUEL QUANTITY............................................................................................. CHECK  IF ENGINE RELIGHT CAN BE ATTEMPTED Apply QRH 70.02A  IF ENGINE RELIGHT CANNOT BE ATTEMPTED (It includes the cases of no fuel remaining or engine damage) Apply QRH 70.03A TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 70.02A 18 JAN 17 ALL ENGINES FAILURE (Cont'd) Ident.: ABN-70-01-00015501.0006001 / 04 AUG 15 Applicable to: ALL IF ENGINE RELIGHT CAN BE ATTEMPTED ENG START SEL...................................................................................IGN START  APPROACHING OR BELOW FL 300: WINDMILL RELIGHT ALL ENG MASTERS.......................................................... OFF 30 S THEN ON ENGs RELIGHT..................................................................... TRY REGULARLY Windmill relight attempts can be repeated until successful, or until the APU bleed is available. APU (below FL 250) ................................................................................START  IF APU AVAILABLE AND WINDMILL RELIGHT UNSUCCESSFUL: STARTER ASSISTED RELIGHT BELOW FL 200 ALL ENG MASTERS................................................................................OFF OPTIMUM SPEED: GREEN DOT (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 WING ANTI ICE....................................................................................... OFF APU BLEED............................................................................................... ON ENG MASTER (ONE AT A TIME).............................................................ON Relight only one engine at a time. Between each attempt to relight the same engine, wait at least 30 s with the associated ENG MASTER lever set to OFF. SPEED BRAKES AVAILABLE  BELOW 10 000 FT AGL CABIN AND COCKPIT........................................................................PREPARE RAM AIR......................................................................................................... ON BARO REF (IF AVAIL).................................................................................. SET COMMERCIAL...............................................................................................OFF ELT  (when conditions permit)................................................................... ON ENGs RELIGHT..................................................................... TRY REGULARLY USE RUDDER WITH CARE  IF DITCHING ANTICIPATED Apply QRH 70.04A  IF FORCED LANDING ANTICIPATED Apply QRH 70.05A TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 70.03A 18 JAN 17 ALL ENGINES FAILURE (Cont'd) Ident.: ABN-70-01-00015504.0002001 / 04 AUG 15 Applicable to: ALL IF ENGINE RELIGHT CANNOT BE ATTEMPTED (It includes the cases of no fuel remaining or engine damage) OPTIMUM SPEED: GREEN DOT (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 GLIDING DISTANCE: 3 NM / 1000 FT AT GREEN DOT SPEED: 3 NM / 1000 FT (300 FT/NM) NO WIND Flight Level Distance (NM) FL 200 FL 300 FL 400 60 90 120 WING ANTI ICE................................................................................................. OFF APU (below FL 250) .....................................................................................START APU BLEED (below FL 200) .............................................................................. ON SPEED BRAKES AVAILABLE  BELOW 10 000 FT AGL CABIN AND COCKPIT........................................................................PREPARE RAM AIR......................................................................................................... ON BARO REF (IF AVAIL).................................................................................. SET COMMERCIAL...............................................................................................OFF ELT  (when conditions permit)................................................................... ON USE RUDDER WITH CARE  IF DITCHING ANTICIPATED Apply QRH 70.04A  IF FORCED LANDING ANTICIPATED Apply QRH 70.05A TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 70.04A ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 18 JAN 17 ALL ENGINES FAILURE (Cont'd) Ident.: ABN-70-01-00016661.0006001 / 04 AUG 15 Applicable to: ALL IF DITCHING ANTICIPATED MIN RAT SPEED: 140 KT GPWS SYS.........................................................................................................OFF GPWS TERR...................................................................................................... OFF  At an appropriate altitude (above 3 000 FT AGL), configure the aircraft for ditching. LAND RECOVERY..........................................................................................ON FOR LANDING................................................................................ USE FLAP 2 EMER GEN is lost at slat extension. The aircraft is supplied only by the batteries. L/G LEVER........................................................................................ CHECK UP VAPP............................................................................................... DETERMINE Weight 120 t 140 t 160 t 180 t 200 t 220 t 240 t VAPP 150 kt 150 kt 153 kt 160 kt 167 kt 173 kt 180 kt Ident.: ABN-70-01-00016662.0013001 / 04 AUG 15 Applicable to: ALL  AT 2 000 FT AGL CABIN OCCUPANTS...................................................NOTIFY FOR DITCHING DITCHING P/B................................................................................................ ON Ditch the aircraft parallel to the swell. If that causes a strong crosswind, ditch the aircraft into the wind.  AT 500 FT AGL BRACE FOR IMPACT............................................................................. ORDER TOUCH DOWN AT MIN V/S TARGET PITCH ATT 11 °  AT TOUCHDOWN ALL ENG MASTERS.....................................................................................OFF APU MASTER SW........................................................................................ OFF  AFTER DITCHING ATC (VHF 1)........................................................................................... NOTIFY ALL FIRE P/Bs (ENG and APU)................................................................ PUSH ALL AGENTS (ENG and APU)................................................................. DISCH Engine agent 2 is not available. EVACUATION........................................................................................ INITIATE ALL BATs...................................................................................................... OFF TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 70.05A ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 18 JAN 17 ALL ENGINES FAILURE (Cont'd) Ident.: ABN-70-01-00015506.0002001 / 04 AUG 15 Applicable to: ALL IF FORCED LANDING ANTICIPATED DESCENT SLOPE (CONF 2, L/G DOWN): 1.7 NM / 1000 FT (600 FT/NM) MIN RAT SPEED: 140 KT GPWS SYS.........................................................................................................OFF GPWS TERR...................................................................................................... OFF  At an appropriate altitude (above 3 000 FT AGL), configure the aircraft for landing. LAND RECOVERY..........................................................................................ON FOR LANDING................................................................................ USE FLAP 2 EMER GEN is lost at slat extension. The aircraft is supplied only by the batteries. MAX SPEED for GRAVITY EXTENTION...................................................200 kt L/G GRVTY EXTN.................................................................................... DOWN Disregard the "USE MAN PITCH TRIM" message on the PFD, because the stabilizer is jammed, due to not sufficient hydraulic power.  When L/G downlocked: L/G LEVER...........................................................................................DOWN VAPP............................................................................................... DETERMINE Adjust the speed to the VAPP indicated in the table below. However, to reach the landing field or runway, it is possible to increase the approach speed. Weight 120 t 140 t 160 t 180 t 200 t 220 t 240 t VAPP 150 kt 150 kt 153 kt 160 kt 167 kt 173 kt 180 kt GND SPLRs..................................................................................................ARM MAX BRK PR: 1 000 PSI Ident.: ABN-70-01-00016668.0005001 / 04 AUG 15 Applicable to: ALL  AT 2 000 FT AGL CABIN OCCUPANTS.................................................... NOTIFY FOR LANDING  AT 500 FT AGL BRACE FOR IMPACT............................................................................. ORDER  AT TOUCHDOWN ALL ENG MASTERS.....................................................................................OFF APU MASTER SW........................................................................................ OFF BRAKES ON ACCU ONLY  WHEN AIRCRAFT STOPPED PARKING BRK................................................................................................ON ATC (VHF 1)........................................................................................... NOTIFY ALL FIRE P/Bs (ENG and APU)................................................................ PUSH ALL AGENTS (ENG and APU)................................................................. DISCH Engine agent 2 is not available. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.05B 18 JAN 17 ALL ENGINES FAILURE (Cont'd)  IF EVACUATION REQUIRED EVACUATION...................................................................................INITIATE ALL BATs................................................................................................. OFF  IF EVACUATION NOT REQUIRED CABIN OCCUPANTS (PA)................................................................ NOTIFY TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 70.06A 18 JAN 17 ENG RELIGHT (IN FLIGHT) Ident.: ABN-70-00010571.0004001 / 11 MAR 13 Applicable to: ALL 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 seconds after fuel flow increases. ‐ Monitor N3 ‐ 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 Restore affected systems and set the XBLEED selector to AUTO.  If no relight: ENG MASTER (affected engine)..................................................................... OFF TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES ENG RELIGHT (IN FLIGHT) (Cont'd) TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 70.06B 18 JAN 17 A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.07A 18 JAN 17 ENG 1(2) STALL Ident.: ABN-70-A-00010572.0004001 / 08 FEB 13 Applicable to: ALL 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:  If in flight: THR LEVER (affected engine)................................................................... IDLE ENG PARAMETERS (affected engine)................................................. CHECK  If abnormal: ENG MASTER (affected engine)........................................................... OFF   If on ground: THR LEVER (affected engine)................................................................... IDLE ENG MASTER (affected engine)................................................................ OFF If the crew detects a stall before the ECAM activation: The following procedure may be applied: THR LEVER (affected engine)........................................................................ IDLE ENG PARAMETERS (affected engine)...................................................... CHECK  If abnormal parameters: ENG MASTER (affected engine)................................................................ OFF ENG 1(2) SHUT DOWN Apply ENG SHUT DOWN procedure. Engine restart at crew discretion.  If normal parameters: ENG A ICE (affected engine)....................................................................... ON WING A ICE..................................................................................................ON Operation of ENG and WING A ICE will increase the stall margin but EGT increases accordingly. THR LEVER (affected engine)..........................................SLOWLY ADVANCE  If stall does not reoccur: CONTINUE ENG OPERATION TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.08A 18 JAN 17 ENG TAILPIPE FIRE Ident.: ABN-70-00010574.0004001 / 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 N3 < 30 %: ENG START SEL........................................................................................CRANK MAN START.......................................................................................................ON  When burning has stopped: MAN START................................................................................................OFF ENG START SEL.................................................................................... NORM TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 70.09A 18 JAN 17 HIGH ENGINE VIBRATION Ident.: ABN-70-00010575.0004001 / 21 JUL 14 Applicable to: ALL The ECAM ’s VIB advisory mainly serves as 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 /N3 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 70.10A ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 18 JAN 17 SUSPECTED ENG FUEL SYS CONTAMINATION Ident.: ABN-70-00013978.0001001 / 08 FEB 13 Applicable to: ALL 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 ENG FUEL SYS CONTAMINATION Ident.: ABN-70-00013979.0001001 / 24 FEB 14 Applicable to: ALL 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 58.1 58.7 59.4 60.1 60.8 61.6 62.5 63.3 64.1 65.0 65.9 66.8 67.7 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 70.10B 18 JAN 17 ENG FUEL SYS CONTAMINATION (Cont'd)  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  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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 18 JAN 17 ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 80.01A 06 MAR 17 CIRCLING APPROACH WITH ONE ENGINE INOPERATIVE Ident.: ABN-80-00010581.0014001 / 08 FEB 13 Applicable to: ALL 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 0 232 224 214 208 200 192 182 170 5 232 224 214 208 200 192 178 158 10 232 224 214 208 200 186 172 158 15 232 224 214 208 194 180 168 156 20 232 224 214 202 188 174 158 150 25 232 224 210 196 182 168 156 146 30 232 218 202 188 174 158 150 35 224 208 194 180 168 156 40 216 200 186 174 45 206 192 178 50 198 184 55 190 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02A 06 MAR 17 BOMB ON BOARD Ident.: ABN-80-00010582.0012001 / 17 MAR 16 Applicable to: ALL 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 using manual pressure mode. 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 using the cabin V/S target selector. During the approach, use automatic pressure mode in order to reduce the differential pressure to zero at touchdown. 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 OCCUPANTS................................................................................ 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.02B 06 MAR 17 BOMB ON BOARD (Cont'd) DESCENT TO CAB ALT + 2 500 ft or MEA or minimum obstacle clearance altitude ................................................................................................................. INITIATE AVOID SHARP MANEUVERS CAB ALT................................................................................................MAINTAIN  When at CAB ALT + 2 500 ft: 1 PSI ΔP...........................................................................................MAINTAIN GALLEY/LAV FAN......................................................................................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 occupants about the emergency encountered and the intentions. Press the EVAC COMMAND pb  . ALL BATs.............................................................................................. OFF  If evacuation not required : CABIN OCCUPANTS (PA)............................................................. NOTIFY TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.03A 06 MAR 17 DITCHING Ident.: ABN-80-00010583.0047001 / 04 AUG 15 Applicable to: ALL This procedure applies when engines are running. If engines are not running, Refer to QRH ABN-70 ALL ENGINES FAILURE - IF DITCHING ANTICIPATED, 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. 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 ELT (when conditions permit).............................................................................. ON APPROACH L/G lever............................................................................................................... UP SLATS and FLAPS.................................................................................MAX AVAIL 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 AGENTS (ENG and APU)..............................................................................DISCH TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.03B 06 MAR 17 DITCHING (Cont'd) EVACUATION............................................................................................. INITIATE Notify the cabin crew about the emergency encountered and the intentions. Press the EVAC COMMAND pb  . ALL BATs............................................................................................................OFF TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.04A 06 MAR 17 FORCED LANDING Ident.: ABN-80-00010584.0048001 / 04 AUG 15 Applicable to: ALL This procedure is applicable if the engines are running. If the engines are not running, Refer to QRH ABN-70 ALL ENGINES FAILURE - IF FORCED LANDING ANTICIPATED: 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. 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 ELT (when conditions permit).............................................................................. ON APPROACH RAM AIR...............................................................................................................ON L/G lever......................................................................................................... DOWN SLATS and FLAPS.................................................................................MAX AVAIL GND SPLR.........................................................................................................ARM MAX BRK PR............................................................................................. 1000 PSI AT 2 000 FT AGL CABIN OCCUPANTS......................................................... 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 AGENTS (ENG and APU).........................................................................DISCH TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.04B 06 MAR 17 FORCED LANDING (Cont'd)  If Evacuation required : EVACUATION...................................................................................INITIATE ALL BATs................................................................................................. OFF  If Evacuation not required : CABIN OCCUPANTS (PA)................................................................ NOTIFY TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.05A 06 MAR 17 EMER DESCENT Ident.: ABN-80-00010585.0005001 / 18 MAY 16 Applicable to: ALL CREW OXY MASKS............................................................................................ USE SIGNS.....................................................................................................................ON EMER DESCENT..........................................................................................INITIATE  If A/THR is not active: THR LEVERS................................................................................................. IDLE SPD BRK............................................................................................................ FULL WHEN DESCENT ESTABLISHED 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. 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. The flight crew can communicate with the ATC using voice, or CPDLC when the voice contact cannot be established or has poor quality. EMER DESCENT (PA)......................................................................... ANNOUNCE The flight crew must inform the cabin of emergency descent on the PA system. 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 set to 100 %, oxygen quantity may be insufficient to cover the entire emergency descent profile ‐ Ensure that crew communication is established with oxygen masks. Avoid the continuous use of the interphone to minimize interference with the breathing noise in the oxygen mask. MAX FL........................................................................................... 100/MEA-MORA  If CAB ALT is above 14 000 ft: CAB OXY MASKS................................................................................. MAN ON Note: Notify the cabin crew, when the aircraft reaches a safe flight level, and when cabin oxygen is no more necessary. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 80.06A 06 MAR 17 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 80.07A 06 MAR 17 OVERWEIGHT LANDING Ident.: ABN-80-00010586.0019001 / 17 MAR 16 Applicable to: ALL 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. 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) CLIMB GRADIENT 2.1 % OAT (°C) AIRPORT ELEVATION (FT) 0 2 000 4 000 6 000 8 000 10 000 12 000 14 000 10 240 232 223 209 196 180 164 148 15 240 232 223 209 194 176 160 144 20 240 232 223 207 191 171 155 140 25 240 232 221 205 188 166 150 136 30 240 232 216 200 182 161 146 35 240 224 208 192 176 40 233 216 199 184 45 222 205 189 50 211 195 55 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 80.08A 06 MAR 17 STALL RECOVERY Ident.: ABN-80-00013762.0001001 / 15 JUN 15 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.09A 06 MAR 17 TAILSTRIKE Ident.: ABN-80-00010587.0001001 / 04 AUG 15 Applicable to: ALL In the event of a tailstrike, apply the following procedure: LAND ASAP MAX FL.............................................................................................. 100/MEA-MORA Limit to FL 100 or to MEA or MORA in order to minimize structural stress. Return to the airport for damage assessment. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 80.10A 06 MAR 17 VOLCANIC ASH ENCOUNTER Ident.: ABN-80-00010588.0007001 / 06 SEP 16 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 OCCUPANTS................................................................................. 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 both engines flame out and speed indications are lost, Refer to QRH ABN-70 ALL ENGINES FAILURE 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.11A 06 MAR 17 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 80.12A 06 MAR 17 WINDSHEAR AHEAD Ident.: ABN-80-00010590.0002001 / 09 APR 15 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.12B 06 MAR 17 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 , or use the LDG PERF application of FlySmart with Airbus for VAPP determination. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.13A 06 MAR 17 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). TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE 80.14A ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 06 MAR 17 COCKPIT WINDSHIELD / WINDOW CRACKED Ident.: ABN-80-00010893.0001001 / 04 AUG 15 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-MORA The inner ply is affected. The flight crew is not able to easily determine if other plies are affected. Descend to FL 230/MEA-MORA and reduce differential pressure to 5 PSI. Note: The maximum flight level is restricted to FL 230/MEA -MORA 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  Note: 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 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.15A 06 MAR 17 ECAM ADVISORY CONDITIONS SYSTEM CONDITIONS RECOMMENDED ACTION Ident.: ABN-80-A-00010592.0001001 / 08 FEB 13 Applicable to: ALL 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 / 28 AUG 15 Applicable to: ALL ELEC IDG OIL TEMP T > 151 °C Reduce IDG load, if possible (GALLEY 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 Applicable to: ALL 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-00010596.0016001 / 20 SEP 13 Applicable to: ALL CKPT & CAB OXY Pulses Green: OXY/DOOR When pressure is < 1 200 PSI Amber: When pressure is < 200 PSI If cockpit masks are not being used check that they are correctly stowed. Ident.: ABN-80-A-00010597.0001001 / 08 FEB 13 Applicable to: ALL 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-00010598.0004001 / 24 FEB 14 Applicable to: ALL ENG OIL QTY < 4 US QTS 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 ≥ 3.3 units N2 ≥ 2.6 units N3 ≥ 4.0 units Refer to QRH ABN-70 High Engine Vibration. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.16A 06 MAR 17 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/B s, 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES 80.17A 06 MAR 17 COMPUTER RESET - GENERAL Ident.: ABN-80-00010641.0001001 / 06 DEC 16 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. Note: The flight crew should report any in-flight reset to the maintenance. The following table lists the various computers for which manual reset capability is provided: • On the overhead RESET panels, • On the system control panel. WARNING The flight crew can attempt a computer reset only when: ‐ An ECAM /OEB /TDU procedure requests to reset the system, or ‐ The Computer Reset Table permits to reset the system. Manual reset on ground triggers complete power up test. Note: In flight, before taking any action on the reset buttons, the PF and PM must crosscheck and verify that the reset button corresponds to the affected system. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 80.18A 06 MAR 17 COMPUTER RESET TABLE ATA EQUIPMENT REMARKS Ident.: ABN-80-F-00010642.0002001 / 21 AUG 13 Applicable to: ALL PACK CONT ZONE CONT NIL AEVC VENT CONT 21 CPC If, in flight, the SMOKE CAB REST SMOKE warning has been temporarily displayed and identified as a false warning, crew rest compartment ventilation may be recovered by resetting both VENT controller channels (simultaneously pull both ventilation controller RESET pb for at least 5 s, then push them). 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 / 06 JAN 16 Applicable to: ALL 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 FM s 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: Due to electrical transient, MANUAL FMGES RESET procedure may be unsuccessful. If so and on ground, the flight crew may attempt the same procedure with engines not running. For more information, Refer to FCOM/PRO-SUP-22-10 Automatic FMGES Reset and Resynchronization - FM Reset MCDU blank or locked ‐ Set MCDU (affected) to OFF ‐ Wait 10 s ‐ Set MCDU (affected) to ON Note: Wait after the message "PLEASE WAIT" disappears before using MCDU. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18B 06 MAR 17 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00016076.0001001 / 17 NOV 16 Applicable to: ALL 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, RMP s must be switched off at least 5 s by using the ON/OFF selector on the RMP control panels. PAX SATCOM SYSTEM  PAX SATCOM system 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 / 23 JUN 15 Applicable to: ALL GPCU /GAPCU * 24 GPCU /GAPCU 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 /GAPCU. 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18C 06 MAR 17 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00010648.0001001 / 21 MAR 11 Applicable to: ALL Commercial equipments and galleys 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. 25 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. Ident.: ABN-80-F-00010649.0002001 / 25 APR 12 Applicable to: ALL 26 Smoke detection function of the On ground CIDS-SDF ‐ Pull both SDF1 (261VU) and SDF2 (262VU) reset buttons ‐ Wait 10 s ‐ Push both SDF1 and SDF2 reset buttons. ‐ Wait 3 min for the system restart to be completed. In flight ‐ Pull both SDF1 (261VU) and SDF2 (262VU) reset buttons ‐ Wait 3 s ‐ Push both SDF1 and SDF2 reset buttons. ‐ Wait 1 min for the system restart to be completed. Ident.: ABN-80-F-00010650.0002001 / 21 AUG 13 Applicable to: ALL 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NIL A330-243F QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18D 06 MAR 17 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00010651.0003001 / 24 FEB 14 Applicable to: ALL FCMC ‐ 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 %: 28 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. Ident.: ABN-80-F-00010652.0001001 / 21 MAR 11 Applicable to: ALL 30 PHC WHC Associated heating is interrupted, when the reset pb is pulled. Ident.: ABN-80-F-00010653.0001001 / 21 MAR 11 Applicable to: ALL 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ATA 80.18E ABNORMAL AND EMERGENCY PROCEDURES 06 MAR 17 Continued from the previous page EQUIPMENT REMARKS Ident.: TDU / ABN-80-F-00015048.0001001 / 07 OCT 13 Applicable to: ALL BSCU* In flight: Not authorized. On ground and only for the following cases: In case of BRAKES RESIDUAL ‐ 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 BRAKING: 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18F 06 MAR 17 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00014555.0001001 / 23 JUN 15 Applicable to: ALL 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 ‐ Check that the affected Engine Bleed Valve is closed on the BLEED SD page. Note: Record the ENG BLEED reset in the logbook (successful or unsuccessful). TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18G 06 MAR 17 Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00010655.0001001 / 17 NOV 11 Applicable to: ALL 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 / 21 APR 15 Applicable to: ALL 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 Applicable to: ALL 49 ECB * Reset must only be attempted when APU speed is below 7 % Ident.: ABN-80-F-00010658.0001001 / 21 MAR 11 Applicable to: ALL 52 PSCU TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NIL A330-243F QUICK REFERENCE HANDBOOK ATA ABNORMAL AND EMERGENCY PROCEDURES 80.18H Continued from the previous page EQUIPMENT REMARKS Ident.: ABN-80-F-00010659.0004001 / 04 MAR 13 Applicable to: ALL EIVMU 70 06 MAR 17 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 06 MAR 17 A330-243F QUICK REFERENCE HANDBOOK NORMAL PROCEDURES TABLE OF CONTENTS NP 1/2 06 DEC 16 Normal Procedures NP-NP Safety Exterior Inspection.......................................................................1/14 Preliminary Cockpit Preparation............................................................. 1/14 Cockpit Preparation................................................................................ 2/14 Before Pushback or Start....................................................................... 3/14 ENG Start............................................................................................... 4/14 After Start............................................................................................... 4/14 Taxi......................................................................................................... 4/14 Before Takeoff........................................................................................ 5/14 Takeoff.................................................................................................... 5/14 After Takeoff........................................................................................... 6/14 Climb.......................................................................................................6/14 Cruise......................................................................................................7/14 Descent Preparation............................................................................... 7/14 Descent...................................................................................................7/14 Aircraft Configuration for Approach........................................................ 8/14 Approach using LOC G/S Guidance...................................................... 9/14 Approach using FINAL APP Guidance.................................................. 9/14 Approach using FINAL APP Guidance for RNAV(RNP).......................10/14 Approach using FPA Guidance............................................................ 11/14 Landing................................................................................................. 12/14 Go Around............................................................................................ 12/14 After Landing........................................................................................ 13/14 Parking..................................................................................................13/14 Securing the Aircraft.............................................................................14/14 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK NORMAL PROCEDURES TABLE OF CONTENTS Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP 2/2 06 DEC 16 NP-NP 1/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK SAFETY EXTERIOR INSPECTION Ident.: NP-NP-00010661.0001001 / 23 DEC 14 Applicable to: ALL PF PM * WHEEL CHOCKS........................................................ CHECK * L/G DOORS...............................................CHECK POSITION * APU AREA................................................................... CHECK PRELIMINARY COCKPIT PREPARATION Ident.: NP-NP-00010662.0014001 / 30 MAR 15 Applicable to: ALL PF PM ENG MASTERS 1, 2............................................................. OFF ENG START selector........................................... CHECK NORM * WEATHER RADAR........................................................... OFF L/G lever............................................................................ DOWN 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 LIGHTS................................................... 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/BRAKE PRESS.................................................CHECK ALTN BRAKING............................................................... CHECK CARGO TEMP panel............................................................. SET EMER EQPT.....................................................................CHECK RAIN REPELLENT........................................................... CHECK * OEB IN QRH................................................................ CHECK EMER CAB EQPT............................................................ CHECK FAP pages........................................................................ CHECK * CAB OCCUPANTS BRIEFING...............................PERFORM * GEAR PINS and COVERS.......CHECK ONBOARD/STOWED * EXTERIOR WALKAROUND...................................PERFORM TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 2/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK COCKPIT PREPARATION Ident.: NP-NP-00010663.0014001 / 26 MAY 15 Applicable to: ALL PF OVERHEAD PANEL: * ALL WHITE LIGHTS.......................................... EXTINGUISH * RCDR GND CTL pb-sw......................................................ON CAPT & PURS/CAPT sw  .................................... AS RQRD * 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 FLOW............................................................AS RQRD ELEC panel...................................................................... CHECK BAT...................................................................................CHECK FUEL T. TANK....................................................................AUTO ENG FIRE.............................................................. CHECK/TEST MAINT panel.....................................................................CHECK VENT panel...................................................................... CHECK PA (3rd occupant).......................................................... RECEPT CVR TEST pb...................................................................PRESS * RESET BUTTONS (right side).....................................CHECK DATA LOADER  ...............................................CHECK OFF CTR INSTRUMENT PANEL: * ISIS.............................................................................. 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...............................................................................STDBY RMP....................................................................................... SET * AIRFIELD DATA......................................................... OBTAIN * MSG RECORD (MCDU).............................................. ERASE * ADS (MCDU)................................................. CHECK ARMED * ACARS  .......................................................... INITIALIZE TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PM NP-NP 3/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM * FMS......................................................................... PREPARE * FMS PREPARATION................................................... CHECK •When both flight crewmembers seated: GLARESHIELD: GLARESHIELD: * 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 BEFORE PUSHBACK OR START Ident.: NP-NP-00010664.0005001 / 09 FEB 15 Applicable to: ALL PF PM CAB DOORS..................................................................CLOSE SLIDES............................................................................... ARM CAB TO CARGO DOORS............................................. CLOSE CABIN SECURED.................................................... CHECKED LOADSHEET....................................................................... CHECK LOADSHEET..................................................................CHECK FOB......................................................................................CHECK FOB................................................................................CHECK FMS TO DATA................................... CHECK/REVISE AS RQRD REVISED FMS TO DATA.......................................... XCHECK SEATING POSITION......................................................... ADJUST SEATING POSITION....................................................ADJUST FMS PERF TO page......................................................SELECT FMS F-PLN page.......................................................SELECT 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 PUSHBACK/START CLEARANCE...............................OBTAIN ATC...................................................... SET FOR OPERATION WINDOW/DOORS............................................... CHECK CLOSED WINDOW/DOORS......................................... CHECK CLOSED SLIDES.................................................................. CHECK ARMED SLIDES............................................................ CHECK ARMED EXTERIOR LIGHTS.................................................................. SET THRUST LEVERS....................................................................IDLE ACCU PRESS..................................................................... CHECK NW STRG DISC................................................ CHECK AS RQRD PARK BRK...................................................................... AS RQRD BEFORE START C/L below the line............................ COMPLETE BEFORE START C/L below the line...................... COMPLETE TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 4/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK ENG START Ident.: NP-NP-00010665.0003001 / 23 DEC 14 Applicable to: ALL PF PM 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-00010666.0006001 / 15 JUN 15 Applicable to: ALL PF PM 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..................................................................... CHECK NWS TOWING FAULT LT  ..................................CHECK off ECAM STATUS................................................................ CHECK ECAM STATUS................................................................ CHECK N/W STEER DISC MEMO.................. CHECK NOT DISPLAYED CLEAR TO DISCONNECT....................................... ANNOUNCE AFTER START C/L................................................... COMPLETE AFTER START C/L................................................... COMPLETE TAXI Ident.: NP-NP-00010667.0040001 / 06 SEP 16 Applicable to: ALL PF PM •Taxi clearance obtained: EXTERIOR LIGHTS............................................................... SET TAXI CLEARANCE.......................................................... OBTAIN PARKING BRAKE handle......................................................OFF BRAKES PRESSURE......................................CHECK AT ZERO THRUST LEVERS........................................................ AS RQRD BRAKES............................................................................CHECK BRAKES PRESSURE......................................CHECK AT ZERO TILLER or RUDDER PEDALS............................. USE AS RQRD FLT CTL............................................................................CHECK FLT CTL............................................................................CHECK •ATC clearance obtained: ATC CLEARANCE........................................................CONFIRM T.O DATA......................................................................... CHECK FMS F-PLAN /SPD...........................................................CHECK FCU ALT /HDG...................................................................... SET BOTH FD................................................................... CHECK ON PFD /ND........................................................................... CHECK PFD /ND........................................................................... CHECK TAKEOFF BRIEFING................................................... CONFIRM RADAR and PREDICTIVE WINDSHEAR SYSTEM..... AS RQRD ATC CODE/MODE..................... CONFIRM/SET FOR TAKEOFF TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 5/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM TERR ON ND............................................................... AS RQRD TERR ON ND............................................................... AS RQRD AUTO BRK............................................................................ MAX T.O CONFIG pb...................................................................TEST T.O MEMO ..................................................... CHECK NO BLUE BEFORE TAKEOFF C/L down to the line................. COMPLETE BEFORE TAKEOFF C/L down to the line................. COMPLETE BEFORE TAKEOFF Ident.: NP-NP-00010668.0005001 / 23 DEC 14 Applicable to: ALL PF PM BRAKE TEMP (if brake fan  running)....................... 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 ENG START selector................................................... AS RQRD SLIDING TABLE  ...................................................STOWED SLIDING TABLE  ...................................................STOWED THRUST BUMP  ...................................................AS RQRD TAKEOFF RUNWAY.................................................... CONFIRM TAKEOFF RUNWAY.................................................... CONFIRM PACKS 1+2.................................................................. AS RQRD BEFORE TAKEOFF C/L below the line.................... COMPLETE BEFORE TAKEOFF C/L below the line.................... COMPLETE TAKEOFF Ident.: NP-NP-00010669.0003001 / 28 JUL 15 Applicable to: ALL PF PM 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: V1.....................................................MONITOR OR ANNOUNCE •AT VR: ROTATION....................................................................... ORDER ROTATION.................................................................. PERFORM •WHEN POSITIVE CLIMB: POSITIVE CLIMB..................................................... ANNOUNCE L/G UP..............................................................................ORDER L/G.............................................................................SELECT UP AP................................................................................. AS RQRD TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 6/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM •AT THR RED ALT: THRUST LEVERS.................................................................... CL PACK 1+2 (if applicable)......................................................... 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 AFTER TAKEOFF Ident.: NP-NP-00010670.0001001 / 23 DEC 14 Applicable to: ALL PF PM 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 / 23 DEC 14 Applicable to: ALL PF PM 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 7/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK CRUISE Ident.: NP-NP-00010672.0011001 / 23 DEC 14 Applicable to: ALL PF PM ECAM MEMO/SD PAGES.............................................. REVIEW FLIGHT PROGRESS........................................................CHECK FUEL.............................................................................MONITOR STEP FLIGHT LEVEL................................... AS APPROPRIATE NAVIGATION ACCURACY.......................................... MONITOR RADAR........................................... ADJUST AS APPROPRIATE DESCENT PREPARATION Ident.: NP-NP-00010673.0002001 / 23 DEC 14 Applicable to: ALL PF PM 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-00010674.0008001 / 23 DEC 14 Applicable to: ALL PF PM 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..................................................................SET SEAT BELTS sw..................................................................... ON EFIS option pb..................................................................... CSTR EFIS option pb.................................................................... CSTR LS pb.............................................................................AS RQRD LS pb............................................................................AS RQRD RADIO NAV........................................................ SELECT/IDENT ENG START selector...................................................AS RQRD TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 8/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM •If GPS PRIMARY not available: NAV ACCY........................................................................ CHECK APPROACH C/L........................................................ COMPLETE APPROACH C/L....................................................... COMPLETE AIRCRAFT CONFIGURATION FOR APPROACH Ident.: NP-NP-00014801.0004001 / 20 JUL 15 Applicable to: ALL PF PM 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 minimum: 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 SPEED TARGET............................................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 OCCUPANTS.......................................................ADVISE TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 9/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM 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; speed target - 5 kt • PITCH : 0 ° nose down; 10 ° nose up • BANK : 7 ° (1) PF if AP is ON, PM if AP is OFF. The PF may request that this action is performed by the PM depending on the situation. APPROACH USING LOC G/S GUIDANCE Ident.: NP-NP-00014802.0001001 / 23 DEC 14 Applicable to: ALL PF PM 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................. MONITOR OR ANNOUNCE •At minimum: CONTINUE or GO-AROUND................................... ANNOUNCE MINIMUM......................................... MONITOR OR ANNOUNCE (1) PF if AP is ON, PM if AP is OFF. The PF may request that this action is performed by the PM depending on the situation. APPROACH USING FINAL APP GUIDANCE Ident.: NP-NP-00014803.0002001 / 23 DEC 14 Applicable to: ALL PF PM DESCENT PREPARATION: WEATHER AND LANDING INFO................................... OBTAIN F-PLN A Page...................................................................CHECK F-PLN A Page..................................................................CHECK PROG Page............................................................... COMPLETE PROG Page.............................................................. COMPLETE TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 10/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM 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.................MONITOR OR ANNOUNCE •At minimum: CONTINUE or GO-AROUND....................................ANNOUNCE MINIMUM.........................................MONITOR OR ANNOUNCE (1) PF if AP is ON, PM if AP is OFF. The PF may request that this action is performed by the PM depending on the situation. APPROACH USING FINAL APP GUIDANCE FOR RNAV(RNP) Ident.: NP-NP-00014806.0003001 / 23 DEC 14 Applicable to: ALL PF PM DESCENT PREPARATION: WEATHER AND LANDING INFO.................................... OBTAIN NAVAID......................................................................DESELECT PROG Page.............................................................. COMPLETE PROG Page............................................................... COMPLETE GO-AROUND STRATEGY............................................. REVIEW DESCENT: GPS PRIMARY ON BOTH FMS......................................CHECK GPS 1+2.................................................. CHECK BOTH IN NAV TERR ON ND...............................................................AS RQRD INITIAL/INTERMEDIATE/FINAL APPROACH: BARO REF/ALTIMETER..................................................CHECK FD or AP /FD.......................................... USE FOR APPROACH L/DEV..........................................................CHECK DISPLAYED APPR pb on FCU............................................................. PRESS APP NAV.................................. CHECK ARMED OR ENGAGED FINAL................................................................. CHECK ARMED •At the Final Descent Point: FINAL APP....................................................CHECK ENGAGED TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 11/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM GO-AROUND ALT................................................................................................ SET(1) FLT PARAMETERS......................................................MONITOR Announce any deviation in excess of: • L/DEV : 1 dot or XTK > 0.1 NM • V/DEV > ½ dot •At minimum + 100 ft: ONE HUNDRED ABOVE..................MONITOR OR ANNOUNCE •At minimum: CONTINUE or GO-AROUND................................... ANNOUNCE MINIMUM..........................................MONITOR OR ANNOUNCE (1) PF if AP is ON, PM if AP is OFF. The PF may request that this action is performed by the PM depending on the situation. APPROACH USING FPA GUIDANCE Ident.: NP-NP-00014804.0002001 / 23 DEC 14 Applicable to: ALL PF PM DESCENT PREPARATION: F-PLN A Page...................................................................CHECK F-PLN A Page.................................................................. CHECK PROG Page...............................................................COMPLETE PROG Page.............................................................. COMPLETE 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 selector......................................................................... 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 ° TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 12/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM •At minimum + 100 ft: ONE HUNDRED ABOVE................. MONITOR OR ANNOUNCE •At minimum: CONTINUE or GO-AROUND....................................ANNOUNCE MINIMUM......................................... MONITOR OR ANNOUNCE (1) PF if AP is ON, PM if AP is OFF. The PF may request that this action is performed by the PM depending on the situation. LANDING Ident.: NP-NP-00010678.0003001 / 23 DEC 14 Applicable to: ALL PF PM •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 •At taxi speed: ALL REVERSER LEVERS................................................. STOW •Before 20 kt: AUTO BRK...............................................................DISENGAGE GO AROUND Ident.: NP-NP-00010679.0001001 / 23 DEC 14 Applicable to: ALL PF PM 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 13/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK Continued from the previous page PF PM •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 / 22 APR 16 Applicable to: ALL PF PM GRND SPLRS................................................................. DISARM EXTERIOR LIGHTS............................................................... SET RADAR................................................................................... OFF PREDICTIVE WINDSHEAR  ..........................................OFF ENG START selector......................................................... NORM FLAPS.......................................................................... RETRACT TCAS...................................................................SET on standby ATC...............................................................................AS RQRD APU....................................................................................START ANTI ICE...................................................................... AS RQRD BRAKE TEMP...................................................................CHECK AFTER LDG C/L...................................................... COMPLETE AFTER LDG C/L...................................................... COMPLETE PARKING Ident.: NP-NP-00010681.0007001 / 09 FEB 15 Applicable to: ALL PF PM ACCU PRESS.................................................................. CHECK ANTI-ICE................................................................................ OFF PARKING BRAKE handle........................................................ON APU BLEED pb-sw..................................................................ON ENG MASTER 1, 2................................................................OFF FUEL PUMPS........................................................................ OFF EXTERIOR LIGHTS............................................................... SET ATC....................................................................................STDBY GROUND CONTACT................................................ ESTABLISH SEAT BELTS sw....................................................................OFF IRS DRIFT RATE............................................................. CHECK FUEL QTY........................................................................ CHECK STATUS............................................................................ CHECK PARK BRK....................................................................AS RQRD BRAKE FAN  ................................................................. OFF DU's........................................................................................ DIM DU's........................................................................................ DIM PARKING C/L............................................................COMPLETE SLIDES..........................................................................DISARME CABIN DOORS................................................ OPEN, AS RQRD TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE NP-NP 14/14 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK SECURING THE AIRCRAFT Ident.: NP-NP-00010682.0001001 / 21 AUG 15 Applicable to: ALL PF PM PARK BRK................................................................. CHECK ON ALL IR MODE selectors.........................................................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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK IN FLIGHT PERFORMANCE TABLE OF CONTENTS PER 1/2 18 JAN 17 Speeds PER-A Operating Speeds.....................................................................................1/2 Green Dot Speed..................................................................................... 1/2 VLS........................................................................................................... 2/2 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........................................................ 4/6 VAPP Determination with Failure............................................................. 5/6 Landing Distance without Failure PER-D Landing Distance without Failure ............................................................1/2 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK IN FLIGHT PERFORMANCE TABLE OF CONTENTS PER 2/2 18 JAN 17 Continued from the previous page One Engine Inoperative PER-E Ceilings..................................................................................................... 1/4 Gross Flight Path Descent at Green Dot Speed...................................... 2/4 Cruise at Long Range Cruise speed........................................................3/4 In Cruise Quick Check Long Range.........................................................4/4 All Engines Operative PER-G Optimum & Maximum Altitudes................................................................1/4 In Cruise Quick Check at a Given Mach Number.................................... 2/4 Cost Index for Long Range Cruise SpeeD...............................................3/4 Standard Descent.....................................................................................3/4 Quick Determination Table of Alternate Flight Planning...........................4/4 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-A 1/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK OPERATING SPEEDS Ident.: PER-A-00010699.0044001 / 08 FEB 13 Applicable to: ALL OPERATING SPEEDS (KT) Weight (1000 KG) S VLS CONF 1 F (1) VLS CONF 2 VLS CONF 3 VREF 240 205 187 168 165 159 157 220 197 179 161 158 152 150 200 187 170 153 150 145 143 180 178 162 145 143 138 136 160 168 152 137 135 130 128 140 157 143 128 126 122 120 120 152 138 123 122 118 118 110 152 138 123 122 118 118 (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). Note: If Weight (W ) <193 t and CG <18%, 1 kt must be added to: VLS CONF 1, VLS CONF 2, VLS CONF 3 and VREF. GREEN DOT SPEED Ident.: PER-A-00010700.0041001 / 08 FEB 13 Applicable to: ALL GREEN DOT SPEED (KT) ALL ENGINES OPERATIVE Weight (1000 KG) at or below FL 200 FL 300 FL 400 240 251 261 271 220 239 249 259 200 227 237 247 180 215 225 235 160 203 213 223 140 191 201 211 120 179 189 199 110 179 189 199 GREEN DOT SPEED WITH ONE OR TWO ENGINES INOP : Subtract 10 kt from these values. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-A 2/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK VLS Ident.: PER-A-00010701.0042001 / 08 FEB 13 Applicable to: ALL VLS CONF 0 (KT) Weight (1000 KG) Note: 1.23 VS 0.3 g buffet margin FL 0 FL 100 FL 200 FL 200 FL 300 FL 400 240 209 222 237 233 245 293 220 200 207 226 220 233 268 200 190 192 214 206 220 243 180 181 181 200 193 206 221 160 170 171 182 177 194 203 140 159 159 163 160 177 187 120 154 154 154 152 169 179 110 154 154 154 152 169 179 If Weight (W ) <193 t and CG <18%, 1 kt must be added in 1.23 VS at: FL 0, FL 100 and FL 200 columns. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-B 1/4 07 JUN 16 USE OF FUEL PENALTY FACTOR TABLES Ident.: PER-B-00014176.0001001 / 10 MAY 16 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 or FUEL CONSUMPT INCRSD 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 % TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-B 2/4 07 JUN 16 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 ELEV REDUND LOST 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) 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 % 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 - 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 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 Spoilers 2, 3, 4 and 6 (1) 0% to 15 % (4) All landing gears are extended 180 % All landing gears doors are extended 15 % Stabilizer is jammed RETRACTION FAULT L(R) LENGTHENING FAULT L/G GEAR NOT UPLOCKED L/G RETRACT GEAR UPLOCK FAULT DOORS NOT CLOSED L/G DOOR TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-B 3/4 IN FLIGHT PERFORMANCE A330-243F 07 JUN 16 QUICK REFERENCE HANDBOOK (1) During the flight, the spoiler(s) may gradually extend and increase(s) the fuel consumption. (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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-B 4/4 07 JUN 16 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-C 1/6 18 JAN 17 METHOD TO DETERMINE AIRCRAFT PERFORMANCE AT LANDING WITHOUT OR WITH A SINGLE FAILURE Ident.: PER-C-00015213.0001001 / 20 AUG 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): TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-C 2/6 18 JAN 17 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): TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-C 3/6 IN FLIGHT PERFORMANCE A330-243F 18 JAN 17 QUICK REFERENCE HANDBOOK RUNWAY CONDITION ASSESSMENT MATRIX FOR LANDING Ident.: PER-C-00014117.0006001 / 20 DEC 16 Applicable to: ALL Runway Surface Conditions Runway State or / and Runway Contaminant Related Landing Performance Observations on Deceleration and Directional Control Code Level Maximum Crosswind for Landing (Gust included) - - 6 DRY 45 kt Good Braking deceleration is normal for the wheel braking effort applied. Directional control is normal. 5 GOOD 45 kt Good to Medium Braking deceleration and controllability is between Good and Medium. 4 GOOD TO MEDIUM 27 kt Medium Braking deceleration is noticeably reduced for the wheel braking effort applied. Directional control may be reduced. 3 MEDIUM 20 kt Medium to Poor Braking deceleration and controllability is between Medium and Poor. Potential for hydroplaning exists. 2 MEDIUM TO POOR 20 kt Poor Braking deceleration is significantly reduced for the wheel braking effort applied. Directional control may be significantly reduced. 1 POOR 15 kt Nil Braking deceleration is minimal to non-existant for the wheel braking effort applied. Directional control may be uncertain. - - - ESF(1) or PIREP(2) Dry Damp Wet Up to 3 mm (1/8'') of water Slush Up to 3 mm (1/8'') Dry snow Up to 3 mm (1/8'') Wet snow Up to 3 mm (1/8'') Frost Compacted snow OAT at or below -15 °C Dry snow More than 3 mm (1/8''), up to 100 mm (4'') Wet snow More than 3 mm (1/8''), up to 30 mm (6/5'') Compacted snow OAT above -15 °C Dry snow over compacted snow Wet snow over compacted snow Slippery when wet Water More than 3 mm (1/8''), up to 12.7 mm (1/2'') Slush More than 3 mm (1/8''), up to 12.7 mm (1/2'') Ice (cold & dry) Wet ice Water on top of Compacted Snow Dry Snow or Wet Snow over ice (1) ESF: Estimated Surface Friction (2) PIREP: Pilot Report of Braking Action Note: Refer to FCOM LIM-AFS chapter for Automatic Approach, Landing and Rollout limitations. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-C 4/6 18 JAN 17 VAPP DETERMINATION WITHOUT FAILURE Ident.: PER-C-00014116.0034001 / 28 FEB 14 Applicable to: ALL The FMGS performs the following VAPP computation for landing in normal configuration (CONF 3 or CONF FULL). TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK VAPP DETERMINATION WITH FAILURE Ident.: PER-C-00014312.0038001 / 28 FEB 14 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-C 5/6 18 JAN 17 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-C 6/6 18 JAN 17 PER-D 1/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK LANDING DISTANCE WITHOUT FAILURE Ident.: PER-D-00014090.0090001 / 28 FEB 14 Applicable to: ALL 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 (ft) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF (2) WGT SPD REF DIST Per 10T (ft) for above Per 5kt 190T 190T ALT WIND Per 1000ft above SL Per 5kt TW TEMP SLOPE Per 10°C Per 1% above Down ISA Slope REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 4 340 + 520 + 270 + 150 + 430 + 130 + 70 - 40 + 1 880 3 4 530 + 560 + 270 + 160 + 450 + 140 + 80 - 40 + 2 190 FULL 5 470 + 460 + 310 + 170 + 480 + 160 + 60 - 10 + 210 3 5 720 + 500 + 330 + 180 + 490 + 170 + 70 - 10 + 220 FULL 7 300 + 510 + 430 + 250 + 700 + 230 + 100 - 90 + 300 3 7 700 + 550 + 450 + 260 + 720 + 240 + 120 - 90 + 320 (1) Automatic Landing correction: if CONF FULL, add 580ft. If CONF 3, add 550ft. (2) Weight correction: if CONF FULL, subtract 150ft per 10T below 190T. If CONF 3, subtract 170ft per 10T below 190T. 5 - GOOD Corrections on Landing Distance (ft) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF (2) WGT SPD REF DIST Per 10T (ft) for above Per 5kt 190T 190T ALT WIND Per 1000ft above SL Per 5kt TW TEMP SLOPE Per 10°C Per 1% above Down ISA Slope REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 5 320 + 570 + 410 + 250 + 730 + 220 + 150 - 90 + 1 450 3 5 690 + 650 + 440 + 270 + 780 + 240 + 190 - 100 + 1 710 FULL 5 840 + 580 + 390 + 250 + 730 + 220 + 160 - 100 + 340 3 6 240 + 660 + 430 + 270 + 780 + 250 + 210 - 140 + 390 FULL 7 300 + 530 + 430 + 250 + 700 + 230 + 100 - 90 + 300 3 7 700 + 620 + 450 + 270 + 730 + 240 + 120 - 90 + 370 (1) Automatic Landing correction: add 660ft. (2) Weight correction: if CONF FULL, subtract 230ft per 10T below 190T. If CONF 3, subtract 280ft per 10T below 190T. 4 - GOOD TO MEDIUM Corrections on Landing Distance (ft) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF (2) WGT SPD REF DIST Per 10T (ft) for above Per 5kt 190T 190T ALT WIND Per 1000ft above SL Per 5kt TW TEMP SLOPE Per 10°C Per 1% above Down ISA Slope REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 6 070 + 420 + 350 + 210 + 640 + 200 + 220 - 160 + 1 640 3 6 440 + 460 + 360 + 230 + 670 + 210 + 260 - 180 + 1 930 FULL 6 580 + 420 + 350 + 220 + 670 + 200 + 250 - 200 + 290 3 6 990 + 460 + 370 + 230 + 700 + 220 + 290 - 230 + 320 FULL 7 330 + 500 + 430 + 250 + 720 + 240 + 190 - 90 + 300 3 7 740 + 540 + 450 + 260 + 740 + 240 + 220 - 100 + 320 (1) Automatic Landing correction: add 640ft. (2) Weight correction: if CONF FULL, subtract 220ft per 10T below 190T. If CONF 3, subtract 260ft per 10T below 190T. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-D 2/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK 3 - MEDIUM Corrections on Landing Distance (ft) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF (2) WGT SPD REF DIST Per 10T (ft) for above Per 5kt 190T 190T ALT WIND Per 1000ft above SL Per 5kt TW TEMP SLOPE Per 10°C Per 1% above Down ISA Slope REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 6 770 + 480 + 380 + 240 + 760 + 230 + 320 - 220 + 1 540 3 7 210 + 520 + 400 + 260 + 790 + 240 + 370 - 240 + 1 820 FULL 7 230 + 480 + 380 + 250 + 780 + 230 + 340 - 260 + 320 3 7 710 + 520 + 400 + 270 + 810 + 250 + 400 - 300 + 360 FULL 7 650 + 510 + 430 + 260 + 800 + 240 + 320 - 130 + 330 3 8 120 + 550 + 450 + 280 + 830 + 260 + 400 - 170 + 370 (1) Automatic Landing correction: add 660ft. (2) Weight correction: if CONF FULL, subtract 250ft per 10T below 190T. If CONF 3, subtract 300ft per 10T below 190T. 2 - MEDIUM TO POOR Corrections on Landing Distance (ft) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF (2) WGT SPD REF DIST Per 10T (ft) for above Per 5kt 190T 190T ALT WIND Per 1000ft above SL Per 5kt TW TEMP SLOPE Per 10°C Per 1% above Down ISA Slope REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 7 870 + 890 + 590 + 420 + 1 290 + 370 + 520 - 270 + 1 060 3 8 640 + 1 010 + 640 + 470 + 1 410 + 420 + 680 - 320 + 1 270 FULL 8 080 + 890 + 580 + 420 + 1 300 + 380 + 530 - 310 + 500 3 8 870 + 1 020 + 640 + 470 + 1 420 + 430 + 700 - 360 + 580 FULL 8 240 + 900 + 580 + 420 + 1 310 + 380 + 540 - 220 + 490 3 9 050 + 1 020 + 630 + 470 + 1 430 + 430 + 710 - 330 + 550 (1) Automatic Landing correction: if CONF FULL, add 770ft. If CONF 3, add 830ft. (2) Weight correction: if CONF FULL, subtract 360ft per 10T below 190T. If CONF 3, subtract 450ft per 10T below 190T. 1 - POOR Corrections on Landing Distance (ft) Braking Mode Maximum MANUAL AUTOBRAKE MED AUTOBRAKE LOW LDG CONF (2) WGT SPD REF DIST Per 10T (ft) for above Per 5kt 190T 190T ALT WIND Per 1000ft above SL Per 5kt TW TEMP SLOPE Per 10°C Per 1% above Down ISA Slope REV OVW Per Thrust Reverser Operative If OVW PROC applied FULL 12 190 + 940 + 550 + 460 + 1 830 + 430 + 2 500 - 700 + 1 060 3 13 300 + 1 050 + 610 + 500 + 1 910 + 480 + 2 940 - 850 + 1 280 FULL 12 390 + 940 + 550 + 460 + 1 840 + 440 + 2 510 - 730 + 500 3 13 530 + 1 050 + 600 + 500 + 1 920 + 490 + 2 960 - 880 + 580 FULL 12 550 + 940 + 540 + 460 + 1 850 + 440 + 2 520 - 750 + 490 3 13 710 + 1 050 + 600 + 510 + 1 930 + 480 + 2 980 - 910 + 550 (1) Automatic Landing correction: if CONF FULL, add 760ft. If CONF 3, add 810ft. (2) Weight correction: if CONF FULL, subtract 460ft per 10T below 190T. If CONF 3, subtract 550ft per 10T below 190T. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 1/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-24-00015147.0001001 / 28 FEB 14 Applicable to: ALL Ident.: PER-24-00014126.0090001 / 28 FEB 14 Applicable to: ALL 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 (ft) FAILURE DC BUS 1+2 FAULT WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 4 700 + 510 + 310 + 160 + 450 + 150 + 90 INOP + 1 800 3 5 4 980 + 550 + 320 + 180 + 470 + 160 + 90 INOP + 2 040 FULL 0 4 700 + 510 + 310 + 160 + 450 + 150 + 90 - 10 + 1 800 3 5 4 980 + 550 + 320 + 180 + 470 + 160 + 90 - 10 + 2 040 DC ESS BUS FAULT with FULL Ice Accretion 3 10 4 930 + 550 + 290 + 170 + 470 + 160 + 80 - 60 + 1 150 15 5 220 + 580 + 290 + 190 + 470 + 170 + 90 - 70 + 1 380 FULL 10 4 930 + 550 + 290 + 170 + 470 + 160 + 80 - 60 + 1 150 3 15 5 220 + 580 + 290 + 190 + 470 + 170 + 90 - 70 + 1 380 3 5 4 980 + 550 + 320 + 180 + 470 + 160 + 90 INOP + 2 040 REV OVW DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 180ft - (2) Weight correction: subtract 160ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft 5 - GOOD Corrections on Landing Distance (ft) FAILURE DC BUS 1+2 FAULT DC BUS 2 FAULT WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 6 000 + 680 + 530 + 300 + 850 + 280 + 230 INOP + 1 140 3 5 6 560 + 750 + 580 + 340 + 930 + 310 + 290 INOP + 1 310 FULL 0 6 000 + 680 + 530 + 300 + 850 + 280 + 230 - 60 + 1 140 5 6 560 + 750 + 580 + 340 + 930 + 310 + 290 - 100 + 1 310 DC ESS BUS FAULT with FULL Ice Accretion 3 10 6 240 + 640 + 440 + 290 + 780 + 260 + 180 - 140 + 690 15 6 790 + 710 + 470 + 340 + 830 + 290 + 230 - 180 + 820 FULL 10 6 240 + 640 + 440 + 290 + 780 + 260 + 180 - 140 + 690 3 15 6 790 + 710 + 470 + 340 + 830 + 290 + 230 - 180 + 820 3 5 6 560 + 750 + 580 + 340 + 930 + 310 + 290 INOP + 1 310 DC ESS BUS SHED with Ice Accretion EMER CONFIG 3 (1) Automatic Landing correction: add 210ft - (2) Weight correction: subtract 250ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 2/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 6 850 + 450 + 450 + 250 + 720 + 230 + 310 INOP + 1 430 3 5 7 380 + 460 + 470 + 270 + 760 + 250 + 370 INOP + 1 650 FULL 0 6 850 + 450 + 450 + 250 + 720 + 230 + 310 - 220 + 1 430 3 5 7 380 + 460 + 470 + 270 + 760 + 250 + 370 - 280 + 1 650 DC ESS BUS FAULT with FULL Ice Accretion 3 10 6 910 + 430 + 370 + 240 + 680 + 220 + 240 - 220 + 910 15 7 410 + 450 + 380 + 270 + 690 + 240 + 280 - 270 + 1 110 FULL 10 6 910 + 430 + 370 + 240 + 680 + 220 + 240 - 220 + 910 3 15 7 410 + 450 + 380 + 270 + 690 + 240 + 280 - 270 + 1 110 3 5 7 380 + 460 + 470 + 270 + 760 + 250 + 370 INOP + 1 650 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 200ft - (2) Weight correction: subtract 240ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft 3 - MEDIUM Corrections on Landing Distance (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 7 750 + 510 + 490 + 290 + 860 + 270 + 460 INOP + 1 290 3 5 8 390 + 540 + 520 + 310 + 900 + 300 + 550 INOP + 1 510 FULL 0 7 750 + 510 + 490 + 290 + 860 + 270 + 460 - 370 + 1 290 3 5 8 390 + 540 + 520 + 310 + 900 + 300 + 550 - 470 + 1 510 DC ESS BUS FAULT with FULL Ice Accretion 3 10 7 680 + 490 + 400 + 280 + 790 + 260 + 340 - 310 + 830 15 8 280 + 520 + 420 + 300 + 810 + 280 + 400 - 370 + 1 010 FULL 10 7 680 + 490 + 400 + 280 + 790 + 260 + 340 - 310 + 830 3 15 8 280 + 520 + 420 + 300 + 810 + 280 + 400 - 370 + 1 010 3 5 8 390 + 540 + 520 + 310 + 900 + 300 + 550 INOP + 1 510 DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG (1) Automatic Landing correction: add 210ft - (2) Weight correction: subtract 270ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 3/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 9 320 + 1 050 + 790 + 540 + 1 640 + 490 INOP + 600 3 5 10 580 + 1 170 + 880 + 630 + 1 850 + 570 + 1 160 INOP + 720 FULL 0 9 320 + 1 050 + 790 + 540 + 1 640 + 490 - 470 + 600 3 5 10 580 + 1 170 + 880 + 630 + 1 850 + 570 + 1 160 - 680 + 720 DC ESS BUS FAULT with FULL Ice Accretion 3 10 9 170 + 570 + 470 + 1 350 + 420 + 560 - 420 + 420 15 10 210 + 1 030 + 620 + 540 + 1 450 + 480 + 740 - 550 + 520 FULL 10 9 170 + 570 + 470 + 1 350 + 420 + 560 - 420 + 420 3 15 10 210 + 1 030 + 620 + 540 + 1 450 + 480 + 740 - 550 + 520 3 5 10 580 + 1 170 + 880 + 630 + 1 850 + 570 + 1 160 INOP + 720 REV OVW DC BUS 1+2 FAULT DC BUS 2 FAULT DC ESS BUS SHED with Ice Accretion EMER CONFIG + 930 + 930 + 830 + 830 (1) Automatic Landing correction: add 260ft - (2) Weight correction: subtract 420ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft 1 - POOR Corrections on Landing Distance (ft) FAILURE DC BUS 1+2 FAULT DC BUS 2 FAULT WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 Landing Distance greater than 18 000 ft for all conditions 3 5 Landing Distance greater than 18 000 ft for all conditions FULL 0 3 5 15 710 + 880 + 790 + 590 + 2 650 + 630 + 4 190 - 3 370 + 600 Landing Distance greater than 18 000 ft for all conditions DC ESS BUS FAULT with FULL Ice Accretion 3 10 13 460 + 970 + 550 + 510 + 1 870 + 490 + 2 520 - 1 180 + 420 15 14 870 + 1 070 + 590 + 570 + 1 960 + 530 + 2 980 - 1 420 + 520 FULL 10 13 460 + 970 + 550 + 510 + 1 870 + 490 + 2 520 - 1 180 + 420 3 15 14 870 + 1 070 + 590 + 570 + 1 960 + 530 + 2 980 - 1 420 + 520 3 5 DC ESS BUS SHED with Ice Accretion EMER CONFIG Landing Distance greater than 18 000 ft for all conditions (1) Automatic Landing correction: add 260ft - (2) Weight correction: subtract 410ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-24 4/4 05 MAR 14 PER-27 1/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-27-00014128.0108001 / 28 FEB 14 Applicable to: ALL 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 5 470 + 620 N/A + 190 + 470 + 180 + 110 - 70 + 1 870 STAB CTL FAULT with man trim available 3 5 4 750 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 900 L/R/L+R ELEV FAULT 2 20 5 490 + 620 N/A + 190 + 470 + 180 + 110 - 70 + 1 850 RUDDER JAM/ RUDDER FAULT 2 10 5 620 + 830 + 430 + 280 + 610 + 220 + 160 - 80 + 1 910 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 7 080 + 440 N/A + 310 + 620 + 260 + 210 - 220 + 1 130 ALTN/DIRECT LAW 3 5 4 750 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 900 YAW DAMPER FAULT 3 5 4 750 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 900 FULL 0 4 590 + 520 + 290 + 160 + 440 + 150 + 80 - 50 + 1 780 3 5 4 860 + 550 + 300 + 170 + 460 + 160 + 80 - 60 + 2 000 FULL 0 4 690 + 510 + 310 + 160 + 450 + 150 + 80 INOP + 1 820 3 5 4 960 + 540 + 310 + 170 + 470 + 160 + 90 INOP + 2 050 3 5 5 430 + 520 + 410 + 200 + 500 + 180 + 130 INOP + 2 370 FULL 0 4 540 + 520 + 280 + 160 + 440 + 140 + 70 - 50 + 1 740 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 4 810 + 550 + 290 + 170 + 460 + 160 + 80 - 60 + 1 950 FULL 0 4 740 + 500 + 320 + 160 + 440 + 160 + 90 - 60 + 1 830 3 5 5 010 + 540 + 320 + 170 + 460 + 170 + 100 - 70 + 2 070 FULL 0 4 640 + 510 + 300 + 160 + 440 + 150 + 80 - 50 + 1 800 3 5 4 920 + 540 + 300 + 170 + 470 + 160 + 90 - 60 + 2 020 FULL 0 4 740 + 500 + 320 + 160 + 440 + 160 + 90 - 60 + 1 830 3 5 5 010 + 540 + 320 + 170 + 460 + 170 + 100 - 70 + 2 070 FULL 0 4 990 + 490 + 380 + 170 + 460 + 170 + 110 - 80 + 1 980 3 5 5 260 + 520 + 370 + 190 + 480 + 180 + 120 - 90 + 2 230 FULL 0 5 160 + 490 + 420 + 190 + 480 + 180 + 120 - 100 + 2 100 3 5 5 430 + 520 + 410 + 200 + 500 + 180 + 130 - 110 + 2 370 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 70ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 2/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 7 270 + 780 N/A + 360 + 870 + 310 + 270 - 210 + 1 090 STAB CTL FAULT with man trim available 3 5 6 060 + 660 + 460 + 290 + 810 + 260 + 200 - 130 + 1 260 L/R/L+R ELEV FAULT 2 20 7 270 + 770 N/A + 360 + 860 + 310 + 270 - 210 + 1 080 RUDDER JAM/ RUDDER FAULT 2 10 7 450 + 950 + 630 + 460 + 1 090 + 370 + 410 - 250 + 1 050 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 9 340 + 320 N/A + 530 + 1 140 + 440 + 490 - 680 + 440 ALTN/DIRECT LAW 3 5 6 060 + 660 + 460 + 290 + 810 + 260 + 200 - 130 + 1 260 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 6 060 + 660 + 460 + 290 + 810 + 260 + 200 - 130 + 1 260 FULL 0 5 790 + 640 + 480 + 280 + 790 + 250 + 190 - 120 + 1 190 3 5 6 300 + 700 + 510 + 320 + 850 + 290 + 240 - 160 + 1 320 FULL 0 5 970 + 670 + 510 + 300 + 820 + 270 + 210 INOP + 1 190 3 5 6 510 + 740 + 560 + 340 + 890 + 300 + 280 INOP + 1 350 3 5 7 660 + 970 + 870 + 450 + 1 140 + 400 + 520 INOP + 1 630 FULL 0 5 670 + 620 + 450 + 270 + 770 + 250 + 180 - 110 + 1 150 3 5 6 190 + 680 + 480 + 310 + 830 + 270 + 220 - 150 + 1 280 FULL 0 6 080 + 690 + 540 + 300 + 850 + 270 + 230 - 150 + 1 180 3 5 6 630 + 760 + 580 + 340 + 920 + 310 + 290 - 200 + 1 350 FULL 0 5 880 + 660 + 500 + 290 + 810 + 260 + 200 - 130 + 1 180 3 5 6 420 + 720 + 530 + 330 + 880 + 290 + 260 - 170 + 1 320 FULL 0 6 080 + 690 + 540 + 300 + 850 + 270 + 230 - 150 + 1 180 3 5 6 630 + 760 + 580 + 340 + 920 + 310 + 290 - 200 + 1 350 FULL 0 6 640 + 800 + 690 + 360 + 960 + 320 + 330 - 220 + 1 290 3 5 7 220 + 880 + 740 + 400 + 1 040 + 360 + 410 - 270 + 1 490 FULL 0 7 050 + 880 + 820 + 400 + 1 050 + 360 + 410 - 270 + 1 400 3 5 7 660 + 970 + 870 + 450 + 1 140 + 400 + 520 - 340 + 1 630 (1) Automatic Landing correction: add 260ft - (2) Weight correction: subtract 130ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 3/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 7 830 + 460 N/A + 270 + 700 + 250 + 310 - 300 + 1 530 STAB CTL FAULT with man trim available 3 5 6 760 + 430 + 380 + 240 + 680 + 230 + 270 - 230 + 1 580 L/R/L+R ELEV FAULT 2 20 7 830 + 460 N/A + 270 + 690 + 260 + 310 - 300 + 1 520 RUDDER JAM/ RUDDER FAULT 2 10 8 090 + 670 + 530 + 380 + 900 + 310 + 440 - 340 + 1 480 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 9 760 + 170 N/A + 420 + 920 + 360 + 490 - 710 + 840 ALTN/DIRECT LAW 3 5 6 760 + 430 + 380 + 240 + 680 + 230 + 270 - 230 + 1 580 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 6 760 + 430 + 380 + 240 + 680 + 230 + 270 - 230 + 1 580 FULL 0 6 550 + 430 + 400 + 230 + 680 + 220 + 260 - 220 + 1 450 3 5 7 030 + 450 + 420 + 250 + 710 + 240 + 300 - 260 + 1 640 FULL 0 6 750 + 450 + 430 + 250 + 700 + 220 + 280 INOP + 1 460 3 5 7 250 + 470 + 450 + 270 + 730 + 250 + 330 INOP + 1 680 3 5 8 420 + 560 + 680 + 330 + 840 + 310 + 550 INOP + 1 980 FULL 0 6 420 + 420 + 380 + 230 + 670 + 210 + 240 - 210 + 1 420 3 5 6 900 + 440 + 400 + 250 + 700 + 230 + 280 - 240 + 1 600 FULL 0 6 860 + 460 + 450 + 250 + 710 + 230 + 300 - 260 + 1 460 3 5 7 370 + 480 + 470 + 270 + 740 + 250 + 350 - 310 + 1 680 FULL 0 6 650 + 440 + 420 + 240 + 690 + 220 + 270 - 230 + 1 450 3 5 7 150 + 460 + 430 + 260 + 720 + 240 + 320 - 280 + 1 650 FULL 0 6 860 + 460 + 450 + 250 + 710 + 230 + 300 - 260 + 1 460 3 5 7 370 + 480 + 470 + 270 + 740 + 250 + 350 - 310 + 1 680 FULL 0 7 460 + 510 + 570 + 280 + 770 + 270 + 400 - 350 + 1 580 3 5 7 980 + 530 + 580 + 310 + 800 + 280 + 460 - 410 + 1 840 FULL 0 7 890 + 550 + 670 + 310 + 810 + 290 + 480 - 430 + 1 700 3 5 8 420 + 560 + 680 + 330 + 840 + 310 + 550 - 490 + 1 980 (1) Automatic Landing correction: add 240ft - (2) Weight correction: subtract 110ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 4/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 8 790 + 530 N/A + 320 + 820 + 290 + 440 - 410 + 1 400 STAB CTL FAULT with man trim available 3 5 7 570 + 500 + 420 + 280 + 800 + 260 + 380 - 320 + 1 440 L/R/L+R ELEV FAULT 2 20 8 800 + 530 N/A + 320 + 820 + 290 + 440 - 410 + 1 380 RUDDER JAM/ RUDDER FAULT 2 10 9 050 + 770 + 570 + 430 + 1 050 + 350 + 620 - 460 + 1 310 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt 10 810 + 230 N/A + 480 + 1 060 + 410 + 660 - 910 + 720 ALTN/DIRECT LAW 3 5 7 570 + 500 + 420 + 280 + 800 + 260 + 380 - 320 + 1 440 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 7 570 + 500 + 420 + 280 + 800 + 260 + 380 - 320 + 1 440 FULL 0 7 340 + 500 + 440 + 270 + 800 + 250 + 370 - 310 + 1 330 3 5 7 910 + 520 + 460 + 290 + 830 + 270 + 440 - 370 + 1 510 FULL 0 7 570 + 520 + 480 + 280 + 820 + 260 + 410 INOP + 1 330 3 5 8 180 + 540 + 500 + 310 + 860 + 290 + 480 INOP + 1 550 3 5 9 660 + 660 + 770 + 390 + 1 000 + 350 + 810 INOP + 1 840 FULL 0 7 170 + 480 + 420 + 260 + 780 + 240 + 350 - 290 + 1 290 3 5 7 740 + 510 + 440 + 280 + 810 + 270 + 410 - 340 + 1 470 FULL 0 7 710 + 530 + 490 + 290 + 830 + 260 + 430 - 360 + 1 330 3 5 8 320 + 550 + 520 + 320 + 870 + 290 + 510 - 430 + 1 550 FULL 0 7 460 + 510 + 460 + 280 + 810 + 250 + 390 - 330 + 1 320 3 5 8 050 + 530 + 480 + 300 + 850 + 280 + 460 - 390 + 1 510 FULL 0 7 710 + 530 + 490 + 290 + 830 + 260 + 430 - 360 + 1 330 3 5 8 320 + 550 + 520 + 320 + 870 + 290 + 510 - 430 + 1 550 FULL 0 8 460 + 600 + 630 + 330 + 910 + 300 + 570 - 490 + 1 450 3 5 9 100 + 620 + 650 + 360 + 940 + 320 + 670 - 570 + 1 700 FULL 0 9 010 + 640 + 740 + 360 + 960 + 330 + 700 - 600 + 1 570 3 5 9 660 + 660 + 770 + 390 + 1 000 + 350 + 810 - 690 + 1 840 (1) Automatic Landing correction: add 270ft - (2) Weight correction: subtract 150ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27 5/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) FAILURE WGT (2) SPD 2 20 11 250 + 1 130 STAB CTL FAULT with man trim available 3 5 9 190 L/R/L+R ELEV FAULT 2 20 11 240 + 1 130 RUDDER JAM/ RUDDER FAULT 2 10 10 970 + 1 430 + 800 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 ALTN/DIRECT LAW 3 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 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available YAW DAMPER FAULT ALT + 990 N/A + 590 + 1 560 + 530 + 930 - 690 + 680 + 650 + 490 + 1 430 + 450 + 710 - 440 + 760 N/A + 590 + 1 560 + 530 + 930 - 690 + 680 + 710 + 1 820 + 580 + 1 200 - 690 + 570 + 770 + 1 830 + 660 + 1 290 - 1 460 + 260 170kt 13 260 + 720 N/A 5 9 190 + 990 + 650 + 490 + 1 430 + 450 + 710 - 440 + 760 3 5 9 190 + 990 + 650 + 490 + 1 430 + 450 + 710 - 440 + 760 FULL 0 8 760 + 990 + 680 + 480 + 1 420 + 430 + 650 - 400 + 700 3 5 9 780 + 1 090 + 740 + 540 + 1 560 + 490 + 860 - 520 + 810 FULL 0 9 090 + 1 040 + 730 + 510 + 1 490 + 460 + 730 INOP + 700 3 5 10 250 + 1 160 + 810 + 590 + 1 650 + 520 + 1 000 INOP + 830 3 5 13 090 + 1 620 + 1 330 + 840 + 2 240 + 750 + 2 250 INOP + 1 060 FULL 0 8 470 + 640 + 450 + 1 360 + 410 + 590 - 360 + 670 3 5 9 480 + 1 040 + 690 + 520 + 1 490 + 460 + 780 - 480 + 770 FULL 0 9 280 + 1 070 + 750 + 520 + 1 530 + 460 + 780 - 470 + 690 3 5 10 460 + 1 200 + 840 + 600 + 1 690 + 540 + 1 060 - 630 + 830 FULL 0 8 920 + 1 010 + 700 + 490 + 1 450 + 440 + 690 - 420 + 690 + 940 3 5 9 990 + 1 120 + 770 + 560 + 1 600 + 500 + 920 - 560 + 800 FULL 0 9 280 + 1 070 + 750 + 520 + 1 530 + 460 + 780 - 470 + 690 3 5 10 460 + 1 200 + 840 + 600 + 1 690 + 540 + 1 060 - 630 + 830 FULL 0 10 540 + 1 290 + 990 + 640 + 1 800 + 570 + 1 160 - 660 + 770 3 5 11 910 + 1 430 + 1 100 + 730 + 1 990 + 650 + 1 630 - 890 + 940 FULL 0 11 550 + 1 470 + 1 200 + 740 + 2 040 + 650 + 1 570 - 830 + 860 3 5 13 090 + 1 620 + 1 330 + 840 + 2 240 + 750 + 2 250 - 1 130 + 1 060 (1) Automatic Landing correction: add 370ft - (2) Weight correction: subtract 300ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330-243F QUICK REFERENCE HANDBOOK PER-27 6/6 05 MAR 14 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA STAB CTL FAULT with man trim not available 2 20 16 230 + 1 150 STAB CTL FAULT with man trim available 3 5 L/R/L+R ELEV FAULT 2 RUDDER JAM/ RUDDER FAULT + 610 + 2 020 + 580 + 3 410 - 1 660 + 680 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 760 20 16 230 + 1 150 + 620 + 2 020 + 570 + 3 420 - 1 660 + 680 2 10 15 990 + 1 450 + 760 + 730 + 2 260 + 630 + 3 810 - 1 680 + 570 The following ECAM alerts with engine out: -RUDDER JAM -RUDDER FAULT (Calculated with 170kt min) 2 170kt ALTN/DIRECT LAW 3 5 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 760 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 N/A N/A Landing Distance greater than 18 000 ft for all conditions 3 5 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 760 FULL 0 13 460 + 1 020 + 640 + 510 + 1 930 + 490 + 2 910 - 1 290 + 700 3 5 14 830 + 1 110 + 690 + 570 + 2 020 + 530 + 3 430 - 1 530 + 810 FULL 0 13 990 + 1 070 + 680 + 540 + 1 980 + 510 + 3 150 INOP + 700 3 5 Landing Distance greater than 18 000 ft for all conditions 3 5 Landing Distance greater than 18 000 ft for all conditions FULL 0 12 960 + 980 + 600 + 490 + 1 880 + 470 + 2 690 - 1 180 + 670 3 5 14 310 + 1 070 + 650 + 550 + 1 980 + 520 + 3 180 - 1 420 + 770 FULL 0 14 260 + 1 090 + 710 + 550 + 2 000 + 520 + 3 280 - 1 460 + 690 3 5 15 880 + 1 200 + 780 + 620 + 2 120 + 580 + 3 970 - 1 780 + 830 FULL 0 13 710 + 1 040 + 660 + 520 + 1 960 + 490 + 3 020 - 1 340 + 690 3 5 15 140 + 1 140 + 710 + 580 + 2 050 + 550 + 3 590 - 1 600 + 800 FULL 0 14 260 + 1 090 + 710 + 550 + 2 000 + 520 + 3 280 - 1 460 + 690 3 5 15 880 + 1 200 + 780 + 620 + 2 120 + 580 + 3 970 - 1 780 + 830 FULL 0 16 340 + 1 280 + 910 + 640 + 2 180 + 600 + 4 370 - 1 970 + 770 3 5 Landing Distance greater than 18 000 ft for all conditions FULL 0 Landing Distance greater than 18 000 ft for all conditions 3 5 Landing Distance greater than 18 000 ft for all conditions (1) Automatic Landing correction: add 370ft - (2) Weight correction: subtract 400ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 1/6 IN FLIGHT PERFORMANCE A330-243F 30 JUN 15 QUICK REFERENCE HANDBOOK Ident.: PER-27A-00014129.0090001 / 09 APR 15 Applicable to: ALL 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 (ft) FAILURE FLAPS FAULT WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA 0≤FLAPS<1+F 2 30 6 060 + 680 N/A + 210 + 480 + 200 + 140 - 90 + 2 970 1+F≤FLAPS<2 2 15 5 300 + 600 + 310 + 190 + 470 + 170 + 120 - 70 + 2 700 2≤FLAPS<3 2 10 4 960 + 580 + 290 + 180 + 480 + 160 + 90 - 60 + 2 340 FLAPS=3 3 5 4 750 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 900 FLAPS>3 FULL 5 4 710 + 530 + 280 + 170 + 460 + 140 + 70 - 50 + 1 410 0≤SLATS<1 2 30 6 010 + 650 N/A + 210 + 480 + 190 + 120 - 90 + 1 390 1≤SLATS<2 2 15 5 210 + 600 + 300 + 190 + 470 + 170 + 100 - 60 + 2 100 SLATS≥2 3 5 4 780 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 880 NO FLAPS/NO SLATS 1 50 7 200 + 760 N/A + 250 + 510 + 230 + 170 - 130 + 2 090 0≤FLAPS<1+F 1 50 7 200 + 760 N/A + 250 + 510 + 230 + 170 - 130 + 2 090 1+F≤FLAPS<2 2 40 6 700 + 690 N/A + 230 + 500 + 210 + 150 - 120 + 1 630 2 30 6 010 + 650 N/A + 210 + 480 + 190 + 120 - 90 + 1 390 FLAPS=3 2 25 5 770 + 610 N/A + 200 + 470 + 180 + 110 - 90 + 880 FLAPS>3 2 25 5 720 + 590 N/A + 190 + 470 + 180 + 90 - 80 + 370 0≤FLAPS<1+F 2 30 5 970 + 670 N/A + 210 + 480 + 190 + 130 - 90 + 2 930 1+F≤FLAPS<2 2 20 5 570 + 620 N/A + 190 + 470 + 180 + 120 - 80 + 2 480 2 15 5 210 + 600 + 300 + 190 + 470 + 170 + 100 - 60 + 2 100 FLAPS=3 3 10 5 010 + 570 + 280 + 180 + 480 + 150 + 80 - 60 + 1 610 FLAPS>3 SLATS FAULT 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 FULL 10 4 960 + 550 + 290 + 170 + 470 + 150 + 80 - 60 + 1 120 0≤FLAPS<1+F 2 30 5 970 + 670 N/A + 210 + 480 + 190 + 130 - 90 + 2 930 1+F≤FLAPS<2 2 15 5 300 + 600 + 310 + 190 + 470 + 170 + 120 - 70 + 2 700 2≤FLAPS<3 2 10 4 960 + 580 + 290 + 180 + 480 + 160 + 90 - 60 + 2 340 FLAPS=3 3 5 4 780 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 880 FLAPS>3 FULL 0 4 510 + 520 + 270 + 160 + 450 + 140 + 70 - 40 + 1 670 (1) Automatic Landing correction: add 150ft - (2) Weight correction: subtract 150ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 2/6 IN FLIGHT PERFORMANCE A330-243F 30 JUN 15 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 (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA 0≤FLAPS<1+F 2 30 8 390 + 930 N/A + 440 + 990 + 380 + 400 - 300 + 1 730 1+F≤FLAPS<2 2 15 7 130 + 790 + 530 + 380 + 910 + 320 + 320 - 210 + 1 670 2≤FLAPS<3 2 10 6 500 + 710 + 490 + 330 + 860 + 290 + 250 - 160 + 1 530 FLAPS=3 3 5 6 060 + 660 + 460 + 290 + 810 + 260 + 200 - 130 + 1 260 FLAPS>3 FULL 5 5 900 + 620 + 430 + 280 + 770 + 240 + 170 - 120 + 900 0≤SLATS<1 2 30 8 070 + 840 N/A + 400 + 910 + 350 + 300 - 270 + 700 1≤SLATS<2 2 15 6 880 + 740 + 490 + 350 + 860 + 300 + 260 - 180 + 1 300 SLATS≥2 3 5 6 080 + 660 + 460 + 290 + 810 + 270 + 210 - 130 + 1 240 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 10 230 + 1 110 N/A + 550 + 1 110 + 470 + 510 - 450 + 920 0≤FLAPS<1+F 1 50 10 230 + 1 110 N/A + 550 + 1 110 + 470 + 510 - 450 + 920 1+F≤FLAPS<2 2 40 9 340 + 980 N/A + 480 + 1 030 + 420 + 420 - 380 + 690 2 30 8 070 + 840 N/A + 400 + 910 + 350 + 300 - 270 + 700 FLAPS=3 2 25 7 580 + 760 N/A + 360 + 860 + 320 + 240 - 230 + 430 FLAPS>3 2 25 7 340 + 710 N/A + 340 + 810 + 290 + 190 - 200 + 170 0≤FLAPS<1+F 2 30 8 100 + 880 N/A + 420 + 940 + 360 + 360 - 270 + 1 730 1+F≤FLAPS<2 2 20 7 550 + 820 N/A + 380 + 910 + 330 + 330 - 240 + 1 450 2 15 6 880 + 740 + 490 + 350 + 860 + 300 + 260 - 180 + 1 300 FLAPS=3 3 10 6 440 + 680 + 470 + 310 + 830 + 280 + 220 - 160 + 1 000 FLAPS>3 FULL 10 6 270 + 640 + 440 + 290 + 790 + 260 + 180 - 140 + 660 0≤FLAPS<1+F 2 30 8 100 + 880 N/A + 420 + 940 + 360 + 360 - 270 + 1 730 1+F≤FLAPS<2 2 15 7 130 + 790 + 530 + 380 + 910 + 320 + 320 - 210 + 1 670 2≤FLAPS<3 2 10 6 500 + 710 + 490 + 330 + 860 + 290 + 250 - 160 + 1 530 FLAPS=3 3 5 6 080 + 660 + 460 + 290 + 810 + 270 + 210 - 130 + 1 240 FLAPS>3 FULL 0 5 580 + 600 + 430 + 260 + 750 + 230 + 160 - 100 + 1 120 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 170ft - (2) Weight correction: subtract 240ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 3/6 IN FLIGHT PERFORMANCE A330-243F 30 JUN 15 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 (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA 0≤FLAPS<1+F 2 30 8 780 + 490 N/A + 310 + 740 + 280 + 400 - 380 + 2 500 1+F≤FLAPS<2 2 15 7 740 + 470 + 420 + 280 + 720 + 260 + 350 - 310 + 2 230 2≤FLAPS<3 2 10 7 160 + 440 + 390 + 260 + 700 + 240 + 300 - 250 + 1 960 FLAPS=3 3 5 6 760 + 430 + 380 + 240 + 680 + 230 + 270 - 230 + 1 580 FLAPS>3 FULL 5 6 600 + 420 + 360 + 230 + 670 + 210 + 230 - 210 + 1 150 0≤SLATS<1 2 30 8 520 + 480 N/A + 300 + 720 + 270 + 330 - 340 + 1 120 1≤SLATS<2 2 15 7 490 + 450 + 390 + 270 + 700 + 250 + 300 - 270 + 1 750 SLATS≥2 3 5 6 790 + 430 + 380 + 240 + 690 + 220 + 270 - 230 + 1 550 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 10 280 + 530 N/A + 360 + 780 + 340 + 460 - 490 + 1 710 0≤FLAPS<1+F 1 50 10 280 + 530 N/A + 360 + 780 + 340 + 460 - 490 + 1 710 1+F≤FLAPS<2 2 40 9 610 + 510 N/A + 340 + 760 + 320 + 410 - 440 + 1 250 2 30 8 520 + 480 N/A + 300 + 720 + 270 + 330 - 340 + 1 120 FLAPS=3 2 25 8 110 + 470 N/A + 280 + 700 + 260 + 290 - 310 + 670 FLAPS>3 2 25 7 900 + 450 N/A + 270 + 690 + 250 + 240 - 280 + 270 0≤FLAPS<1+F 2 30 8 520 + 480 N/A + 300 + 720 + 280 + 370 - 340 + 2 480 1+F≤FLAPS<2 2 20 8 100 + 470 N/A + 290 + 720 + 260 + 360 - 330 + 2 020 2 15 7 490 + 450 + 390 + 270 + 700 + 250 + 300 - 270 + 1 750 FLAPS=3 3 10 7 110 + 440 + 390 + 250 + 690 + 240 + 270 - 250 + 1 320 FLAPS>3 FULL 10 6 930 + 430 + 370 + 240 + 680 + 230 + 240 - 220 + 890 0≤FLAPS<1+F 2 30 8 520 + 480 N/A + 300 + 720 + 280 + 370 - 340 + 2 480 1+F≤FLAPS<2 2 15 7 740 + 470 + 420 + 280 + 720 + 260 + 350 - 310 + 2 230 2≤FLAPS<3 2 10 7 160 + 440 + 390 + 260 + 700 + 240 + 300 - 250 + 1 960 FLAPS=3 3 5 6 790 + 430 + 380 + 240 + 690 + 220 + 270 - 230 + 1 550 FLAPS>3 FULL 0 6 310 + 410 + 360 + 220 + 660 + 210 + 230 - 190 + 1 370 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 230ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 4/6 IN FLIGHT PERFORMANCE A330-243F 30 JUN 15 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 (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA 0≤FLAPS<1+F 2 30 9 920 + 570 N/A + 360 + 870 + 330 + 580 - 530 + 2 310 1+F≤FLAPS<2 2 15 8 730 + 540 + 470 + 330 + 850 + 300 + 510 - 430 + 2 040 2≤FLAPS<3 2 10 8 060 + 510 + 430 + 300 + 820 + 270 + 430 - 360 + 1 800 FLAPS=3 3 5 7 570 + 500 + 420 + 280 + 800 + 260 + 380 - 320 + 1 440 FLAPS>3 FULL 5 7 340 + 480 + 400 + 260 + 780 + 250 + 330 - 290 + 1 040 0≤SLATS<1 2 30 9 550 + 560 N/A + 340 + 840 + 310 + 470 - 470 + 1 010 1≤SLATS<2 2 15 8 420 + 520 + 430 + 310 + 820 + 290 + 440 - 380 + 1 600 SLATS≥2 3 5 7 600 + 500 + 420 + 280 + 800 + 250 + 380 - 320 + 1 420 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 11 570 + 620 N/A + 420 + 920 + 380 + 650 - 660 + 1 560 0≤FLAPS<1+F 1 50 11 570 + 620 N/A + 420 + 920 + 380 + 650 - 660 + 1 560 1+F≤FLAPS<2 2 40 10 780 + 600 N/A + 390 + 900 + 360 + 580 - 600 + 1 130 2 30 9 550 + 560 N/A + 340 + 840 + 310 + 470 - 470 + 1 010 FLAPS=3 2 25 9 040 + 540 N/A + 320 + 820 + 290 + 410 - 420 + 600 FLAPS>3 2 25 8 740 + 520 N/A + 310 + 800 + 280 + 340 - 370 + 240 0≤FLAPS<1+F 2 30 9 600 + 560 N/A + 350 + 850 + 320 + 530 - 470 + 2 290 1+F≤FLAPS<2 2 20 9 130 + 550 N/A + 330 + 840 + 300 + 520 - 460 + 1 850 2 15 8 420 + 520 + 430 + 310 + 820 + 290 + 440 - 380 + 1 600 FLAPS=3 3 10 7 950 + 510 + 420 + 290 + 810 + 270 + 390 - 340 + 1 200 FLAPS>3 FULL 10 7 710 + 490 + 400 + 280 + 790 + 260 + 340 - 310 + 800 0≤FLAPS<1+F 2 30 9 600 + 560 N/A + 350 + 850 + 320 + 530 - 470 + 2 290 1+F≤FLAPS<2 2 15 8 730 + 540 + 470 + 330 + 850 + 300 + 510 - 430 + 2 040 2≤FLAPS<3 2 10 8 060 + 510 + 430 + 300 + 820 + 270 + 430 - 360 + 1 800 FLAPS=3 3 5 7 600 + 500 + 420 + 280 + 800 + 250 + 380 - 320 + 1 420 FLAPS>3 FULL 0 7 030 + 470 + 400 + 250 + 770 + 240 + 330 - 260 + 1 250 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 (1) Automatic Landing correction: add 170ft - (2) Weight correction: subtract 260ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-27A 5/6 IN FLIGHT PERFORMANCE A330-243F 30 JUN 15 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 (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA 0≤FLAPS<1+F 2 30 13 370 + 1 300 + 710 + 1 760 + 630 + 1 450 - 1 000 + 1 220 1+F≤FLAPS<2 2 15 11 290 + 1 190 + 750 + 630 + 1 660 + 560 + 1 140 - 720 + 1 020 2≤FLAPS<3 2 10 10 160 + 1 090 + 690 + 560 + 1 560 + 500 + 890 - 550 + 920 FLAPS=3 3 5 9 190 + 990 + 650 + 490 + 1 430 + 450 + 710 - 440 + 760 FLAPS>3 FULL 5 8 700 + 910 + 580 + 450 + 1 330 + 410 + 550 - 380 + 530 0≤SLATS<1 2 30 12 320 + 1 170 N/A + 630 + 1 600 + 570 + 990 - 810 + 470 1≤SLATS<2 2 15 10 700 + 1 110 + 680 + 580 + 1 550 + 520 + 910 - 620 + 800 SLATS≥2 3 5 9 220 + 1 000 + 650 + 490 + 1 440 + 440 + 710 - 440 + 730 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 15 760 + 1 390 N/A + 800 + 1 830 + 720 + 1 630 - 1 290 + 800 0≤FLAPS<1+F 1 50 15 760 + 1 390 N/A + 800 + 1 830 + 720 + 1 630 - 1 290 + 800 1+F≤FLAPS<2 2 40 14 230 + 1 300 N/A + 730 + 1 740 + 650 + 1 330 - 1 080 + 520 2 30 12 320 + 1 170 N/A + 630 + 1 600 + 570 + 990 - 810 + 470 FLAPS=3 2 25 11 230 + 1 070 N/A + 560 + 1 470 + 510 + 770 - 660 + 280 FLAPS>3 2 25 10 540 + 980 N/A + 510 + 1 360 + 470 + 580 - 550 + 120 0≤FLAPS<1+F 2 30 12 670 + 1 220 N/A + 660 + 1 660 + 590 + 1 240 - 870 + 1 240 1+F≤FLAPS<2 2 20 11 890 + 1 210 N/A + 640 + 1 660 + 570 + 1 180 - 800 + 910 2 15 10 700 + 1 110 + 680 + 580 + 1 550 + 520 + 910 - 620 + 800 FLAPS=3 3 10 9 730 + 1 010 + 640 + 510 + 1 450 + 460 + 730 - 500 + 610 FLAPS>3 FULL 10 9 190 + 470 + 1 340 + 420 + 560 - 420 + 400 0≤FLAPS<1+F 2 30 12 670 + 1 220 + 660 + 1 660 + 590 + 1 240 - 870 + 1 240 1+F≤FLAPS<2 2 15 11 290 + 1 190 + 750 + 630 + 1 660 + 560 + 1 140 - 720 + 1 020 2≤FLAPS<3 2 10 10 160 + 1 090 + 690 + 560 + 1 560 + 500 + 890 - 550 + 920 FLAPS=3 3 5 9 220 + 1 000 + 650 + 490 + 1 440 + 440 + 710 - 440 + 730 FLAPS>3 FULL 0 8 250 + 430 + 1 310 + 390 + 540 - 330 + 630 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 N/A + 930 + 900 + 570 N/A + 600 (1) Automatic Landing correction: add 210ft - (2) Weight correction: subtract 400ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330-243F QUICK REFERENCE HANDBOOK PER-27A 6/6 30 JUN 15 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 (ft) FAILURE WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA 0≤FLAPS<1+F 2 30 1+F≤FLAPS<2 2 15 16 560 + 1 200 + 710 + 650 + 2 080 + 600 + 3 930 - 1 800 + 1 020 2≤FLAPS<3 2 10 15 140 + 1 110 + 660 + 580 + 2 020 + 550 + 3 430 - 1 530 + 920 FLAPS=3 3 5 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 760 FLAPS>3 FULL 5 13 000 + 960 + 560 + 490 + 1 860 + 470 + 2 520 - 1 140 + 530 0≤SLATS<1 2 30 17 300 + 1 190 N/A + 660 + 2 050 + 620 + 3 460 - 1 780 + 470 1≤SLATS<2 2 15 15 690 + 1 130 + 640 + 610 + 2 020 + 560 + 3 430 - 1 600 + 800 SLATS≥2 3 5 13 870 + 1 030 + 620 + 530 + 1 930 + 500 + 2 970 - 1 320 + 730 NO FLAPS/NO SLATS FLAPS FAULT SLATS FAULT 1 50 Landing Distance greater than 18 000 ft for all conditions 0≤FLAPS<1+F 1 50 Landing Distance greater than 18 000 ft for all conditions 1+F≤FLAPS<2 2 40 Landing Distance greater than 18 000 ft for all conditions 2 30 17 300 + 1 190 N/A + 660 + 2 050 + 620 + 3 460 - 1 780 + 470 FLAPS=3 2 25 15 890 + 1 100 N/A + 600 + 1 970 + 560 + 2 980 - 1 520 + 280 FLAPS>3 2 25 14 840 + 1 020 N/A + 550 + 1 890 + 530 + 2 500 - 1 310 + 120 0≤FLAPS<1+F 2 30 17 850 + 1 230 N/A + 680 + 2 090 + 640 + 3 950 - 1 910 + 1 240 1+F≤FLAPS<2 2 20 17 160 + 1 220 N/A + 660 + 2 080 + 610 + 3 930 - 1 870 + 910 2 15 15 690 + 1 130 + 640 + 610 + 2 020 + 560 + 3 430 - 1 600 + 800 FLAPS=3 3 10 14 390 + 1 050 + 600 + 550 + 1 960 + 520 + 2 990 - 1 370 + 610 FLAPS>3 FULL 10 13 490 + 970 + 550 + 510 + 1 880 + 490 + 2 530 - 1 190 + 400 0≤FLAPS<1+F 2 30 17 850 + 1 230 N/A + 680 + 2 090 + 640 + 3 950 - 1 910 + 1 240 1+F≤FLAPS<2 2 15 16 560 + 1 200 + 710 + 650 + 2 080 + 600 + 3 930 - 1 800 + 1 020 2≤FLAPS<3 2 10 15 140 + 1 110 + 660 + 580 + 2 020 + 550 + 3 430 - 1 530 + 920 FLAPS=3 3 5 13 870 + 1 030 + 620 + 530 + 1 930 + 500 + 2 970 - 1 320 + 730 FLAPS>3 FULL 0 12 560 + 940 + 470 + 1 850 + 450 + 2 510 - 1 100 + 630 0≤SLATS<1 2≤FLAPS<3 1≤SLATS<2 2≤FLAPS<3 SLATS≥2 Landing Distance greater than 18 000 ft for all conditions + 560 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 480ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-28 1/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-28-00014138.0090001 / 28 FEB 14 Applicable to: ALL 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 4 930 + 550 + 290 + 170 + 470 + 160 + 80 - 60 + 1 150 3 15 5 220 + 580 + 290 + 190 + 470 + 170 + 90 - 70 + 1 380 REV OVW (1) Automatic Landing correction: add 120ft - (2) Weight correction: subtract 160ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft 5 - GOOD Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 6 240 + 640 + 440 + 290 + 780 + 260 + 180 - 140 + 690 3 15 6 790 + 710 + 470 + 340 + 830 + 290 + 230 - 180 + 820 REV OVW (1) Automatic Landing correction: add 140ft - (2) Weight correction: subtract 250ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft 4 - GOOD TO MEDIUM Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 6 910 + 430 + 370 + 240 + 680 + 220 + 240 - 220 + 910 3 15 7 410 + 450 + 380 + 270 + 690 + 240 + 280 - 270 + 1 110 (1) Automatic Landing correction: add 130ft - (2) Weight correction: subtract 240ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-28 2/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 7 680 + 490 + 400 + 280 + 790 + 260 + 340 - 310 + 830 3 15 8 280 + 520 + 420 + 300 + 810 + 280 + 400 - 370 + 1 010 REV OVW (1) Automatic Landing correction: add 140ft - (2) Weight correction: subtract 270ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft 2 - MEDIUM TO POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 9 170 + 570 + 470 + 1 350 + 420 + 560 - 420 + 420 3 15 10 210 + 1 030 + 620 + 540 + 1 450 + 480 + 740 - 550 + 520 REV OVW + 930 (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 420ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft 1 - POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 13 460 + 970 + 550 + 510 + 1 870 + 490 + 2 520 - 1 180 + 420 3 15 14 870 + 1 070 + 590 + 570 + 1 960 + 530 + 2 980 - 1 420 + 520 (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 510ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 1/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-29-00014130.0090001 / 28 FEB 14 Applicable to: ALL 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 (ft) FAILURE G SYS LO PR WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 4 900 + 450 + 290 + 160 + 450 + 140 + 90 - 70 + 1 730 3 5 5 200 + 480 + 300 + 170 + 460 + 160 + 100 - 80 + 1 960 FULL 0 4 640 + 510 + 300 + 160 + 440 + 150 + 80 0 + 1 800 3 5 4 920 + 540 + 300 + 170 + 470 + 160 + 90 - 10 + 2 020 FULL 0 4 540 + 520 + 290 + 150 + 440 + 150 + 70 0 + 1 740 3 5 4 820 + 550 + 290 + 170 + 470 + 150 + 80 - 10 + 1 950 B SYS LO PR with G SYS FULL 0 / 140kt 6 340 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 6 700 min) + 660 + 440 + 230 + 630 + 210 + 230 - 130 + 1 650 + 740 + 450 + 240 + 640 + 230 + 270 - 180 + 1 910 Y SYS LO PR with G SYS FULL 0 / 140kt 5 250 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 5 500 min) + 420 + 350 + 180 + 480 + 160 + 120 - 50 + 1 780 + 460 + 350 + 190 + 490 + 180 + 130 - 60 + 2 030 B SYS LO PR Y SYS LO PR G+Y G+B B+Y 0≤FLAPS<1+F 2 30 6 630 + 590 N/A + 220 + 490 + 200 + 170 - 50 + 3 160 1+F≤FLAPS<2 2 20 6 330 + 510 N/A + 210 + 490 + 200 + 180 - 50 + 2 640 2≤FLAPS<3 2 20 6 240 + 520 N/A + 210 + 490 + 190 + 150 - 50 + 2 030 FLAPS=3 3 15 6 090 + 470 + 370 + 210 + 500 + 190 + 150 - 40 + 1 500 FLAPS>3 FULL 10 5 770 + 450 + 370 + 200 + 500 + 180 + 130 - 30 + 1 240 SLATS<1 2 30 8 470 + 910 N/A + 300 + 670 + 270 + 320 - 210 + 1 400 1≤SLATS<2 2 25 8 080 + 900 N/A + 280 + 660 + 260 + 310 - 180 + 1 630 SLATS≥2 3 15 7 440 + 750 + 450 + 270 + 660 + 240 + 290 - 150 + 1 410 2 20 5 780 + 610 N/A + 200 + 480 + 180 + 130 INOP + 2 130 (1) Automatic Landing correction: add 180ft - (2) Weight correction: subtract 10ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 2/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 6 150 + 650 + 490 + 300 + 850 + 270 + 230 - 160 + 1 050 3 5 6 750 + 730 + 530 + 340 + 930 + 300 + 290 - 200 + 1 200 FULL 0 5 880 + 660 + 500 + 290 + 810 + 260 + 200 - 30 + 1 180 3 5 6 420 + 720 + 530 + 330 + 880 + 290 + 260 - 60 + 1 320 FULL 0 5 680 + 620 + 450 + 270 + 770 + 240 + 180 - 20 + 1 160 3 5 6 200 + 680 + 490 + 310 + 840 + 270 + 220 - 50 + 1 290 B SYS LO PR with G SYS FULL 0 / 140kt 6 740 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 7 240 min) + 810 + 570 + 320 + 910 + 290 + 300 - 210 + 1 200 + 900 + 610 + 360 + 970 + 320 + 380 - 240 + 1 400 Y SYS LO PR with G SYS FULL 0 / 140kt 6 810 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 7 360 min) + 740 + 610 + 350 + 970 + 310 + 320 - 260 + 1 090 + 840 + 660 + 390 + 1 050 + 350 + 400 - 310 + 1 270 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 9 610 + 1 090 N/A + 530 + 1 180 + 460 + 620 - 320 + 1 800 1+F≤FLAPS<2 2 20 9 070 + 1 040 N/A + 500 + 1 150 + 430 + 600 - 300 + 1 480 2≤FLAPS<3 2 20 8 800 + 990 N/A + 470 + 1 110 + 410 + 500 - 260 + 1 110 FLAPS=3 3 15 8 350 + 910 + 670 + 460 + 1 080 + 390 + 450 - 230 + 840 FLAPS>3 FULL 10 7 640 + 820 + 630 + 400 + 1 020 + 350 + 350 - 160 + 680 SLATS<1 2 30 9 620 + 1 130 N/A + 490 + 1 090 + 420 + 510 - 290 + 810 1≤SLATS<2 2 25 9 100 + 1 090 N/A + 460 + 1 050 + 400 + 480 - 250 + 1 010 SLATS≥2 3 15 8 170 + 970 + 630 + 420 + 1 000 + 360 + 420 - 180 + 930 2 20 8 140 + 930 N/A + 430 + 1 000 + 380 + 410 INOP + 1 230 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 10ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 3/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 6 480 + 430 + 390 + 230 + 680 + 210 + 250 - 210 + 1 410 3 5 6 970 + 450 + 410 + 250 + 700 + 240 + 290 - 250 + 1 620 FULL 0 6 650 + 440 + 420 + 240 + 690 + 220 + 270 - 100 + 1 450 3 5 7 150 + 460 + 430 + 260 + 720 + 240 + 320 - 140 + 1 650 FULL 0 6 420 + 420 + 380 + 230 + 670 + 220 + 240 - 80 + 1 420 3 5 6 910 + 440 + 400 + 250 + 700 + 230 + 290 - 110 + 1 610 B SYS LO PR with G SYS FULL 0 / 140kt 7 110 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 7 550 min) + 520 + 480 + 260 + 730 + 240 + 330 - 260 + 1 510 + 550 + 500 + 280 + 750 + 260 + 380 - 280 + 1 760 Y SYS LO PR with G SYS FULL 0 / 140kt 7 090 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 7 530 min) + 460 + 480 + 260 + 730 + 240 + 320 - 250 + 1 460 + 490 + 490 + 280 + 750 + 260 + 370 - 280 + 1 700 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 9 190 + 510 N/A + 330 + 760 + 310 + 470 - 270 + 2 710 1+F≤FLAPS<2 2 20 8 840 + 520 N/A + 320 + 770 + 290 + 480 - 270 + 2 220 2≤FLAPS<3 2 20 8 630 + 510 N/A + 310 + 750 + 280 + 420 - 240 + 1 690 FLAPS=3 3 15 8 340 + 510 + 500 + 320 + 760 + 280 + 400 - 230 + 1 230 FLAPS>3 FULL 10 7 790 + 490 + 490 + 290 + 760 + 270 + 340 - 170 + 1 000 SLATS<1 2 30 9 540 + 620 N/A + 350 + 790 + 310 + 450 - 320 + 1 280 1≤SLATS<2 2 25 9 100 + 610 N/A + 330 + 770 + 300 + 440 - 280 + 1 500 SLATS≥2 3 15 8 360 + 570 + 510 + 310 + 760 + 290 + 410 - 230 + 1 290 2 20 8 670 + 510 N/A + 320 + 760 + 290 + 420 INOP + 1 710 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 10ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 4/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 7 240 + 490 + 430 + 260 + 790 + 240 + 360 - 300 + 1 290 3 5 7 840 + 520 + 450 + 290 + 830 + 260 + 420 - 350 + 1 490 FULL 0 7 460 + 510 + 460 + 280 + 810 + 250 + 390 - 160 + 1 320 3 5 8 050 + 530 + 480 + 300 + 850 + 280 + 460 - 210 + 1 510 FULL 0 7 180 + 480 + 420 + 260 + 780 + 240 + 350 - 130 + 1 300 3 5 7 760 + 510 + 440 + 280 + 820 + 270 + 410 - 180 + 1 470 B SYS LO PR with G SYS FULL 0 / 140kt 7 990 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 8 540 min) + 540 + 530 + 300 + 860 + 280 + 470 - 360 + 1 360 + 570 + 550 + 320 + 890 + 300 + 550 - 410 + 1 610 Y SYS LO PR with G SYS FULL 0 / 140kt 7 980 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 8 520 min) + 540 + 530 + 300 + 860 + 280 + 460 - 360 + 1 330 + 570 + 550 + 320 + 880 + 300 + 540 - 410 + 1 570 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 10 440 + 610 N/A + 390 + 910 + 360 + 680 - 410 + 2 520 1+F≤FLAPS<2 2 20 10 060 + 610 N/A + 380 + 910 + 340 + 690 - 410 + 2 040 2≤FLAPS<3 2 20 9 790 + 600 N/A + 360 + 890 + 330 + 600 - 370 + 1 550 FLAPS=3 3 15 9 420 + 600 + 560 + 360 + 900 + 330 + 570 - 340 + 1 130 FLAPS>3 FULL 10 8 750 + 570 + 540 + 330 + 880 + 310 + 490 - 260 + 900 SLATS<1 2 30 10 780 + 630 N/A + 400 + 930 + 360 + 650 - 470 + 1 160 1≤SLATS<2 2 25 10 300 + 610 N/A + 380 + 910 + 340 + 630 - 420 + 1 360 SLATS≥2 3 15 9 440 + 600 + 560 + 360 + 900 + 320 + 580 - 340 + 1 170 2 20 9 850 + 600 N/A + 370 + 900 + 330 + 620 INOP + 1 570 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 20ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-29 5/6 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 8 560 + 640 + 460 + 1 370 + 410 + 610 - 370 + 660 3 5 9 650 + 1 070 + 710 + 530 + 1 530 + 480 + 820 - 500 + 790 FULL 0 8 920 + 1 010 + 700 + 490 + 1 450 + 440 + 690 - 210 + 690 3 5 9 990 + 1 120 + 770 + 560 + 1 600 + 500 + 920 - 340 + 800 FULL 0 8 490 + 640 + 450 + 1 360 + 410 + 590 - 170 + 670 3 5 + 950 + 940 9 510 + 1 050 + 700 + 520 + 1 500 + 470 + 790 - 280 + 780 B SYS LO PR with G SYS FULL 0 / 140kt 9 700 + 1 110 + 810 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 10 820 + 1 250 + 890 min) + 550 + 1 600 + 490 + 860 - 680 + 690 + 630 + 1 770 + 560 + 1 180 - 860 + 840 Y SYS LO PR with G SYS FULL 0 / 140kt 9 720 + 1 110 + 820 supplied by the RAT (Calculated with 140kt 3 5 / 140kt 10 840 + 1 260 + 900 min) + 550 + 1 610 + 500 - 680 + 690 + 640 + 1 770 + 570 + 1 180 - 870 + 840 G+Y G+B B+Y + 870 0≤FLAPS<1+F 2 30 14 490 + 1 440 N/A + 800 + 1 930 + 720 + 1 890 - 1 090 + 1 450 1+F≤FLAPS<2 2 20 13 820 + 1 460 N/A + 790 + 1 970 + 700 + 1 900 - 1 030 + 1 040 2≤FLAPS<3 2 20 13 200 + 1 380 N/A + 740 + 1 870 + 660 + 1 530 - 880 + 780 FLAPS=3 3 15 12 200 + 1 310 + 870 + 700 + 1 800 + 610 + 1 280 - 710 + 590 FLAPS>3 FULL 10 10 830 + 1 170 + 790 + 600 + 1 650 + 540 - 460 + 470 SLATS<1 2 30 14 590 + 1 430 N/A + 790 + 1 920 + 710 + 1 640 - 1 120 + 550 1≤SLATS<2 2 25 13 880 + 1 400 N/A + 770 + 1 890 + 680 + 1 580 - 1 000 + 660 SLATS≥2 3 15 12 170 + 1 300 + 860 + 690 + 1 790 + 610 + 1 270 - 710 + 590 2 20 13 300 + 1 390 + 740 + 1 890 + 670 + 1 570 INOP + 790 N/A + 920 (1) Automatic Landing correction: add 240ft - (2) Weight correction: subtract 120ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330-243F QUICK REFERENCE HANDBOOK PER-29 6/6 05 MAR 14 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 (ft) FAILURE G SYS LO PR B SYS LO PR Y SYS LO PR WGT FLAPS LEVER ΔVREF for LDG (2) SPD ALT WIND TEMP SLOPE REV OVW REF Per Per Per Per 1% Per Thrust If OVW DIST 10T 1000ft Per 10°C Per 5kt Down Reverser PROC (ft) for above above 5kt TW above Slope Operative applied 190T 190T SL ISA FULL 0 13 090 + 990 + 600 + 500 + 1 900 + 470 + 2 750 - 1 210 + 660 3 5 14 600 + 1 090 + 670 + 560 + 2 000 + 530 + 3 320 - 1 480 + 790 FULL 0 13 710 + 1 040 + 660 + 520 + 1 960 + 490 + 3 020 - 750 + 690 3 5 15 140 + 1 140 + 710 + 580 + 2 050 + 550 + 3 590 - 1 000 + 800 FULL 0 12 990 + 980 + 600 + 490 + 1 890 + 470 + 2 700 - 620 + 670 3 5 14 370 + 1 070 + 650 + 550 + 1 980 + 520 + 3 210 - 840 + 780 B SYS LO PR with G SYS FULL 0 / 140kt 14 870 + 1 120 + 760 + 570 + 2 050 + 550 + 3 520 - 950 supplied by the RAT (Calculated with 140kt 3 5 / 140kt Landing Distance greater than 18 000 ft for all conditions min) + 690 Y SYS LO PR with G SYS FULL 0 / 140kt 14 940 + 1 130 + 770 + 580 + 2 060 + 550 + 3 550 - 980 supplied by the RAT (Calculated with 140kt 3 5 / 140kt Landing Distance greater than 18 000 ft for all conditions min) + 690 G+Y G+B B+Y 0≤FLAPS<1+F 2 30 Landing Distance greater than 18 000 ft for all conditions 1+F≤FLAPS<2 2 20 Landing Distance greater than 18 000 ft for all conditions 2≤FLAPS<3 2 20 Landing Distance greater than 18 000 ft for all conditions FLAPS=3 3 15 Landing Distance greater than 18 000 ft for all conditions FLAPS>3 FULL 10 Landing Distance greater than 18 000 ft for all conditions SLATS<1 2 30 Landing Distance greater than 18 000 ft for all conditions 1≤SLATS<2 2 25 Landing Distance greater than 18 000 ft for all conditions SLATS≥2 3 15 Landing Distance greater than 18 000 ft for all conditions 2 20 Landing Distance greater than 18 000 ft for all conditions (1) Automatic Landing correction: add 230ft - (2) Weight correction: subtract 210ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-30 1/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-30-00014132.0090001 / 28 FEB 14 Applicable to: ALL 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 (ft) 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 (ft) 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 4 930 + 550 + 290 + 170 + 470 + 160 + 80 - 60 + 1 150 15 5 220 + 580 + 290 + 190 + 470 + 170 + 90 - 70 + 1 380 REV OVW (1) Automatic Landing correction: add 120ft - (2) Weight correction: subtract 160ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft 5 - GOOD Corrections on Landing Distance (ft) 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 (ft) 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 6 240 + 640 + 440 + 290 + 780 + 260 + 180 - 140 + 690 15 6 790 + 710 + 470 + 340 + 830 + 290 + 230 - 180 + 820 REV OVW (1) Automatic Landing correction: add 140ft - (2) Weight correction: subtract 250ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft 4 - GOOD TO MEDIUM Corrections on Landing Distance (ft) 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 (ft) 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 6 910 + 430 + 370 + 240 + 680 + 220 + 240 - 220 + 910 15 7 410 + 450 + 380 + 270 + 690 + 240 + 280 - 270 + 1 110 (1) Automatic Landing correction: add 130ft - (2) Weight correction: subtract 240ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-30 2/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) 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 7 680 + 490 + 400 + 280 + 790 + 260 + 340 - 310 + 830 15 8 280 + 520 + 420 + 300 + 810 + 280 + 400 - 370 + 1 010 REV OVW (1) Automatic Landing correction: add 140ft - (2) Weight correction: subtract 270ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft 2 - MEDIUM TO POOR Corrections on Landing Distance (ft) 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 (ft) 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 9 170 + 570 + 470 + 1 350 + 420 + 560 - 420 + 420 15 10 210 + 1 030 + 620 + 540 + 1 450 + 480 + 740 - 550 + 520 REV OVW + 930 (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 420ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft 1 - POOR Corrections on Landing Distance (ft) 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 (ft) 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 13 460 + 970 + 550 + 510 + 1 870 + 490 + 2 520 - 1 180 + 420 15 14 870 + 1 070 + 590 + 570 + 1 960 + 530 + 2 980 - 1 420 + 520 (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 510ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 1/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-32-00014133.0090001 / 28 FEB 14 Applicable to: ALL 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 5 750 + 730 + 330 + 200 + 590 + 180 + 190 - 130 + 1 750 3 5 6 170 + 790 + 350 + 210 + 610 + 200 + 220 - 160 + 1 950 FULL 0 4 730 + 570 + 290 + 170 + 500 + 150 + 90 - 60 + 1 620 3 5 5 020 + 600 + 310 + 180 + 510 + 170 + 110 - 70 + 1 830 FULL 0 5 050 + 630 + 320 + 190 + 550 + 170 + 120 - 80 + 1 550 3 5 5 410 + 680 + 340 + 200 + 560 + 190 + 140 - 100 + 1 770 REV OVW (1) Automatic Landing correction: add 180ft - (2) Weight correction: subtract 160ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft 5 - GOOD Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 6 060 + 710 + 420 + 260 + 760 + 230 + 220 - 140 + 1 200 3 5 6 570 + 770 + 450 + 300 + 820 + 260 + 270 - 170 + 1 320 FULL 0 5 870 + 640 + 450 + 280 + 800 + 250 + 190 - 130 + 1 060 3 5 6 420 + 710 + 480 + 320 + 870 + 280 + 250 - 170 + 1 180 FULL 0 6 270 + 700 + 470 + 300 + 880 + 270 + 240 - 170 + 980 3 5 6 870 + 770 + 510 + 340 + 950 + 310 + 300 - 210 + 1 090 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 250ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 2/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 6 290 + 560 + 360 + 220 + 650 + 210 + 230 - 190 + 1 490 3 5 6 770 + 590 + 380 + 240 + 680 + 220 + 270 - 230 + 1 680 FULL 0 6 690 + 440 + 380 + 240 + 720 + 220 + 280 - 230 + 1 330 3 5 7 220 + 470 + 400 + 260 + 750 + 240 + 330 - 280 + 1 500 FULL 0 7 190 + 490 + 400 + 260 + 790 + 240 + 360 - 290 + 1 250 3 5 7 780 + 510 + 430 + 290 + 830 + 260 + 420 - 340 + 1 420 REV OVW (1) Automatic Landing correction: add 190ft - (2) Weight correction: subtract 230ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft 3 - MEDIUM Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 7 010 + 470 + 400 + 250 + 760 + 240 + 330 - 270 + 1 340 3 5 7 580 + 500 + 420 + 280 + 800 + 250 + 390 - 320 + 1 520 FULL 0 7 460 + 510 + 420 + 270 + 840 + 260 + 400 - 320 + 1 200 3 5 8 090 + 540 + 440 + 300 + 880 + 270 + 470 - 380 + 1 370 FULL 0 8 030 + 560 + 440 + 300 + 940 + 270 + 510 - 380 + 1 120 3 5 8 720 + 590 + 470 + 330 + 980 + 300 + 600 - 460 + 1 280 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 260ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 3/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 8 220 + 900 + 600 + 430 + 1 310 + 390 + 540 - 330 + 670 3 5 9 190 + 990 + 650 + 490 + 1 430 + 440 + 710 - 440 + 770 FULL 0 8 670 + 950 + 610 + 450 + 1 400 + 410 + 630 - 390 + 600 3 5 9 700 + 1 060 + 660 + 520 + 1 530 + 460 + 820 - 510 + 700 FULL 0 9 210 + 1 010 + 620 + 480 + 1 500 + 430 + 750 - 460 + 550 3 5 10 310 + 1 130 + 690 + 550 + 1 650 + 490 + 980 - 590 + 640 REV OVW (1) Automatic Landing correction: add 220ft - (2) Weight correction: subtract 400ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft 1 - POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 0 12 530 + 940 + 570 + 470 + 1 840 + 450 + 2 510 - 1 100 + 670 3 5 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 770 FULL 0 13 250 + 1 000 + 580 + 490 + 2 000 + 480 + 3 230 - 1 240 + 600 3 5 14 680 + 1 100 + 620 + 550 + 2 110 + 520 + 3 820 - 1 490 + 700 FULL 0 14 120 + 1 070 + 630 + 560 + 2 420 + 550 + 3 230 - 1 430 + 550 3 5 15 670 + 1 170 + 700 + 620 + 2 550 + 610 + 3 820 - 1 710 + 640 (1) Automatic Landing correction: add 220ft - (2) Weight correction: subtract 480ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-32 4/4 05 MAR 14 PER-34 1/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-34-00014134.0107001 / 28 FEB 14 Applicable to: ALL 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 4 750 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 900 ALL ADR OFF 3 N/A 5 220 + 580 + 290 + 190 + 470 + 170 + 90 - 70 + 1 380 ADR/IR DISAGREE 3 5 4 750 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 900 REV OVW (1) Automatic Landing correction: add 120ft - (2) Weight correction: subtract 160ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft 5 - GOOD Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 6 060 + 660 + 460 + 290 + 810 + 260 + 200 - 130 + 1 260 ALL ADR OFF 3 N/A 6 790 + 710 + 470 + 340 + 830 + 290 + 230 - 180 + 820 ADR/IR DISAGREE 3 5 6 060 + 660 + 460 + 290 + 810 + 260 + 200 - 130 + 1 260 REV OVW (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 260ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft 4 - GOOD TO MEDIUM Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 6 760 + 430 + 380 + 240 + 680 + 230 + 270 - 230 + 1 580 ALL ADR OFF 3 N/A 7 410 + 450 + 380 + 270 + 690 + 240 + 280 - 270 + 1 110 ADR/IR DISAGREE 3 5 6 760 + 430 + 380 + 240 + 680 + 230 + 270 - 230 + 1 580 (1) Automatic Landing correction: add 150ft - (2) Weight correction: subtract 240ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-34 2/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 7 570 + 500 + 420 + 280 + 800 + 260 + 380 - 320 + 1 440 ALL ADR OFF 3 N/A 8 280 + 520 + 420 + 300 + 810 + 280 + 400 - 370 + 1 010 ADR/IR DISAGREE 3 5 7 570 + 500 + 420 + 280 + 800 + 260 + 380 - 320 + 1 440 REV OVW (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 280ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft 2 - MEDIUM TO POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 ALL ADR OFF 3 N/A ADR/IR DISAGREE 3 5 9 190 + 990 + 650 + 490 + 1 430 + 450 + 710 - 440 + 760 10 210 + 1 030 + 620 + 540 + 1 450 + 480 + 740 - 550 + 520 9 190 + 490 + 1 430 + 450 + 710 - 440 + 760 REV OVW + 990 + 650 (1) Automatic Landing correction: add 210ft - (2) Weight correction: subtract 440ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft 1 - POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA DOUBLE ADR/IR FAULT 3 5 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 760 ALL ADR OFF 3 N/A 14 870 + 1 070 + 590 + 570 + 1 960 + 530 + 2 980 - 1 420 + 520 ADR/IR DISAGREE 3 5 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 760 (1) Automatic Landing correction: add 200ft - (2) Weight correction: subtract 520ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-36 1/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-36-00014137.0090001 / 28 FEB 14 Applicable to: ALL 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 4 930 + 550 + 290 + 170 + 470 + 160 + 80 - 60 + 1 150 3 15 5 220 + 580 + 290 + 190 + 470 + 170 + 90 - 70 + 1 380 REV OVW (1) Automatic Landing correction: add 120ft - (2) Weight correction: subtract 160ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft 5 - GOOD Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 6 240 + 640 + 440 + 290 + 780 + 260 + 180 - 140 + 690 3 15 6 790 + 710 + 470 + 340 + 830 + 290 + 230 - 180 + 820 REV OVW (1) Automatic Landing correction: add 140ft - (2) Weight correction: subtract 250ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft 4 - GOOD TO MEDIUM Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 6 910 + 430 + 370 + 240 + 680 + 220 + 240 - 220 + 910 3 15 7 410 + 450 + 380 + 270 + 690 + 240 + 280 - 270 + 1 110 (1) Automatic Landing correction: add 130ft - (2) Weight correction: subtract 240ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-36 2/2 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 7 680 + 490 + 400 + 280 + 790 + 260 + 340 - 310 + 830 3 15 8 280 + 520 + 420 + 300 + 810 + 280 + 400 - 370 + 1 010 REV OVW (1) Automatic Landing correction: add 140ft - (2) Weight correction: subtract 270ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft 2 - MEDIUM TO POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 9 170 + 570 + 470 + 1 350 + 420 + 560 - 420 + 420 3 15 10 210 + 1 030 + 620 + 540 + 1 450 + 480 + 740 - 550 + 520 REV OVW + 930 (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 420ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft 1 - POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA FULL 10 13 460 + 970 + 550 + 510 + 1 870 + 490 + 2 520 - 1 180 + 420 3 15 14 870 + 1 070 + 590 + 570 + 1 960 + 530 + 2 980 - 1 420 + 520 (1) Automatic Landing correction: add 160ft - (2) Weight correction: subtract 510ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 1/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK Ident.: PER-70-00014135.0093001 / 28 FEB 14 Applicable to: ALL 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 4 840 + 550 + 300 + 170 + 460 + 150 + 80 - 60 + 2 030 SHUTDOWN with damage but no Ice Accretion 3 5 4 840 + 550 + 300 + 170 + 460 + 150 + 80 - 60 + 2 030 SHUTDOWN with damage and Ice Accretion 3 15 5 340 + 570 + 310 + 190 + 470 + 170 + 100 - 80 + 1 550 THR LEVER FAULT/ DISAGREE 3 5 4 760 + 550 + 280 + 170 + 470 + 150 + 80 - 10 + 1 900 REV UNLOCKED with buffet 2 25 5 740 + 630 N/A + 200 + 480 + 180 + 110 - 80 + 1 630 REV UNLOCKED without buffet 3 5 4 750 + 550 + 280 + 170 + 470 + 150 + 80 - 50 + 1 900 REV OVW (1) Automatic Landing correction: add 130ft - (2) Weight correction: subtract 160ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 4 340ft 5 - GOOD Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 6 270 + 720 + 530 + 320 + 860 + 290 + 250 - 170 + 1 310 SHUTDOWN with damage but no Ice Accretion 3 5 6 270 + 720 + 530 + 320 + 860 + 290 + 250 - 170 + 1 310 SHUTDOWN with damage and Ice Accretion 3 15 7 100 + 780 + 540 + 370 + 890 + 320 + 270 - 240 + 880 THR LEVER FAULT/ DISAGREE 3 5 6 070 + 660 + 470 + 300 + 820 + 270 + 210 - 50 + 1 250 REV UNLOCKED with buffet 2 25 7 670 + 810 N/A + 380 + 890 + 330 + 280 - 240 + 880 REV UNLOCKED without buffet 3 5 6 060 + 660 + 460 + 290 + 810 + 260 + 200 - 130 + 1 260 (1) Automatic Landing correction: add 180ft - (2) Weight correction: subtract 260ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 5 320ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 2/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 6 980 + 460 + 430 + 260 + 700 + 240 + 300 - 280 + 1 650 SHUTDOWN with damage but no Ice Accretion 3 5 6 980 + 460 + 430 + 260 + 700 + 240 + 300 - 280 + 1 650 SHUTDOWN with damage and Ice Accretion 3 15 7 710 + 480 + 440 + 290 + 710 + 260 + 320 - 340 + 1 220 THR LEVER FAULT/ DISAGREE 3 5 6 810 + 430 + 390 + 240 + 690 + 230 + 280 - 150 + 1 570 REV UNLOCKED with buffet 2 25 8 170 + 470 N/A + 290 + 710 + 260 + 320 - 320 + 1 320 REV UNLOCKED without buffet 3 5 6 760 + 430 + 380 + 240 + 680 + 230 + 270 - 230 + 1 580 REV OVW (1) Automatic Landing correction: add 170ft - (2) Weight correction: subtract 240ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 070ft 3 - MEDIUM Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 7 840 + 540 + 480 + 290 + 820 + 280 + 440 - 390 + 1 510 SHUTDOWN with damage but no Ice Accretion 3 5 7 840 + 540 + 480 + 290 + 820 + 280 + 440 - 390 + 1 510 SHUTDOWN with damage and Ice Accretion 3 15 8 650 + 560 + 480 + 330 + 830 + 300 + 460 - 470 + 1 100 THR LEVER FAULT/ DISAGREE 3 5 7 660 + 490 + 420 + 280 + 820 + 260 + 410 - 250 + 1 440 REV UNLOCKED with buffet 2 25 9 170 + 550 N/A + 330 + 830 + 300 + 460 - 440 + 1 200 REV UNLOCKED without buffet 3 5 7 570 + 500 + 420 + 280 + 800 + 260 + 380 - 320 + 1 440 (1) Automatic Landing correction: add 180ft - (2) Weight correction: subtract 280ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 6 770ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 3/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 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 (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 9 690 + 1 120 + 770 + 550 + 1 550 + 490 + 880 - 580 + 750 SHUTDOWN with damage but no Ice Accretion 3 5 9 690 + 1 120 + 770 + 550 + 1 550 + 490 + 880 - 580 + 750 SHUTDOWN with damage and Ice Accretion 3 15 10 890 + 1 160 + 730 + 600 + 1 580 + 530 + 930 - 780 + 530 THR LEVER FAULT/ DISAGREE 3 5 9 320 + 1 010 + 680 + 510 + 1 510 + 460 + 760 - 350 + 720 REV UNLOCKED with buffet 2 25 11 780 + 1 150 N/A + 610 + 1 570 + 550 + 960 - 750 + 570 REV UNLOCKED without buffet 3 5 9 190 + 650 + 490 + 1 430 + 450 + 710 - 440 + 760 REV OVW + 990 (1) Automatic Landing correction: add 240ft - (2) Weight correction: subtract 440ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 7 870ft 1 - POOR Corrections on Landing Distance (ft) 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 (ft) for above above 5kt TW above Slope Operative applied LDG 190T 190T SL ISA SHUTDOWN with no damage 3 5 14 460 + 1 170 + 740 + 580 + 1 930 + 550 + 3 100 - 1 700 + 750 SHUTDOWN with damage but no Ice Accretion 3 5 14 460 + 1 170 + 740 + 580 + 1 930 + 550 + 3 100 - 1 700 + 750 SHUTDOWN with damage and Ice Accretion 3 15 15 660 + 1 210 + 700 + 630 + 1 960 + 590 + 3 130 - 1 890 + 530 THR LEVER FAULT/ DISAGREE 3 5 14 620 + 970 + 630 + 530 + 2 110 + 520 + 3 900 - 1 720 + 720 REV UNLOCKED with buffet 2 25 16 770 + 1 170 N/A + 630 + 2 040 + 600 + 3 440 - 1 720 + 570 REV UNLOCKED without buffet 3 5 13 850 + 1 030 + 610 + 530 + 1 940 + 500 + 2 970 - 1 320 + 760 (1) Automatic Landing correction: add 230ft - (2) Weight correction: subtract 490ft per 10T below 190T REF DIST without failure (valid for all FLAPS LEVER positions) = 12 190ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-70 4/4 05 MAR 14 A330-243F PER-E 1/4 IN FLIGHT PERFORMANCE 05 MAR 14 QUICK REFERENCE HANDBOOK CEILINGS Ident.: PER-E-00010707.0021001 / 11 FEB 11 Applicable to: ALL 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 -900 ft -1 600 ft GREEN DOT -400 ft -1 100 ft TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-E 2/4 05 MAR 14 GROSS FLIGHT PATH DESCENT AT GREEN DOT SPEED Ident.: PER-E-00010708.0024001 / 11 FEB 11 Applicable to: ALL ONE ENGINE OUT TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK CRUISE AT LONG RANGE CRUISE SPEED Ident.: PER-E-00010709.0024001 / 11 FEB 11 Applicable to: ALL ONE ENGINE OUT TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-E 3/4 05 MAR 14 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK IN CRUISE QUICK CHECK LONG RANGE Ident.: PER-E-00010710.0024001 / 16 MAR 11 Applicable to: ALL ONE ENGINE OUT TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-E 4/4 05 MAR 14 PER-G 1/4 IN FLIGHT PERFORMANCE A330-243F 05 MAR 14 QUICK REFERENCE HANDBOOK OPTIMUM & MAXIMUM ALTITUDES Ident.: PER-G-00010713.0001001 / 01 OCT 12 Applicable to: ALL ALL ENGINES CORRECTIONS ENGINE ANTI ICE ON TOTAL ANTI ICE ON PACK FLOW HI OR/AND CARGO COOL ON ≤ ISA + 7 -300 ft -500 ft -200 ft ISA + 15 -400 ft -900 ft -200 ft ISA + 20 -800 ft -1 900 ft -400 ft Note: No bleed corrections on optimum altitudes. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-G 2/4 05 MAR 14 IN CRUISE QUICK CHECK AT A GIVEN MACH NUMBER Ident.: PER-G-00010714.0022001 / 11 FEB 11 Applicable to: ALL ALL ENGINES TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-G 3/4 05 MAR 14 COST INDEX FOR LONG RANGE CRUISE SPEED Ident.: PER-G-00010715.0005001 / 08 FEB 13 Applicable to: ALL 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. STANDARD DESCENT Ident.: PER-G-00010716.0026001 / 11 FEB 11 Applicable to: ALL ALL ENGINES TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330-243F QUICK REFERENCE HANDBOOK QUICK DETERMINATION TABLE OF ALTERNATE FLIGHT PLANNING Ident.: PER-G-00010717.0022001 / 11 FEB 11 Applicable to: ALL ALL ENGINES TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-G 4/4 05 MAR 14 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-H 1/2 05 MAR 14 IN CRUISE QUICK CHECK FL 100 LONG RANGE Ident.: PER-H-00010718.0022001 / 11 FEB 11 Applicable to: ALL FLIGHT WITHOUT CAB PRESS TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-H 2/2 05 MAR 14 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK PER-I 1/6 05 MAR 14 GROUND DISTANCE / AIR DISTANCE CONVERSION Ident.: PER-I-00010719.0001001 / 01 OCT 12 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE IN FLIGHT PERFORMANCE A330-243F QUICK REFERENCE HANDBOOK IAS / MACH CONVERSION Ident.: PER-I-00010720.0001001 / 01 OCT 12 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 2/6 05 MAR 14 IN FLIGHT PERFORMANCE A330-243F QUICK REFERENCE HANDBOOK ISA TEMPERATURE AND PRESSURE ALTITUDE CORRECTION Ident.: PER-I-00015042.0001001 / 28 FEB 14 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 3/6 05 MAR 14 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 4/6 05 MAR 14 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK WIND COMPONENT Ident.: PER-I-00014336.0001001 / 16 MAY 12 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 5/6 05 MAR 14 A330-243F IN FLIGHT PERFORMANCE QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE PER-I 6/6 05 MAR 14 A330-243F QUICK REFERENCE HANDBOOK OPERATIONAL DATA TABLE OF CONTENTS OPS 1/2 06 DEC 16 Aircraft Configuration Summary..................................................... OPS.00A Severe Turbulence ........................................................................ OPS.01A Hydraulic Architecture.....................................................................OPS.02A Flight Controls Architecture............................................................ OPS.03A Required Equipment for CAT2 and CAT3...................................... OPS.04A TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK OPERATIONAL DATA TABLE OF CONTENTS Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS 2/2 06 DEC 16 OPS.00A OPERATIONAL DATA A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK AIRCRAFT CONFIGURATION SUMMARY Ident.: OPS-ACS-00017240.0001001 / 08 SEP 15 Applicable to: ALL For awareness and for the specified aircraft, the following table provides the flight crew with a list of optional aircraft systems and functions related to aircraft flight operations. Ident.: OPS-ACS-00017251.0001001 / 08 SEP 15 Applicable to: ALL Item System Installed SURV No AUTO FLT No AUTO FLT No AUTO FLT Yes NAV Yes DATALINK Yes AUTO FLT No AUTO FLT Yes AUTO FLT No NAV Yes NAV Yes AUTO FLT Yes Ident.: OPS-ACS-00017128.0001001 / 08 SEP 15 Applicable to: ALL ADS-B OUT Ident.: OPS-ACS-00017127.0001001 / 08 SEP 15 Applicable to: ALL AP / FD TCAS Ident.: OPS-ACS-00017126.0002001 / 14 OCT 15 Applicable to: ALL AP Automatic Disconnection at Minima Ident.: OPS-ACS-00017132.0002001 / 08 SEP 15 Applicable to: ALL Automatic FD Bar Engagement at Go-Around Ident.: OPS-ACS-00017133.0002001 / 08 SEP 15 Applicable to: ALL BUSS Ident.: OPS-ACS-00017134.0002001 / 08 SEP 15 Applicable to: ALL CPDLC Ident.: OPS-ACS-00017144.0001001 / 08 SEP 15 Applicable to: ALL FLS Function in the FMS Ident.: OPS-ACS-00017145.0010001 / 08 SEP 15 Applicable to: ALL FMS 2 Release 1A Ident.: OPS-ACS-00017153.0001001 / 08 SEP 15 Applicable to: ALL GLS Ident.: OPS-ACS-00017155.0002001 / 08 SEP 15 Applicable to: ALL GPS Ident.: OPS-ACS-00017156.0002001 / 08 SEP 15 Applicable to: ALL GPS PRIMARY Function Ident.: OPS-ACS-00017157.0002001 / 08 SEP 15 Applicable to: ALL NAV Mode Automatically Engaged (Armed) at Go-Around TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F OPS.00B OPERATIONAL DATA 06 DEC 16 QUICK REFERENCE HANDBOOK Ident.: OPS-ACS-00017159.0002001 / 08 SEP 15 Applicable to: ALL PWS SURV Yes NAV Yes SURV No AUTO FLT Yes SURV No ENG No Ident.: OPS-ACS-00017176.0002001 / 08 SEP 15 Applicable to: ALL QFE BARO Setting Ident.: OPS-ACS-00019771.0001001 / 10 MAY 16 Applicable to: ALL RAAS Ident.: OPS-ACS-00017177.0002001 / 08 SEP 15 Applicable to: ALL RNP AR Ident.: OPS-ACS-00017178.0001001 / 08 SEP 15 Applicable to: ALL ROW / ROPS Ident.: OPS-ACS-00017189.0001001 / 22 MAR 16 Applicable to: ALL Soft Go-Around Function TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.01A OPERATIONAL DATA A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK SEVERE TURBULENCE Ident.: OPS-00012057.0021001 / 23 NOV 16 Applicable to: ALL Speed and Thrust Setting (N1) for Turbulence Speed FL SPD or Mach 120 GROSS WEIGHT (1 000 kg) 130 140 150 160 170 180 190 200 210 220 230 240 410 0.8 72.5 73.4 74.5 75.5 76.7 78.0 79.9 82.3 - - - - - 390 0.8 71.6 72.3 73.0 74.0 75.0 76.0 77.1 78.5 80.4 82.6 - - - 370 0.8 70.8 71.4 72.0 72.7 73.4 74.4 75.3 76.3 77.3 78.6 80.4 82.4 - 350 260 69.4 69.9 70.4 71.1 71.8 72.6 73.4 74.3 75.3 76.4 77.5 79.0 80.7 330 260 68.2 68.7 69.3 69.9 70.6 71.3 72.1 72.9 73.8 74.7 75.8 77.1 78.4 310 260 66.9 67.4 68.0 68.6 69.3 70.0 70.7 71.5 72.3 73.2 74.1 75.1 76.3 290 260 65.6 66.1 66.7 67.3 67.8 68.5 69.1 69.9 70.6 71.5 72.3 73.2 74.2 270 260 64.4 64.9 65.4 66.0 66.6 67.2 67.8 68.5 69.1 69.9 70.6 71.5 72.4 250 260 63.1 63.6 64.1 64.6 65.2 65.8 66.5 67.2 67.9 68.6 69.4 70.2 71.0 200 240 57.8 58.4 59.1 59.7 60.4 61.2 62.0 62.9 63.6 64.4 65.3 66.2 67.2 150 240 54.8 55.3 55.9 56.5 57.2 57.9 58.7 59.4 60.2 61.0 61.8 62.8 63.7 100 240 52.4 52.9 53.3 53.8 54.4 55.0 55.6 56.3 57.0 57.7 58.5 59.3 60.1 50 240 50.7 51.2 51.7 52.1 52.5 53.0 53.5 54.0 54.5 55.1 55.7 56.4 57.1 SEAT BELTS...........................................................................................................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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OPERATIONAL DATA A330-243F QUICK REFERENCE HANDBOOK HYDRAULIC ARCHITECTURE Ident.: OPS-00010722.0012001 / 27 AUG 14 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.02A 06 DEC 16 OPERATIONAL DATA A330-243F QUICK REFERENCE HANDBOOK FLIGHT CONTROLS ARCHITECTURE Ident.: OPS-00010723.0004001 / 29 JUN 16 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.03A 06 DEC 16 OPS.04A OPERATIONAL DATA A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK REQUIRED EQUIPMENT FOR CAT2 AND CAT3 Ident.: OPS-00012527.0008001 / 23 DEC 14 Applicable to: ALL 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 1 (displayed on both sides) 2 2 2 2 2 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 BSCU CHANNEL CAPABILITY RADIO ALTIMETERS ILS RECEIVER GLS  (2) RECEIVER (for GLS  approach) ATTITUDE INDICATION (PFD 1/PFD2) ADR /IR BEAM EXCESSIVE DEVIATION TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OPS.04B OPERATIONAL DATA A330-243F 06 DEC 16 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↓ NOT FMGS MONITORED FOR FMA LDG CAPABILITY WINDSHIELD HEAT (L or R windshield) 1 for PF WINDSHIELD WIPERS OR RAIN REPELLENT (if activated) 1 for PF ND AUTO CALLOUT FUNCTION ATTITUDE INDICATION (STBY) 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. TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F OPERATIONAL DATA QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 06 DEC 16 A330-243F QUICK REFERENCE HANDBOOK Identification OEB49 Issue 2 OPERATIONS ENGINEERING BULLETINS LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN Abnormal V Alpha Prot ECAM Entry None Applicable to: ALL Title TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OEBPROC 1/2 18 JAN 17 A330-243F QUICK REFERENCE HANDBOOK OPERATIONS ENGINEERING BULLETINS LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE OEBPROC 2/2 18 JAN 17 A330-243F OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK 49.01A 11 MAY 15 RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB – RED OEB ABNORMAL V ALPHA PROT Ident.: OEBPROC-49-00015964.0001001 / 11 MAY 15 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 TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F OPERATIONS ENGINEERING BULLETINS QUICK REFERENCE HANDBOOK Intentionally left blank TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE BLANK 11 MAY 15 C2 ABNORMAL AND EMERGENCY PROCEDURES A330-243F QUICK REFERENCE HANDBOOK 06 MAR 17 EMER LANDING ALL ENG FAILURE 1 Ident.: 00014256.0001001 / 06 MAR 17 Applicable to: ALL Apply the following if not able to maintain altitude after the loss of thrust near the ground. DITCHING FORCED LANDING APU............................................ START APU............................................ START LAND RECOVERY...........................ON LAND RECOVERY...........................ON LANDING GEAR...............................UP FLAPS LEVER.....................................2 FLAPS LEVER.....................................2 VAPP.................................DETERMINE VAPP.................................DETERMINE GW 120 t 140 t 160 t 180 t 200 t 220 t 240 t VAPP 150 kt 150 kt 153 kt 160 kt 167 kt 173 kt 180 kt DITCHING pb................................... ON SPLRS............................................ARM At 500 ft AGL or below: BRACE FOR IMPACT...............ORDER For flare: TOUCH DOWN AT MIN V/S TARGET PITCH ATT 11 ° At touchdown: ALL ENG MASTERS...................... OFF APU MASTER SW..........................OFF EMER EVAC PROC...................APPLY At 1 000 ft AGL at the latest: LANDING GEAR...... DOWN by GRVTY At 500 ft AGL or below: BRACE FOR IMPACT...............ORDER For flare: TOUCH DOWN AT MIN V/S At touchdown: ALL ENG MASTERS...................... OFF APU MASTER SW..........................OFF EMER EVAC PROC...................APPLY EMERGENCY EVACUATION Ident.: 00010643.0003001 / 08 FEB 13 Applicable to: ALL AIRCRAFT/PARKING BRK.......................................................................... STOP/ON ATC (VHF 1)....................................................................................................NOTIFY CABIN OCCUPANTS (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 occupants about the emergency encountered and the intentions. Press the EVAC COMMAND pb  . ALL BATs......................................................................................................... OFF TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F QUICK REFERENCE HANDBOOK ABNORMAL AND EMERGENCY PROCEDURES C2 06 MAR 17 EMERGENCY EVACUATION (Cont'd)  If evacuation not required: CABIN OCCUPANTS (PA).........................................................................NOTIFY TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE C3 NORMAL PROCEDURES A330-243F 06 DEC 16 QUICK REFERENCE HANDBOOK BEFORE START APPROACH Ident.: 00010684.0002001 / 22 MAR 11 Applicable to: ALL Ident.: 00010692.0001001 / 17 JUN 14 Applicable to: ALL COCKPIT PREP..................... COMPLETED (BOTH) GEAR PINS and COVERS.......................REMOVED SIGNS.........................................................ON/AUTO ADIRS..................................................................NAV FUEL QUANTITY................................... _____KG.LB TO DATA............................................................. SET BARO REF................................... _____SET (BOTH) WINDOWS/DOORS........................CLOSED (BOTH) CABIN........................................................SECURED 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.: 00010686.0002001 / 19 AUG 10 Applicable to: ALL ANTI ICE.................................................... AS RQRD ECAM STATUS.........................................CHECKED PITCH TRIM........................................._____CHECK RUDDER TRIM.................................................ZERO BEFORE TAKEOFF Ident.: 00010687.0002001 / 11 JUL 16 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 CABIN READY  SPLRS ARM FLAPS TO ‐ AUTO BRK MAX ‐ TO CONFIG NORM TAKEOFF RWY............._____CONFIRMED (BOTH) CABIN OCCUPANTS ................................ ADVISED TCAS.................................................. TA OR TA/RA ENGINE START SEL.................................AS RQRD PACKS....................................................... AS RQRD AFTER TAKEOFF / CLIMB Ident.: 00010689.0001001 / 19 AUG 10 Applicable to: ALL LDG GEAR............................................................ UP FLAPS...................................................RETRACTED PACKS...................................................................ON BARO REF................................... _____SET (BOTH) LANDING Ident.: 00010694.0002001 / 11 JUL 16 Applicable to: ALL CABIN OCCUPANTS..................................ADVISED A/THR..................................................... SPEED/OFF AUTOBRAKE............................................. AS RQRD ECAM MEMO.....................................LDG NO BLUE ‐ SIGNS ON ‐ CABIN READY  ‐ LDG GEAR DN ‐ FLAPS LDG ‐ SPLRS ARM AFTER LANDING Ident.: 00010695.0002001 / 22 APR 16 Applicable to: ALL FLAPS...................................................RETRACTED SPOILERS............................................... DISARMED APU................................................................. START RADAR................................................................ OFF PREDICTIVE WINDSHEAR SYSTEM................ OFF PARKING Ident.: 00010696.0001001 / 19 AUG 10 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 / 14 OCT 13 Applicable to: ALL ADIRS.................................................................. OFF OXYGEN..............................................................OFF APU BLEED ....................................................... OFF EMER EXIT LT....................................................OFF SIGNS..................................................................OFF APU AND BAT.................................................... OFF Consider COLD WEATHER TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE A330-243F NORMAL PROCEDURES QUICK REFERENCE HANDBOOK TAKEOFF CG / TRIM POS Ident.: 00012519.0005001 / 14 MAR 12 Applicable to: ALL TPA A330-243F FLEET AS PER AIRCRAFT ALLOCATION TABLE C3 06 DEC 16

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