A330/A340
FLIGHT CREW
OPERATING MANUAL
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© AIRBUS 2005. All rights reserved.
REFERENCE: CAL A330/A340 FLEET FCOM
ISSUE DATE: 30 JUN 15
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A330/A340
FLIGHT CREW
OPERATING MANUAL
Issue date: 30 JUN 15
This is the FLIGHT CREW OPERATING MANUAL at issue date 30 JUN 15 for the A330/A340 and
replacing last issue dated 18 MAR 15
CAL A330/A340 FLEET
FCOM
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30 JUN 15
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A330/A340
FLIGHT CREW
OPERATING MANUAL
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FCOM
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30 JUN 15
FILING INSTRUCTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
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FCOM
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FLIGHT CREW
OPERATING MANUAL
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FLIGHT CREW
OPERATING MANUAL
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A340 Controls and Indicators (CFM)
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FLIGHT CREW
OPERATING MANUAL
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FLIGHT CREW
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No Operations Engineering Bulletin impacting FCOM
CAL A330/A340 FLEET
FCOM
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30 JUN 15
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LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN
A330/A340
FLIGHT CREW
OPERATING MANUAL
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A330/A340
FLIGHT CREW
OPERATING MANUAL
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CAL A330/A340 FLEET
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Subsection Title
Rev. Date
LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETIN
30 JUN 15
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
30 JUN 15
LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS
30 JUN 15
General Information
30 JUN 15
LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS
30 JUN 15
Introduction
18 MAR 15
General Arrangement
18 FEB 14
General
18 FEB 14
Main Components
28 NOV 12
Temperature and Flow Regulation
18 MAR 15
System Operation under Failure Condition
18 FEB 14
Controls and Indicators
18 MAR 15
Warnings and Cautions
18 FEB 14
Electrical Supply
18 FEB 14
General
18 FEB 14
Main Components
18 FEB 14
System Operation
18 FEB 14
Controls and Indicators
18 FEB 14
Warnings and Cautions
18 FEB 14
Electrical Supply
07 APR 11
General
18 FEB 14
Avionics Ventilation
18 FEB 14
Avionics Ground Cooling
18 MAR 15
Battery Ventilation
07 APR 11
Lavatory and Galley Ventilation
25 NOV 11
Pack Bay Ventilation
07 APR 11
Controls and Indicators
18 MAR 15
Warnings and Cautions
20 JAN 15
Electrical Supply
18 FEB 14
General
07 APR 11
System Operation
28 NOV 12
Controls and Indicators
28 NOV 12
Warnings and Cautions
18 FEB 14
Electrical Supply
18 FEB 14
Description
18 FEB 14
System Interface Diagram
15 FEB 13
FMGES Modes of Operation
15 FEB 13
Management of the Displays
20 AUG 10
MCDU
18 FEB 14
FCU
15 FEB 13
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FLIGHT CREW
OPERATING MANUAL
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CAL A330/A340 FLEET
FCOM
Subsection Title
Thrust Levers
Primary Flight Display
Navigation Display
Warnings and Cautions
ELECTRICAL SUPPLY
General
General
Position Computation
Evaluation of Position Accuracy
Radio Navigation Tuning
Alignment of Inertial Reference System
Navigation Database
General
General
FMS2 Honeywell
General
FMS2 Honeywell
Optimization
Cost Index (CI)
Predictions
FMS2 Honeywell
FMS2 Honeywell
MCDU - Data Format List
Effect of Baro Reference Setting
Procedures
Clear Key (Clearing Function)
Engine Out
Secondary Flight Plan
Pilots/Stored Route Function
Time Marker
Step Alts
Time Constraint
Report Page
Diversion
Navigation
Polar Navigation
Navigation Procedures with Failures
MCDU Back Up Navigation
AOC Functions
Rev. Date
30 MAY 12
15 FEB 13
15 FEB 13
18 MAR 15
18 FEB 14
07 APR 11
07 APR 11
18 FEB 14
18 MAR 15
15 FEB 13
18 MAR 15
18 MAR 15
20 AUG 10
28 NOV 12
30 MAY 13
18 MAR 15
28 NOV 12
18 MAR 15
20 AUG 10
18 FEB 14
30 JUN 15
20 JAN 15
07 APR 11
28 NOV 12
07 APR 11
07 APR 11
18 FEB 14
07 APR 11
07 APR 11
28 NOV 12
28 NOV 12
28 NOV 12
30 MAY 12
07 APR 11
20 JAN 15
20 JAN 15
07 APR 11
20 JAN 15
15 FEB 13
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FLIGHT CREW
OPERATING MANUAL
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CAL A330/A340 FLEET
FCOM
Subsection Title
Print Functions
General
Flight Director
Autopilot (AP)
Speed/Mach Control
AP/FD Modes General
AP/FD Lateral Modes
Principles
Climb Mode
Open Climb Mode
Descent Mode
Open Descent Mode
Altitude Acquire Mode
Altitude Hold Mode
Vertical Speed Mode - Flight Path Angle Mode
Mode Reversions
General
Takeoff
General
Precision Approach
Non Precision Approach
Go Around (GA)
Autothrust
Flight Mode Annunciator (FMA)
General
Acquisition/Monitoring
Characteristic Speeds Computation
Weight and Center of Gravity Computation
AFT CG Monitoring
Windshear Detection
Auto Flight - AOC Functions
Auto Flight - Print Interface
General
VHF/HF/SELCAL
Radio Tuning
Electrical Supply
General
Controls
Interphone Systems
Rev. Date
07 APR 11
15 FEB 13
18 FEB 14
18 FEB 14
20 JAN 15
20 AUG 10
15 FEB 13
20 AUG 10
28 NOV 12
15 FEB 13
15 FEB 13
15 FEB 13
20 AUG 10
15 FEB 13
28 NOV 12
15 FEB 13
15 FEB 13
18 FEB 14
08 FEB 12
27 JUN 14
30 JUN 15
28 NOV 12
18 FEB 14
30 JUN 15
07 APR 11
15 FEB 13
07 APR 11
07 APR 11
15 FEB 13
15 FEB 13
28 NOV 12
07 APR 11
07 APR 11
18 FEB 14
18 FEB 14
20 JAN 15
18 FEB 14
18 FEB 14
18 FEB 14
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FLIGHT CREW
OPERATING MANUAL
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CAL A330/A340 FLEET
FCOM
Subsection Title
Rev. Date
Call Systems
20 JAN 15
Passenger Address
28 NOV 12
Emer EVAC
18 FEB 14
Landscape Camera
28 NOV 12
Electrical Supply
07 APR 11
DESCRIPTION
18 MAR 15
CONTROLS AND INDICATORS ON OVERHEAD PANEL
18 MAR 15
ELECTRICAL SUPPLY
18 FEB 14
Emergency Locator Transmitter
30 MAY 13
ACARS Functions
15 FEB 13
General
30 JUN 15
Controls and Indicators
30 JUN 15
Electrical supply
30 MAY 13
Onboard Mobile Telephony System
20 JAN 15
Warnings and Cautions
20 JAN 15
General
27 JUN 14
AC Generation
18 FEB 14
DC Generation
05 MAR 14
Contactors
18 FEB 14
Circuit Breakers
07 APR 11
General
18 FEB 14
Normal Configuration
18 FEB 14
Abnormal Configuration
18 FEB 14
Distribution Table
18 FEB 14
Controls and Indicators
30 JUN 15
Warnings and Cautions
18 FEB 14
General
18 FEB 14
Cockpit Plan
18 FEB 14
Seats
28 NOV 12
Cockpit Window
28 NOV 12
Pilot's Instrument Panels
18 FEB 14
Pedestal
18 FEB 14
Overhead Panel
18 FEB 14
Foot Warmer
25 NOV 11
Electrical Supply
18 FEB 14
Description
18 FEB 14
Cockpit Door Locking System (CDLS)
18 FEB 14
Cockpit Door Surveillance System (CDSS)
18 FEB 14
Electrical Supply
07 APR 11
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FLIGHT CREW
OPERATING MANUAL
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CAL A330/A340 FLEET
FCOM
Subsection Title
Rev. Date
Flight Crew Rest Compartment (If Installed)
18 FEB 14
Lower Deck Mobile Crew Rest Compartment (LDMCR)
07 APR 11
General
20 JAN 15
General
20 JAN 15
Controls and Indicators
20 JAN 15
Electrical Supply
20 JAN 15
Video Control Center (VCC) (If Installed)
20 JAN 15
In-Flight Entertainment Center (IFEC) (If Installed)
20 JAN 15
Introduction
20 JAN 15
Controls and Indicators
20 JAN 15
Description
30 MAY 12
General
28 NOV 12
Description
18 FEB 14
Controls and Indicators
18 FEB 14
Warnings and Cautions
18 FEB 14
Electrical Supply
18 FEB 14
Description
28 NOV 12
Controls And Indicators
07 APR 11
WARNINGS AND CAUTIONS
18 FEB 14
Electrical Supply
28 NOV 12
Description
28 NOV 12
Warnings and Cautions
18 FEB 14
Electrical Supply
20 JAN 15
Smoke Detection
18 FEB 14
Fire Extinguishing
18 FEB 14
Controls and Indicators
28 NOV 12
Warnings and Cautions
18 FEB 14
Electrical Supply
28 NOV 12
Smoke Detection
20 JAN 15
Controls and Indicators
30 JUN 15
Warnings and Cautions
20 JAN 15
Smoke Detection
18 FEB 14
Fire Extinguishing
07 APR 11
Warnings and Cautions
18 FEB 14
Electrical Supply
18 FEB 14
Smoke Detection
20 JAN 15
Warnings and Cautions
20 JAN 15
General
27 JUN 14
Architecture
27 JUN 14
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FLIGHT CREW
OPERATING MANUAL
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CAL A330/A340 FLEET
FCOM
Subsection Title
General
Pitch Control
Lateral Control
Maneuver Load Alleviation (MLA)
Turbulence Damping Function
General
Alternate Law
Direct Law
Abnormal Attitude Laws
Mechanical Back Up
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
General
Tanks
Fuel Control and Monitoring System (FCMS)
Fuel Quantity Indication and Level Sensing
Engine Feed
Fuel Feed Sequence
Automatic Fuel Transfers
Manual Fuel Transfers
CG Control - Trim Tank Transfer
APU Feed
Refueling - Defueling
Jettison
Fuel Recirculation System
Controls and Indicators
Warnings and Cautions
Electrical Supply
General
Generation
Distribution
Controls and Indicators
Electrical Supply
Description
Rev. Date
18 FEB 14
18 MAR 15
18 FEB 14
07 APR 11
07 APR 11
30 MAY 12
18 FEB 14
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
20 JAN 15
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
27 JUN 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
28 NOV 12
07 APR 11
05 MAR 14
18 FEB 14
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
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30 JUN 15
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A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
R
R
R
R
Continued from the previous page
Localization
DSC-30-20-10
DSC-30-20-20
DSC-30-20-30
DSC-30-20-40
DSC-30-30-10
DSC-30-30-20
DSC-30-30-30
DSC-30-30-40
DSC-30-40-10
DSC-30-40-20
DSC-30-40-30
DSC-30-40-40
DSC-30-50-10
DSC-30-50-20
DSC-30-50-30
DSC-30-50-40
DSC-30-55-10
DSC-30-55-20
DSC-30-55-30
DSC-30-60-10
DSC-30-60-20
DSC-30-60-30
DSC-30-70-10
DSC-30-70-20
DSC-30-70-30
DSC-31-05-10
DSC-31-05-20
DSC-31-05-30
DSC-31-05-40
DSC-31-05-50
DSC-31-05-60
DSC-31-10
DSC-31-15
DSC-31-20
DSC-31-25-10
DSC-31-25-20
DSC-31-27
DSC-31-30
DSC-31-40
CAL A330/A340 FLEET
FCOM
Subsection Title
Description
Control and Indicators
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
DESCRIPTION
SYSTEM OPERATION
ELECTRICAL SUPPLY
DESCRIPTION
CONTROLS AND INDICATORS
ELECTRICAL SUPPLY
Description
Warnings and Cautions
Electrical Supply
Introduction
Cockpit Arrangement
Architecture
Controls and Switching
Reconfiguring the DMC
Reconfiguring the DUS
ECAM Description
Indications on E/WD
Indications on SD
GENERAL
EXAMPLE
OEB Reminder
ECAM Controls
Indications on PFD
Rev. Date
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
20 AUG 10
20 AUG 10
18 FEB 14
28 NOV 12
28 NOV 12
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
07 APR 11
07 APR 11
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
30 JUN 15
30 JUN 15
07 APR 11
18 FEB 14
26 JUL 11
18 MAR 15
30 JUN 15
Continued on the following page
PLP-LESS P 7/16
30 JUN 15
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A330/A340
FLIGHT CREW
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R
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Localization
DSC-31-45
DSC-31-50
DSC-31-55-10
DSC-31-55-20
DSC-31-60-10
DSC-31-60-20
DSC-31-60-30
DSC-31-75
DSC-31-80
DSC-32-10-10
DSC-32-10-20
DSC-32-10-30
DSC-32-10-40
DSC-32-10-50
DSC-32-20-10
DSC-32-20-20
DSC-32-20-30
DSC-32-20-40
DSC-32-30-10
DSC-32-30-20
DSC-32-30-30
DSC-32-30-40
DSC-32-40-10
DSC-32-40-20
DSC-32-40-30
DSC-32-40-40
DSC-33-10-10
DSC-33-10-20
DSC-33-10-30
DSC-33-10-40
DSC-33-20-10
DSC-33-20-20
DSC-33-20-30
DSC-33-30-10
DSC-33-30-20
DSC-33-30-30
DSC-33-30-40
DSC-33-40-10
DSC-34-10-10
CAL A330/A340 FLEET
FCOM
Subsection Title
Indications on ND
EFIS Controls
General
Controls and Indicators
Flight Data Recording System
Controls and Indicators
Aircraft Condition Monitoring System (ACMS)
Warnings and Cautions
Electrical Supply
Description
Landing Gear System Interface
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
General
Description
Controls and Indicators
Electrical Supply
General
Controls and Indicators
Electrical Supply
GENERAL
OPERATION
CONTROLS AND INDICATORS
ELECTRICAL SUPPLY
Controls and Indicators
Description
Rev. Date
20 JAN 15
18 FEB 14
18 FEB 14
07 APR 11
18 FEB 14
28 NOV 12
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
07 APR 11
27 JUN 14
20 JAN 15
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
07 APR 11
28 NOV 12
18 MAR 15
05 AUG 14
18 FEB 14
28 NOV 12
18 FEB 14
27 JUN 14
07 APR 11
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
18 MAR 15
18 FEB 14
Continued on the following page
PLP-LESS P 8/16
30 JUN 15
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LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
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R
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Localization
DSC-34-10-20
DSC-34-10-30
DSC-34-10-40
DSC-34-15-10
DSC-34-15-20
DSC-34-15-30
DSC-34-15-40
DSC-34-20
DSC-34-25
DSC-34-30-10
DSC-34-30-20
DSC-34-30-30
DSC-34-30-40
DSC-34-30-50
DSC-34-40-10
DSC-34-40-20
DSC-34-40-30
DSC-34-50-10
DSC-34-50-20
DSC-34-50-30
DSC-34-50-35
DSC-34-50-40
DSC-34-60-10
DSC-34-60-20
DSC-34-60-30
DSC-34-60-40
DSC-34-60-50
DSC-34-70-10
DSC-34-70-20
DSC-34-70-30
DSC-34-70-40
DSC-34-70-50
DSC-34-70-60
DSC-34-80-10
DSC-34-80-20
DSC-34-80-30
DSC-34-80-40
DSC-34-90-30
DSC-35-10
CAL A330/A340 FLEET
FCOM
Subsection Title
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Normal Operation
Operation in Case of Failure
Warning and Cautions
Standby Instruments
ISIS
Tuning
NAVAIDS
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Remote ATC Box
Warnings and Cautions
Electrical Supply
Description
Predictive Windshear System
Controls and Indicators
Warning and Cautions
Electrical Supply
Description
GPWS Basic Modes
EGPWS Functions
Controls and Indicators
Warnings and Cautions
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
Electrical Supply
General
Rev. Date
18 FEB 14
20 JAN 15
18 FEB 14
07 APR 11
15 FEB 13
07 APR 11
18 MAR 15
18 FEB 14
30 JUN 15
15 FEB 13
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
04 OCT 11
18 FEB 14
18 FEB 14
18 MAR 15
07 APR 11
18 FEB 14
18 FEB 14
18 MAR 15
05 MAR 14
20 JAN 15
15 FEB 13
18 FEB 14
18 FEB 14
27 JUN 14
18 FEB 14
25 NOV 11
18 FEB 14
18 FEB 14
20 JAN 15
18 FEB 14
18 FEB 14
18 FEB 14
07 APR 11
07 APR 11
Continued on the following page
PLP-LESS P 9/16
30 JUN 15
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
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Localization
DSC-35-20-10
DSC-35-20-20
DSC-35-20-30
DSC-35-30-10
DSC-35-30-20
DSC-35-30-30
DSC-35-30-40
DSC-35-40-10
DSC-36-10-10
DSC-36-10-20
DSC-36-10-30
DSC-36-10-40
DSC-36-10-50
DSC-36-10-60
DSC-36-10-70
DSC-36-20
DSC-36-30
DSC-36-40
DSC-38-10
DSC-38-20
DSC-45-10
DSC-45-20
DSC-45-30
DSC-45-35
DSC-45-40
DSC-46-10
DSC-46-20
DSC-46-30
DSC-46-40
DSC-46-55-10
DSC-46-55-20
DSC-46-55-30
DSC-46-60
DSC-46-65
DSC-46-70
DSC-49-10-10
DSC-49-10-20
DSC-49-20
DSC-49-30
CAL A330/A340 FLEET
FCOM
Subsection Title
Description
Controls and Indicators
Electrical Supply
Description
Controls and Indicators
Warnings and Cautions
Electrical Supply
DESCRIPTION
General
Engine Bleed System
APU Bleed Air Supply
HP Ground Air Supply
Crossbleed
Leak Detection
Operation Following Failures
Controls and Indicators
Warnings and Cautions
ELECTRICAL SUPPLY
Description
Electrical Supply
DESCRIPTION
SYSTEM OPERATION
Data Loader
Printer
ELECTRICAL SUPPLY
General
ATSU Communication Function
AOC APPLICATIONS
CNS/ATM
Glareshield
DCDU
MCDU
Warnings and Cautions
AINS
Electrical Supply
General
Main Components
Controls and Indicators
WARNINGS AND CAUTIONS
Rev. Date
18 FEB 14
05 AUG 14
07 APR 11
30 JUN 15
28 NOV 12
20 JAN 15
07 APR 11
28 NOV 12
18 FEB 14
18 FEB 14
28 NOV 12
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
18 FEB 14
05 AUG 14
18 MAR 15
18 FEB 14
15 FEB 13
18 FEB 14
30 MAY 12
18 FEB 14
15 FEB 13
18 FEB 14
18 FEB 14
18 FEB 14
30 JUN 15
18 FEB 14
07 APR 11
18 FEB 14
18 FEB 14
18 FEB 14
Continued on the following page
PLP-LESS P 10/16
30 JUN 15
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
R
R
Continued from the previous page
Localization
DSC-49-40
DSC-52-10-10
DSC-52-10-20
DSC-52-10-30
DSC-52-10-40
DSC-52-10-50
DSC-52-10-60
DSC-52-10-70
DSC-52-10-80
DSC-52-20
DSC-52-30
DSC-52-40
DSC-70-10
DSC-70-20
DSC-70-30-10
DSC-70-30-30
DSC-70-30-40
DSC-70-30-50
DSC-70-40-10
DSC-70-40-20
DSC-70-40-30
DSC-70-40-40
DSC-70-40-50
DSC-70-50
DSC-70-60
DSC-70-70
DSC-70-80-10
DSC-70-80-20
DSC-70-80-30
DSC-70-80-40
DSC-70-90
DSC-70-92
DSC-70-97
DSC-70-98
PRO-PLP-LETDU
PRO-NOR-SRP-01-05
PRO-NOR-SRP-01-10
PRO-NOR-SRP-01-15
PRO-NOR-SRP-01-20
CAL A330/A340 FLEET
FCOM
Subsection Title
Rev. Date
ELECTRICAL SUPPLY
07 APR 11
General
18 FEB 14
Passengers Doors
27 JUN 14
Emergency Exits
30 MAY 13
Cargo Doors
18 FEB 14
Avionics Compartment Access Door
07 APR 11
Cockpit Door
07 APR 11
Escape Slides/Rafts
18 FEB 14
Doors and Slides Control System
27 JUN 14
Controls and Indicators
18 FEB 14
WARNINGS AND CAUTIONS
18 FEB 14
ELECTRICAL SUPPLY
07 APR 11
ENGINE
18 FEB 14
FADEC
18 FEB 14
GENERAL
28 NOV 12
THRUST LEVERS
18 FEB 14
THRUST RATING LIMIT
18 FEB 14
THRUST CONTROL
18 FEB 14
GENERAL
18 FEB 14
FUEL PUMP UNIT/ MAIN ENGINE PUMP
18 FEB 14
SHUT-OFF VALVES
18 FEB 14
HYDROMECHANICAL UNIT / FUEL METERING UNIT
18 FEB 14
IDG OIL COOLING SYSTEM
18 FEB 14
OIL SYSTEM
18 FEB 14
AIRBLEED SYSTEM
18 FEB 14
THRUST REVERSER SYSTEM
18 FEB 14
General
05 MAR 14
Ignition System
27 JUN 14
Engine Starting System
18 FEB 14
Alternate Start/Ignition Information
28 NOV 12
A330 Controls and Indicators (GE)
30 JUN 15
A340 Controls and Indicators (CFM)
30 JUN 15
A330 Electrical Supply
18 FEB 14
A340 Electrical Supply
30 MAY 12
LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS
30 JUN 15
Introduction
28 NOV 12
Cockpit Preparation
15 FEB 13
Before Push Back or Start
28 NOV 12
Taxi
20 JAN 15
Continued on the following page
PLP-LESS P 11/16
30 JUN 15
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
R
R
Continued from the previous page
Localization
PRO-NOR-SRP-01-30
PRO-NOR-SRP-01-40
PRO-NOR-SRP-01-50
PRO-NOR-SRP-01-60
PRO-NOR-SRP-01-70
PRO-NOR-SRP-01-80
PRO-SPO-20
PRO-SPO-25-10
PRO-SPO-25-20
PRO-SPO-25-30
PRO-SPO-25-40
PRO-SPO-30
PRO-SPO-35
PRO-SPO-40-10
PRO-SPO-40-20
PRO-SPO-40-30
PRO-SPO-40-40
PRO-SPO-40-50
PRO-SPO-40-60
PRO-SPO-40A-10
PRO-SPO-40A-20
PRO-SPO-40A-30
PRO-SPO-40A-40
PRO-SPO-40A-50
PRO-SPO-40A-60
PRO-SUP-22-10
PRO-SUP-22-20-15
PRO-SUP-22-30
PER-PLP-LETDU
PER-LOD-GEN
PER-LOD-CGO
PER-LOD-FUL
PER-LOD-WBA-LTS
PER-LOD-WBA-FIT-10
PER-OPD-GEN
PER-OPD-CON-AEO
PER-OPD-CON-OEI
PER-OPD-CON-TEI
PER-THR-GEN
CAL A330/A340 FLEET
FCOM
Subsection Title
Rev. Date
TAKEOFF
18 FEB 14
Climb
20 JAN 15
Cruise
20 JAN 15
Descent
18 MAR 15
Approach
20 JAN 15
Go-Around
20 JAN 15
Flight without Cabin Pressurization
30 JUN 15
General
07 APR 11
Limitations
18 FEB 14
Procedures
20 JAN 15
Performance
18 FEB 14
HIGH ALTITUDE OPERATION
07 APR 11
FLIGHT OVER MOUNTAINOUS AREA
28 NOV 12
General
07 APR 11
Technical Condition of the Aircraft
18 FEB 14
Operational Limitations
07 APR 11
Normal Operating Procedures
25 NOV 11
Abnormal Operating Procedures
07 APR 11
Performance
28 NOV 12
General
18 FEB 14
Operational Limitations
18 FEB 14
Dispatch Consideration
18 FEB 14
Diversion During Extended Range Operations
20 JAN 15
Procedures
18 FEB 14
Performance
18 FEB 14
FMGES Reset and other Abnormal Procedures
20 JAN 15
FMS2 Honeywell Specificities
20 JAN 15
Navigation Database
18 FEB 14
LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS
30 JUN 15
GENERAL
20 AUG 10
CARGO LOADING
18 FEB 14
FUEL
30 JUN 15
LTS LOAD AND TRIM SHEET
18 FEB 14
FUEL INDEX TABLE
18 FEB 14
GENERAL
07 APR 11
ALL ENGINES OPERATIVE
18 FEB 14
ONE ENGINE INOPERATIVE
18 FEB 14
TWO ENGINE INOPERATIVE
20 AUG 10
GENERAL
07 APR 11
Continued on the following page
PLP-LESS P 12/16
30 JUN 15
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
Localization
PER-THR-MTO
PER-THR-DTO
PER-THR-MGA
PER-THR-FLX
PER-THR-MCT
PER-THR-MCL
PER-THR-MCR
PER-TOF-THR-FLX-10
PER-TOF-THR-FLX-20
PER-TOF-THR-FLX-30
PER-TOF-THR-FLX-40
PER-TOF-THR-DRT
PER-TOF-TOC-05
PER-TOF-TOC-10-10
PER-TOF-TOC-10-20
PER-TOF-TOC-10-30
PER-TOF-TOC-12-10
PER-TOF-TOC-12-20
PER-TOF-TOC-12-30
PER-TOF-TOC-12-40
PER-TOF-TOC-12-50
PER-TOF-TOC-14-10
PER-TOF-TOC-14-20
PER-TOF-TOC-14-25
PER-TOF-TOC-14-30
PER-TOF-TOC-16-10
PER-TOF-TOC-16-20
PER-TOF-TOC-16-30
PER-TOF-TOC-18-10
PER-TOF-TOC-18-20
PER-TOF-TOC-18-30
PER-TOF-TOC-18-40
PER-TOF-TOC-18-50
PER-TOF-TOC-20-10
PER-TOF-TOC-20-20
PER-TOF-TOC-20-30
CAL A330/A340 FLEET
FCOM
Subsection Title
Rev. Date
MAXIMUM TAKEOFF
18 FEB 14
DERATED TAKEOFF
18 FEB 14
MAXIMUM GO AROUND
18 FEB 14
FLEXIBLE TAKEOFF
18 FEB 14
MAXIMUM CONTINUOUS
18 FEB 14
MAXIMUM CLIMB
18 FEB 14
MAXIMUM CRUISE
18 FEB 14
DEFINITION OF FLEXIBLE TAKEOFF
07 APR 11
USE OF FLEXIBLE TAKEOFF
07 APR 11
REQUIREMENTS
18 FEB 14
RECOMMENDATION
18 FEB 14
DERATED TAKEOFF
05 MAR 14
INTRODUCTION
07 APR 11
TAKEOFF PERFORMANCE
18 FEB 14
TAKEOFF CHART DESCRIPTION
07 APR 11
ADDITIONAL INFORMATION
20 JAN 15
DETERMINATION OF MAXIMUM TAKEOFF WEIGHT AND
20 JAN 15
SPEEDS
VMU CHECK
07 APR 11
EXTRAPOLATION
07 APR 11
MAXIMUM STRUCTURAL TAKEOFF WEIGHT
07 APR 11
SUMMARY
07 APR 11
DETERMINATION OF FLEXIBLE TAKEOFF TEMPERATURE
20 JAN 15
AND SPEEDS
FLEXIBLE TAKEOFF NOT POSSIBLE
18 FEB 14
FLEXIBLE TAKEOFF POSSIBLE BUT NOT USED
18 FEB 14
SUMMARY
07 APR 11
TAKEOFF PERFORMANCE
18 FEB 14
TAKEOFF CHART DESCRIPTION
07 APR 11
ADDITIONAL INFORMATION
20 JAN 15
DETERMINATION OF MAXIMUM TAKEOFF WEIGHT AND
20 JAN 15
SPEEDS
VMU CHECK
07 APR 11
EXTRAPOLATION
20 AUG 10
MAXIMUM STRUCTURAL TAKEOFF WEIGHT
07 APR 11
SUMMARY
07 APR 11
DETERMINATION OF FLEXIBLE TAKEOFF TEMPERATURE
20 JAN 15
AND SPEEDS
FLEXIBLE TAKEOFF NOT POSSIBLE
07 APR 11
SUMMARY
07 APR 11
Continued on the following page
PLP-LESS P 13/16
30 JUN 15
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
Localization
PER-TOF-TOD-24
PER-TOF-TOD-25-10
PER-TOF-TOD-25-20
PER-TOF-CTA-10
PER-TOF-CTA-20
PER-TOF-CTA-30
PER-TOF-CTA-40-10
PER-TOF-CTA-40-20
PER-TOF-CTA-40-30
PER-TOF-CTA-40-40
PER-FPL-GEN-MFR
PER-FPL-GEN-FPL
PER-FPL-FLP-QFP-10
PER-FPL-FLP-QFP-20
PER-FPL-FLP-QFP-30
PER-FPL-FLP-QFP-40
PER-FPL-FLP-QFP-50
PER-FPL-FLP-ALN-20
PER-CLB-GEN
PER-CLB-ALT-CLB
PER-CLB-CLT
PER-CLB-DCL-10
PER-CLB-DCL-20
PER-CLB-DCL-30
PER-CLB-DCL-40
PER-CRZ-ALT-10
PER-CRZ-ALT-20
PER-CRZ-CRT-10
PER-CRZ-CRT-20
PER-CRZ-CRT-30
PER-CRZ-CRT-40
PER-CRZ-CRT-50
PER-CRZ-ICQ-10
PER-CRZ-ICQ-20
PER-HLD-GEN
PER-HLD-HLD
PER-DES-GEN
PER-DES-STD
CAL A330/A340 FLEET
FCOM
Subsection Title
Rev. Date
QNH/BLEEDS CORRECTION
18 FEB 14
SPEEDS LIMITED BY VMC
18 FEB 14
V2 LIMITED BY VMU/VMCA
18 FEB 14
GENERAL
20 JAN 15
DEFINITIONS
20 JAN 15
OPERATIONAL CONDITIONS
07 APR 11
TAKEOFF PERFORMANCE
07 APR 11
TAKEOFF FROM A WET RUNWAY
18 FEB 14
TAKEOFF FROM A CONTAMINATED RUNWAY
18 FEB 14
EXAMPLE
20 JAN 15
MINIMUM RECOMMENDED FUEL REQUIREMENTS
18 FEB 14
FLIGHT PLAN
20 AUG 10
INTRODUCTION
18 FEB 14
CORRECTION FOR DEVIATION FROM REFERENCE LANDING
07 APR 11
WEIGHT
EXAMPLE
20 JAN 15
FLIGHT PLANNING AT A GIVEN MACH NUMBER
18 FEB 14
FLIGHT PLANNING AT LONG RANGE SPEED
18 FEB 14
ALL ENGINES OPERATIVE
18 FEB 14
GENERAL
18 FEB 14
CLIMB CEILINGS
20 JAN 15
CLIMB TABLES
20 JAN 15
USE OF DERATED CLIMB
07 APR 11
DERATED CLIMB LEVEL DETERMINATION
18 FEB 14
DERATED CLIMB 1 TABLES
20 JAN 15
DERATED CLIMB 2 TABLES
20 JAN 15
OPTIMUM AND MAXIMUM ALTITUDES
20 JAN 15
WIND ALTITUDE TRADE FOR CONSTANT SPECIFIC RANGE
18 FEB 14
GENERAL
07 APR 11
CRUISE AT M.80
18 FEB 14
CRUISE AT M.82
18 FEB 14
CRUISE AT M.84
18 FEB 14
CRUISE AT LONG RANGE
18 FEB 14
GENERAL
20 JAN 15
EXAMPLE
20 JAN 15
GENERAL
20 JAN 15
HOLDING TABLES
20 JAN 15
GENERAL
18 FEB 14
STANDARD
18 FEB 14
Continued on the following page
PLP-LESS P 14/16
30 JUN 15
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
Localization
PER-DES-EMG
PER-GOA-GEN
PER-GOA-ACG-NOR
PER-GOA-ACG-CAT
PER-LDG-GEN
PER-LDG-CTA-20
PER-LDG-DIS-MAT
PER-LDG-DIS-RLD
PER-OEI-GEN-05
PER-OEI-GEN-10
PER-OEI-GEN-15
PER-OEI-GEN-20
PER-OEI-ALT-10
PER-OEI-CRT-10
PER-OEI-CRT-20
PER-OEI-ICQ-10
PER-OEI-ICQ-20
PER-OEI-HLD
PER-OEI-DES-10
PER-OEI-DES-15
PER-OEI-DES-20
PER-OEI-DES-30
PER-OEI-ALN
PER-TEI-GEN
PER-TEI-ALT-10
PER-TEI-CRT-10
PER-TEI-ICQ
PER-TEI-HLD
PER-TEI-DES-10
PER-TEI-DES-20
Subsection Title
EMERGENCY
GENERAL
NORMAL
CATII
GENERAL
DEFINITIONS
Runway Condition Assessment Matrix for Landing
REQUIRED LANDING DISTANCES / MANUAL LANDING
GENERAL
STANDARD STRATEGY
OBSTACLE STRATEGY
FIXED SPEED STRATEGIES
CEILINGS
STANDARD AND OBSTACLE STRATEGIES
FIXED SPEED STRATEGIES
IN CRUISE QUICK CHECK AT LONG RANGE
FIXED SPEED STRATEGIES
HOLDING
STANDARD STRATEGY
OBSTACLE STRATEGY
FIXED SPEED STRATEGIES
DESCENT TO LANDING
ALTERNATE
GENERAL
CEILINGS
STANDARD STRATEGY
IN CRUISE QUICK CHECK
HOLDING
STANDARD STRATEGY
DESCENT TO LANDING
Rev. Date
20 JAN 15
05 MAR 14
18 FEB 14
18 FEB 14
30 MAY 12
20 JAN 15
05 AUG 14
20 JAN 15
20 JAN 15
20 JAN 15
20 JAN 15
20 JAN 15
20 JAN 15
20 JAN 15
20 JAN 15
20 JAN 15
20 JAN 15
18 FEB 14
20 JAN 15
20 JAN 15
18 FEB 14
18 FEB 14
07 APR 11
20 JAN 15
20 JAN 15
20 JAN 15
07 APR 11
07 APR 11
20 JAN 15
20 JAN 15
(1) Evolution code : N=New, R=Revised, E=Effectivity, M=Moved
CAL A330/A340 FLEET
FCOM
PLP-LESS P 15/16
30 JUN 15
PRELIMINARY PAGES
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
Intentionally left blank
CAL A330/A340 FLEET
FCOM
PLP-LESS P 16/16
30 JUN 15
PRELIMINARY PAGES
AIRCRAFT ALLOCATION TABLE
A330/A340
FLIGHT CREW
OPERATING MANUAL
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
Registration Number
Model
0402
B-18801
340-313
0406
B-18802
340-313
0411
B-18803
340-313
0415
B-18805
340-313
0433
B-18806
340-313
0541
B-18807
340-313
0602
B-18301
330-302
0607
B-18302
330-302
0641
B-18303
330-302
0671
B-18305
330-302
0675
B-18306
330-302
0691
B-18307
330-302
0699
B-18308
330-302
0707
B-18309
330-302
0714
B-18310
330-302
0725
B-18351
330-302
0752
B-18311
330-302
0769
B-18312
330-302
0805
B-18352
330-302
0823
B-18315
330-302
0838
B-18316
330-302
0861
B-18317
330-302
0920
B-18353
330-302
1177
B-18355
CAL A330/A340 FLEET
FCOM
FSN
330-302
Continued on the following page
PLP-AAT P 1/2
20 JAN 15
PRELIMINARY PAGES
AIRCRAFT ALLOCATION TABLE
A330/A340
FLIGHT CREW
OPERATING MANUAL
Continued from the previous page
(1)
M
MSN
FSN
Registration Number
Model
1272
B-18356
330-302
1278
B-18357
330-302
1346
B-18358
330-302
1367
B-18359
330-302
1450
B-18360
330-302
1539
B-18361
330-302
(1) Evolution code : N=New, R=Revised
CAL A330/A340 FLEET
FCOM
PLP-AAT P 2/2
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
MODIFICATION
C10655
Linked SB
49-3029 01
49-4033 01
Incorp. Date
Title
07 APR 11
Applicable to: ALL
D17250
AIRBORNE AUXILIARY POWER - CONTROL AND
MONITORING - UPDATE ELECTRONIC CONTROL
BOX (VECB) SOFTWARE OF APU 331-350
20 AUG 10
Applicable to: ALL
D17251
AIR CONDITIONING-DEFINE VENTILATION OF
FORWARD CARGO COMPARTMENT
20 AUG 10
Applicable to: ALL
D17253
AIR CONDITIONING-DEFINE TEMPERATURE
CONTROL OF FORWARD CARGO COMPARTMENT
20 AUG 10
AIR CONDITIONING-DEFINE HEATING SYSTEM FOR
LOWER DECK BULK CARGO COMPARTMENT
Applicable to: ALL
D17263
20 AUG 10
Applicable to: B-18801, B-18802, B-18803, B-18805
D17512
20 AUG 10
WATER/WASTE - INSTALL A 3RD WASTE TANK
DOORS-EMERGENCY EXIT-INTRODUCE "TYPE A
DOOR"
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D17864
20 AUG 10 WATER/WASTE-POTABLE WATER SYSTEM
INTRODUCE INDEPENDANT PRESSURIZATION
Applicable to: ALL
D17890
20 AUG 10 EQUIPMENT/FURNISHINGS-CREW REST
COMPARTMENT-INSTALL STRUCTURAL
PROVISIONS
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D17891
20 AUG 10 EQUIPMENT/FURNISHINGS-CREW REST
COMPARTMENT-INSTALL SYSTEM PROVISIONS
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D18022
20 AUG 10 FIRE PROTECTION-EXTEND DURATION OF CARGO
COMPARTMENT FIRE SUPPRESSION
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
D18034
20 AUG 10 ICE AND RAIN PROTECTION-INSTALL GIRT BAR
FITTING HEATING SYSTEM FOR ENTRY DOORS
Applicable to: ALL
D18123
20 AUG 10 EQUIPMENT/FURNISHINGS-INSTALL PROVISIONS
FOR AN UNDERFLOOR CREW REST CONTAINER
(BFE)
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 1/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
D18217
Linked SB
Incorp. Date
Title
20 AUG 10
Applicable to: ALL
D18218
FIRE PROTECTION-INSTALL H.T.L. EXTINGUISHER
IN FWD AND AFT CARGO COMPARTMENT
20 AUG 10
Applicable to: ALL
D18236
LIGHTS-NAVIGATION-INSTALL DUPLICATED
NAVIGATION LIGHTS
20 AUG 10
EQUIPMENT/FURNISHINGS-CREW REST ROOM UNCLIP BFE U.C.R.C. CIRCUIT BREAKERS
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D18762
20 AUG 10 DOORS-CARGO COMPARTMENT DOOR HYDRAULIC
SYSTEM-INTRODUCE MODIFIED ELECTRICAL
(MANUAL) SELECTOR VALVE
Applicable to: ALL
D19283
20 AUG 10 APU-CONTROL AND MONITORING- INTRODUCE
STANDARD-7 ECB
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D19367
20 AUG 10 AIR CONDITIONING - PRESSURE CONTROL
AND MONITORING - IMPROVE LANDING FIELD
ELEVATION SELECTOR
Applicable to: ALL
D19437
20 AUG 10 AIR CONTIONING-PRESSURE CONTROL AND
MONITORING-IMPROVE CABIN PRESSURE
CONTROLLER (CPC)
Applicable to: ALL
D19479
20 AUG 10 APU - CONTROL AND MONITORING - INTRODUCE
IMPROVED ECB -8
Applicable to: ALL
D19781
20 AUG 10 FLIGHT CONTROLS-RUDDER MECHANICAL
CONTROL-REPLACE FIBER GLASS CONTROL ROD
BY ALUMINIUM ALLOY ROD
Applicable to: ALL
D19899
20 AUG 10 AIR CONDITIONNING - LWR DK CARGO COMPT.
VENTILATION AND COOLING (FWD AND AFT) INTRODUCE COMMON VENTILATION CONTROLLER
Applicable to: ALL
D19920
20 AUG 10 EQUIPMENT/FURNISHINGS-EMERGENCY- DELETE
SLIDES AND INSTALL SLIDE RAFTS ON EXIT TYPE A
DOOR 3 ON A330-300
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 2/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
D40398
Applicable to: ALL
D40487
Linked SB
Incorp. Date
20 AUG 10
Title
AIRBORNE AUXILIARY POWER - CONTROL AND
MONITORING - INTRODUCE VERSATILE ECB
FUEL - APU FUEL PUMP SYSTEM - PREVENT AN
ELECTRICAL ESS NETWORK "OVERLOAD" (A330)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D40488
20 AUG 10 FUEL - APU FUEL PUMP SYSTEM - PREVENT AN
ELECTRICAL ESS NETWORK 'OVERLOAD' (A340)
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D40534
20 AUG 10 AIR CONDITIONING - PRESSURE CONTROL
- INTRODUCE MODIFIED CABIN PRESSURE
CONTROLLER P/N 20793-01AA
Applicable to: ALL
D40555
20 AUG 10 LIGHTS - CABIN EMERGENCY LIGHTING
- INTRODUCE IMPROVED EPSU (FOR
115V-AC-SYSTEM)
Applicable to: ALL
D40775
20 AUG 10 FIRE PROTECTION - SMOKE DETECTION - INSTALL
PHOTO-ELECTRIC CELL SMOKE DETECTORS
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
D40814
20 AUG 10 OXYGEN PASSENGER - OXYGEN SYSTEM INTRODUCE IMPROVED 02 CONTAINER SERIES 15
MIN. FROM VENDOR DRAEGER
Applicable to: ALL
D41253
20 AUG 10 LIGHTS - CABIN EMERGENCY LIGHTING INTRODUCE A NEW EPSU (FOR 6V-DC-SYSTEM)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18801, B-18802, B-18803, B-18805, B-18806
D41519
20 AUG 10 COMMUNCIATION-EXTERNAL VIDEO
MONITORING-INSTALL EXTERNAL VIEW CAMERA
Applicable to: ALL
D41807
20 AUG 10 LIGHTS-CABIN EMERGENCY LIGHTING- INSTALL
PHOTOLUMINISCENT ESCAPE PATH MARKING
FLOOR
Applicable to: ALL
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 3/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
D41829
Linked SB
Incorp. Date
Title
COMMUNICATIONS - CIDS - PED SWITCH AT FAP
FROM P/C ELECTRICAL POWER SUPPLY
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D42265
20 AUG 10 AIR CONDITIONING - PACK CONTROL AND
INDICATING - INTRODUCE PACK CONTROLLER B-01
Applicable to: ALL
D42415
07 APR 11 WATER/WASTE - TOILET SYSTEM - DELETE WASTE
TANK BALANCING SYSTEM FOR TWO TANK
VERSIONS (SERIAL SOLUTION)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18806, B-18807
D42587
07 APR 11 FUSELAGE - GENERAL - REAR FUSELAGE
INTRODUCE CFRP PRESSURE BULKHEAD FRAME
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D42829
20 AUG 10 COMMUNICATIONS - GENERAL - BASIC PROVISIONS
FOR IN FLIGHT ENTERTAINMENT SYSTEM
A330/A340-200/300
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D42874
20 AUG 10 COMMUNICATIONS - GENERAL - ADAPT ATA
23 CABIN SYSTEMS FOR ENHANCED CABIN
A330/A340-300
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D42876
20 AUG 10 AIR CONDITIONING-GENERAL-ADAPT SYSTEM TO
ENHANCED CABIN FOR BASIC AIRCRAFT (COMMON
PART)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D43046
20 AUG 10 E/F-PASSENGER COMPARTMENT SEATSINTRODUCE IN-SEAT POWER SUPPLY SYSTEM
(ISPSS) 110V FROM VENDOR K.I.D.
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18801, B-18802, B-18803,
B-18805, B-18806, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 4/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
D43203
Linked SB
Incorp. Date
Title
20 AUG 10
Applicable to: B-18806, B-18807
D43619
WATER/WASTE - TOILET SYSTEM - INSTALL
OPTIONAL 3 WASTE TANK SYSTEM INCLUDING
BALANCING
20 AUG 10
Applicable to: ALL
D43999
EQUIPMENT/FURNISHINGS-COCKPIT- INSTALL ELT
REMOTE CONTROL PANEL IN COCKPIT -SEXTANT-
20 AUG 10
E/F-PAX COMPARTMENT SEATS INSTALLATION OF
A PED (PASSENGER ELCTRONIC DEVICE)ON/OFF
SWITCHIN THE COCKPIT)
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D44099
25-4181 02
20 AUG 10 EQUIPMENT/FURNISHINGS - COCKPIT - INSTALL AN
ARMOURED COCKPIT DOOR
Applicable to: ALL
D44330
20 AUG 10 PNEUMATIC - LEAK DETECTION - INTRODUCE
ADAPTED DUAL LOOP OVERHEAT LEAK DETECTION
ON APU BLEED AIR DUCT
Applicable to: B-18307, B-18308, B-18309, B-18310, B-18311, B-18312, B-18315, B-18316, B-18317, B-18351,
B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D44341
20 AUG 10 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT
- INSTALL NOISE REDUCED COCKPIT DOOR LOCK
SYSTEM
Applicable to: B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311, B-18312, B-18315, B-18316,
B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D44356
20 AUG 10 AIR CONDITIONING - AIR CONDITIONNING
((PACKS)) - INTRODUCE NEW PACK -08 STANDARD
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D44363
25-4194 00
20 AUG 10 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT
- INSTALL A DECOMPRESSION PANEL IN COCKPIT
DOOR FROM VENDOR RBE
Applicable to: ALL
D44364
25 NOV 11 AIR CONDITIONING - PRESSURIZATION CONTROL
- INSTALL ECAM INDICATION FOR 3RD SAFETY
VALVE (INTERIM SOLUTION)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 5/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
D44428
Applicable to: ALL
D44434
Linked SB
27-4112 00
Incorp. Date
07 APR 11
Title
FLIGHT CONTROLS - SLAT/FLAP CONTROL
COMPUTER (SFCC) - INTRODUCE MODIFIED
SLAT/FLAP CONTROL COMPUTER (STD -509)
AIR CONDITIONING - LOWER DECK CARGO
COMPARTMENT - INTRODUCE VENTILATION
CONTROLLER -03AD
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D44532
25-4218 03
20 AUG 10 EQUIPMENT/FURNISHINGS - CURTAINS AND
PARTITIONS -MODIFY CDLS STRIKE TOLERANCE
Applicable to: B-18301, B-18302, B-18303, B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D44567
20 AUG 10 OXYGEN - PASSENGER OXYGEN - INTRODUCE
IMPROVED PASSENGER OXYGEN CONTAINER FOR
CHEMICAL SYS.15 MIN (DRAEGER,TYPE V/VI)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
D44690
20 AUG 10 EQUIPMENT/FURNISHINGS - CURTAINS AND
PARTITIONS - INSTALL A MAXIMUM NOISE
REDUCED COCKPIT DOOR LOCK SYSTEM (CDLS)
Applicable to: B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311, B-18312, B-18315, B-18316,
B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D44784
20 AUG 10 AIR CONDITIONING - PRESSURE CONTROL AND
MONITORING-INTRODUCE RESIDUAL PRESSURE
CONTROL UNIT (RPCU)
Applicable to: B-18308, B-18309, B-18310, B-18311, B-18312, B-18315, B-18316, B-18317, B-18351, B-18352,
B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D44931
07 APR 11 FLIGHT CONTROLS - SLAT/FLAP CONTROL
COMPUTER - INTRODUCE REDESIGNED SLAT/FLAP
CONTROL COMPUTER (SFCC)
Applicable to: B-18315, B-18316, B-18317, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359,
B-18360, B-18361
D45206
20 AUG 10 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT
SEATS- INSTALL A PED (PAX ELECTRONIC DEVICE)
"ON/OFF" SWITCH IN THE VIDEO CONTROL
INCLUDING WIRING PROV.
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 6/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
D45552
Linked SB
20 AUG 10
Title
COMMUNICATIONS - VIDEO MONITORING - INSTALL
A COCKPIT DOOR SURVEILLANCE SYSTEM (CDSS)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18801, B-18802, B-18803, B-18805, B-18806
D45874
52-4078 03
20 AUG 10 DOORS - COCKPIT DOOR RELEASE SYSTEM OVERRIDE ELECTRICAL SYSTEM
Applicable to: B-18301, B-18302, B-18801, B-18802, B-18803, B-18805, B-18806
D45966
20 AUG 10 INDICATION/RECORDING SYSTEM - RECORDERS INSTALL FDIMU HARDWARE ON A330/A340
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D46066
07 APR 11 COMMUNICATIONS- PAX MUSIC ENTERTAINMENT
-ADD SWITCHES FOR REMOVAL OF ELECTRICAL
POWER FROM THE IFE EQUIPMENT
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D46190
20 AUG 10 AIR CONDITIONING - CABIN AIR DISTRIBUTION
- MODIFY AIR EXTRACTION VENTILATION
CONTROLER
Applicable to: B-18315, B-18316, B-18317, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359,
B-18360, B-18361
D46296
07 APR 11 DOORS - DOOR AND ESCAPE SLIDE CONTROL
SYSTEM - MODIFY THE DOOR AND ESCAPE SLIDE
CONTROL SYSTEM (DSCS)
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D46710
07 APR 11 EQUIPMENT/FURNISHING - CURTAINS AND
PARTITIONS - INTRODUCE IMPROVED
DECOMPRESSION PANEL IN COCKPIT DOOR
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D47069
20 AUG 10 DOORS - COCKPIT DOOR - RELEASE SYSTEM ELECTRICAL BACKUP SYSTEM
Applicable to: B-18301, B-18302, B-18303
D49216
20 AUG 10 DOORS - COCKPIT DOOR RELEASE SYSTEMELECTRICAL BACK- UP SYSTEM
Applicable to: B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311, B-18312, B-18315, B-18316,
B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D49762
04 OCT 11 EQUIPMENT/FURNISHINGS - PAX COMPARTMENT
INSTALL PED SIGNS INSTEAD OF NS SIGNS
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D50055
30 MAY 12 OXYGEN - PASSENGER OXYGEN - ADAPT WIRING
ON PASS INFO RELAY (SOCKET) FOR CHEMICAL
OXYGEN SYSTEM
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
23-4156 12
Incorp. Date
PLP-LOM P 7/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
D50127
Linked SB
20 JAN 15
Title
HYD PWR - GREEN MAIN HYD PWR -INTRODUCE
NEW HSMU P/N WITH AUTO CLEARANCE OF GREEN
RESERVOIR LOW LEVEL LATCH
Applicable to: B-18301, B-18306, B-18307, B-18309, B-18310, B-18352, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
D50143
07 APR 11 INFORMATION SYSTEMS - AIRPLAINE INFORMATION
NETWORK SYSTEM (AINS) - REMOVE BASIC ANSU
V6
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
D51916
07 APR 11 COMMUNICATIONS - PASSENGER MUSIC
ENTERTAINMENT - REMOVE ADDITIONAL
SWITCHES FOR VCC IN THE COCKPIT
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
H12049
20 AUG 10 LANDING GEAR-CENTER LINE GEAR -INSTALL
PROVISIONS FOR T.P.I.S (TYRE PRESSURE
INDICATING SYSTEM)
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H12050
20 AUG 10 LANDING GEAR-NOSE AND MAIN GEARS- INSTALL
PROVISIONS FOR T.P.I.S (TYRE PRESSURE
INDICATING SYSTEM)
Applicable to: ALL
H12051
20 AUG 10 FUEL-REFUEL COUPLING-INSTALL ON THE LEFT
WING
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
H12083
20 AUG 10 INDICATING/RECORDING SYSTEMS- UNITS
CHANGES-REPLACE KILOG BY POUNDS
Applicable to: ALL
H12331
20 AUG 10 LANDING GEAR-TPIS-INSTALL A LABINAL SYSTEM
ON NOSE WHEELS
Applicable to: ALL
H12332
20 AUG 10 LANDING GEAR-TPIS-INSTALL A LABINAL SYSTEM
ON GOODRICH MAIN WHEELS
Applicable to: ALL
H12600
20 AUG 10 WINGS-GENERAL-DEFINE A340 GROWTH VERSION
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H12675
20 AUG 10 GENERAL-COMPLETE BASIC A/C DEFINITION (A330)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
29-3112 01
29-4087 00
Incorp. Date
PLP-LOM P 8/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
H12719
Applicable to: ALL
H13038
Linked SB
Incorp. Date
Title
20 AUG 10
FUEL-TRIM TRANSFER SYSTEM-FIT FORWARD
TRANSFER PUMP IN THE TRIM HORIZONTAL
STABILIZER
20 AUG 10
LANDING GEAR - NLG - INSTALL A WARNING
SYSTEM IN COMPLIANCE WITH JAR 25-745
Applicable to: ALL
H13130
20 AUG 10 FUEL-GENERAL-INCREASE FUEL CAPACITY
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H13154
20 AUG 10 LANDING GEAR - MAIN GEAR - FIT STRENGTHENED
MAIN LANDING GEAR FOR GROWTH A/C
Applicable to: ALL
H13259
20 AUG 10 FUEL - GENERAL - ADAPT A330 EIS FUEL SYSTEM
TO SUIT A330A+
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
H13462
20 AUG 10 FUEL - TANKS - INCREASE TRIM TANK CAPACITY BY
230 LITRES
Applicable to: ALL
H13486
20 AUG 10 FUEL - APU PUMP SYSTEM - FIT TIME DELAY RELAY
IN FORWARD APU PUMP CONTROL CIRCUIT
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H13532
20 AUG 10 GENERAL - INTRODUCE A340/300 INCREASED
DESIGN WEIGHT MTOW 275T, MLW 190T, MZFW
178T (WV021)
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H13614
20 AUG 10 FUEL - REFUEL/DEFUEL SYSTEM - INSTALL
PRESSURE SWITCH AT WING CENTRE SECTION
REAR WALL
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H13629
20 AUG 10 FUEL - CROSSFEED SYSTEM - REMOVE
CONNECTION FROM APU FEEDLINE
Applicable to: ALL
H13633
20 AUG 10 FUEL - REFUEL/DEFUEL SYSTEM - INSTALL
PRESSURE SWITCH AT WING CENTRE SECTION
REAR WALL (A330 ONLY)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 9/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
H13666
Applicable to: ALL
H13745
Linked SB
Incorp. Date
20 AUG 10
Title
FUEL - FMCS - FIT FCMC (STAGE 7.1) WITH
CHANGES TO SOFTWARE FOR A330 AND A340
AIRCRAFT
FUEL - MANUAL MAGNETIC INDICATORS - DELETE
REDUNDANT INDICATORS
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H13876
20 AUG 10 LANDING GEAR - NORMAL BRAKING - INSTALL
BSCU SOFTWARE STANDARD S7A
Applicable to: ALL
H13959
20 AUG 10 ICE AND RAIN PROTECTION - WING ICE
PROTECTION - RELOCATE OUTBOARD VALVE TO
INBOARD POSITION
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
H14023
20 AUG 10 LANDING GEAR - NORMAL BRAKING - INSTALL
BSCU SOFTWARE STANDARD S8C
Applicable to: ALL
H14027
20 AUG 10 FUEL - FCMS - INSTALL FCMC STAGE 9.0
Applicable to: ALL
H14072
20 AUG 10 LANDING GEAR - MAIN GEAR - INTRODUCE
SCALLOP ON GROWTH MAIN FITTING TO IMPROVE
FATIGUE LIFE (PROD. SOLUTION)
Applicable to: ALL
H14084
20 AUG 10 LANDING GEAR - NORMAL BRAKING - INSTALL
BSCU SOFTWARE STANDARD S8D
Applicable to: ALL
H14152
20 AUG 10 LANDING GEAR - NOSE GEAR DOORS - CHANGE
MARKINGS FOR MAXIMUM TOWING/PUSHBACK
TURNING ANGLE
Applicable to: ALL
H14328
20 AUG 10 GENERAL - DESIGN WEIGHT - CERTIFY A340 WITH
TRIPLE MTOW 275/260/218T
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
H14467
28-4096 01
20 AUG 10 FUEL - FCMS - ACTIVATE CREW ALERT 'FUEL
FU/FOB DISCREPANCY'
Applicable to: ALL
H14515
28-4095 01
20 AUG 10 FUEL - FCMS - INSTALL FCMC STAGE 10.0
Applicable to: ALL
H14525
20 AUG 10 FUEL - TANKS - REMOVE EXPANSION TANKS
Applicable to: B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 10/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
H14584
Applicable to: ALL
H14656
Linked SB
28-4094 00
Incorp. Date
20 AUG 10
Title
FUEL - MANUAL MAGNETIC INDICATORS - DELETE
ATTITUDE MONITOR (FIN 5000QT)
LANDING GEAR - MAIN GEAR - INTRODUCE NEW
UPPER AND LOWER TORQUE LINK AND APEX PIN
SUB-ASSEMBLIES
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
H14705
32-4187 01
20 AUG 10 LANDING GEAR - NORMAL BRAKING - INTRODUCE
STAGE 9 STANDARD BSCU
Applicable to: ALL
H15267
20 AUG 10 GENERAL - DESIGN WEIGHTS - CERTIFY A330
WV050 MTOW 230T, MLW 185T, MZFW 173T WITH
REVISED A/C DESIGN SERVICE GOAL
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
H15451
20 AUG 10 GENERAL-DESIGN WEIGHTS-CERTIFY DOUBLE
WEIGHTS MTOW 230T MLW 185T MZFW 173T MTOW
205T MLW 185T MZFW 173T (A330-300)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
H15487
20 AUG 10 GENERAL-DESIGN WEIGHTS-CERTIFY A330-300
WV053 MTOW 205T, MLW 185T, MZFW 173T
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
H15723
28-3102 00
07 APR 11 FUEL-FCMS- INSTALL FCMC STAGE 11.0
28-4119 00
Applicable to: ALL
H15805
32-3194 01
20 AUG 10 LANDING GEAR-NORMAL BRAKING-INTRODUCE
32-4238 01
STAGE 9C STANDARD BSCU
Applicable to: ALL
H15864
07 APR 11 FUEL-MANUAL MAGNETIC INDICATORS-REDUCE
QUANTITY OF MAGNETIC FUEL LEVEL INDICATOR
(MFLI)
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 11/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
H16032
Linked SB
Incorp. Date
Title
LANDING GEAR-NOSE-REMOVAL OF THE
OVERSTEER WARNING SYSTEM FROM ALL NEW
PRODUCTION AIRCRAFT
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
H16141
28-3112 00
07 APR 11 FUEL-FUEL CONTROL AND MONITORING SYSTEM
28-4128 00
(FCMS)-UPDATE FCMC SOFTWARE TO STAGE 12
Applicable to: ALL
H16450
32-3244 01
07 APR 11 LANDING GEAR - PARKING/ULTIMATE EMERGENCY
32-4285 01
BRAKING - ACTIVATE PARKING BRAKE
MONITORING FUNCTION FOR LR
Applicable to: ALL
H16473
07 APR 11 LANDING GEAR - NOSE GEAR - REINSTALL NLG
OVERSTEER WARNING SYSTEM
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S10052
20 AUG 10 AIR CONDITIONING-AVIONICS COMPARTMENTDEFINE GROUND COOLING UNIT INSTALLATION
Applicable to: ALL
S10062
20 AUG 10 ICE AND RAIN PROTECTION-DEFINE RAIN
REPELLENT SYSTEM
Applicable to: ALL
S10063
20 AUG 10 ICE AND RAIN PROTECTION-DEFINE ADVISORY
DUAL ICE DETECTION SYSTEM
Applicable to: ALL
S10072
07 APR 11 NAVIGATION-DEFINE MORA DISPLAY ON ND
Applicable to: ALL
S10077
20 AUG 10 DOORS-COCKPIT DOOR-PROVIDE ELECTRICAL
RELEASE LATCH
Applicable to: ALL
S10132
20 AUG 10 NAVIGATION - TCAS - INSTALL ALLIED SIGNAL TCAS
II SYSTEM
Applicable to: ALL
S10139
20 AUG 10 ELECTRICAL POWER-INSTALL A BATTERY
DISCHARGE WARNING
Applicable to: ALL
S10142
20 AUG 10 EQUIPMENT/FURNISHINGS-COCKPIT- INSTALL
FLOOR HEATING PANELS
Applicable to: ALL
S10240
20 AUG 10 COMMUNICATIONS-AUDIO MANAGEMENT-IMPROVE
AUDIO CONTROL PANEL (A C P)
Applicable to: ALL
Continued on the following page
CAL A330/A340 FLEET
FCOM
07 APR 11
PLP-LOM P 12/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S10300
Linked SB
Incorp. Date
Title
20 AUG 10
Applicable to: ALL
S10425
OXYGEN-CREW OXYGEN-INSTALL A 115 CU FEET
STEEL CYLINDER
20 AUG 10
Applicable to: ALL
S10491
ONBOARD MAINTENANCE SYSTEMS-UP AND DOWN
DATA LOADING-ADD A SECOND ROTATING KNOB
20 AUG 10
CERTIFICATION DOCUMENTS-PROVIDE FERRY
FLIGHT CAPABILITY WITH THREE ENGINES
OPERATIVE
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S10621
20 AUG 10 ENGINE FUEL AND CONTROL - GENERAL - PROVIDE
DERATED TAKE OFF FACILITY FOR CFMI ENGINES
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S11135
20 AUG 10 INDICATING/RECORDING SYSTEMS-FMGECREPLACE METERS BY FEET
Applicable to: ALL
S11344
20 AUG 10 NAVIGATION-TCAS-INSTALL PROVISIONS FOR FULL
TIME DISPLAY AND ABOVE/BELOW FUNCTIONS
Applicable to: ALL
S11354
20 AUG 10 FLIGHT CONTROLS-RUDDER-INSTALL ON SECOND
TRAVEL LMITER UNIT
Applicable to: ALL
S11364
20 AUG 10 ELECTRICAL POWER-GENERAL-MODIFY SUPPLY TO
CERTAIN CIRCUITS FOR ETOPS
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S11566
20 AUG 10 FLIGHT CONTROLS-INTRODUCE VISUAL
INDICATION OF SIMULTANEOUS SIDE STICK
ACTIONS
Applicable to: ALL
S11606
20 AUG 10 COMMUNICATIONS -SATELLITE COMMUNICATION INSTALL 'COLLINS' HIGH RATE SATCOM AVIONICS
Applicable to: ALL
S11658
20 AUG 10 INDICATING/RECORDING SYSTEMS-DISPLAY A
RISING RUNWAY SYMBOL ON THE PFD
Applicable to: ALL
S11767
20 AUG 10 POWER-PLANT-CFM56-5C-INTRODUCE
CFM56-5C4-ENGINE ON A340-300B
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 13/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S11778
Linked SB
Incorp. Date
Title
DOORS-CENTERLINE GEAR DOORS-INSTALL
SPOILER ( PRODUCTION SOLUTION )
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S11925
20 AUG 10 FUEL - MAIN FUEL PUMP SYSTEM - INSTALL 2
EXPANSION TANKS
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S11963
20 AUG 10 AIR CONDITIONING-AVIONICS EQUIPMENT
VENTILATION-INCREASE HORN TIME DELAY
WARNINGIN CASE OF VENT EXTRA FAULT
Applicable to: ALL
S12319
20 AUG 10 EXHAUST - THRUST REVERSER - INSTALL
INDEPENDENT SHUT OFF VALVE AND ACTIVATE T/R
LOCK CONTROL
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S12358
20 AUG 10 FLIGHT CONTROLS - CHANGE WIRING OF FCPC1
AND FCSC1 FAULT INDICATOR LIGHTS
Applicable to: ALL
S12383
20 AUG 10 INDICATING/RECORDING SYSTEMS - ELECTRICAL
CLOCK - INSTALL SMITH P/N 2610-13
Applicable to: ALL
S12470
20 AUG 10 NAVIGATION - ATC/MODE S - INSTALL ATC
CONTROL PANEL P/N 879-2525-014 FROM VENDOR
SEXTANT
Applicable to: ALL
S12609
20 AUG 10 NAVIGATION - ADIRS - FIT REDUCED VERTICAL
SEPARATION MINIMUM (RVSM)
Applicable to: ALL
S12779
20 AUG 10 AUTOFLIGHT - FMEGC - INSTALL IMPROVED
AUTOPILOT FOR GE ENGINES
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S12809
20 AUG 10 NAVIGATION -ATC/MOD S-INSTALL ATC-TCAS
CONTROL PANEL - SEXTANT - (SFE) P/N
C124-04-AA01
Applicable to: ALL
S12819
20 AUG 10 ICE AND RAIN PROTECTION - ICE DETECTION INTRODUCE LIGHTED VISUAL ICING INDICATOR
Applicable to: ALL
Continued on the following page
CAL A330/A340 FLEET
FCOM
25 NOV 11
PLP-LOM P 14/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S12935
Linked SB
Incorp. Date
Title
INDICATING/RECORDING SYSTEM -ELECTRONIC
INSTRUMENT SYSTEM (E.I.S) - INSTALL DMC
SOFTWARE V107X ON DMC B HARDWARE STD
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S12938
20 AUG 10 INDICATING/RECORDING SYSTEM -ELECTRONIC
INSTRUMENT SYSTEM (EIS) - INSTALL DMC
SOFTWARE V507X ON DMC B HARDWARE STD
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S12945
20 AUG 10 FLIGHT CONTROLS - EFCS / CONTROL INPUT AND
POWER SUPPLY - PROVIDE A SECOND ELECTRICAL
POWER SUPPLY TO FCSC2
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S13048
20 AUG 10 ELECTRICAL POWER-ELECTRICAL CONTRACTOR
MANAGEMENT SYSTEM - INSTALL NEW ECMU
STANDARD 5
Applicable to: ALL
S13072
25 NOV 11 NAVIGATION - ADIRS - INSTALL HONEYWELL 4 MCU
ADIRU WITH GPS PRIMARY CAPABILITY
Applicable to: B-18355
S13080
20 AUG 10 FLIGHT CONTROLS - CONTROL INPUTS AND
POWER SUPPLY - PROVIDE A SECOND ELECTRICAL
POWER SUPPLY TO FCPC3
Applicable to: ALL
S13133
20 AUG 10 ICE AND RAIN PROTECTION - WINDSHIELD RAIN
PROTECTION - DEACTIVATE RAIN REPELLENT
SYSTEM
Applicable to: ALL
S13148
20 AUG 10 EQUIPMENT/FURNISHINGS - COCKPIT - INSTALL
NEW GENERATION OF SEATS
Applicable to: ALL
S13154
20 AUG 10 AUTO FLIGHT - FMGEC - INTRODUCE L6 STD FOR
CFMI
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S13179
20 AUG 10 AUTO FLIGHT - FLIGHT ENVELOPE - INSTALL
PLACARD SPEED VFE CONF. 1
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 15/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S13230
Applicable to: ALL
S13253
Linked SB
Incorp. Date
20 AUG 10
Title
NAVIGATION - TCAS - INSTALL IMPROVED ALLIED
SIGNAL II (-1208)
ELECTRICAL POWER - AC MAIN DISTRIBUTION
- ACTIVATE NEW GALLEY LOAD SHEDDING
PRINCIPAL
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S13267
20 AUG 10 NAVIGATION - WEATHER RADAR SYSTEM ACTIVATE ALLIED SIGNAL PREDICTIVE WINDSHEAR
FUNCTION
Applicable to: ALL
S13271
20 AUG 10 INDICATING/RECORDING SYSTEM-ELECTRONIC
INSTRUMENT SYSTEM (E.I.S.) - INSTALL DMC
SOFTWARE V509X WITH DMC B HARDWARE
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S13310
20 AUG 10 INFORMATION SYSTEMS - COCKPIT INFORMATION
SYSTEMS - INTRODUCE PROVISIONS FOR ATSU
AND DCDU
Applicable to: ALL
S13317
25 NOV 11 NAVIGATION - ADIRS - INSTALL HONEYWELL 4
MCU STANDARD ADIRU WITH NEW/OPTIMIZED
HARDWARE
Applicable to: B-18355
S13333
20 AUG 10 COMMUNICATIONS - AUDIO INTEGRATING - INSTALL
AMU FOR SATCOM
Applicable to: ALL
S13396
20 AUG 10 INDICATING/RECORDING SYSTEM-ELECTRONIC
INSTRUMENT SYSTEM (E.I.S.) - INSTALL DMC
SOFTWARE V109X WITH DMC B HARDWARE
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S13433
20 AUG 10 ENGINE FUEL AND CONTROL - GENERAL - PROVIDE
DERATED TAKE-OFF FACILITIES FOR G.E. ENGINES
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S13434
20 AUG 10 INDICATING/RECORDING SYSTEM - FWC - DEFINE
NEW OEB REMINDER FUNCTION
Applicable to: ALL
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 16/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S13455
Linked SB
Incorp. Date
Title
20 AUG 10
Applicable to: ALL
S13456
AUTO FLIGHT-FLIGHT CONTROL UNIT- ACTIVATE
AUTOMATIC ENGAGEMENT OF FLIGHT DIRECTOR
WITH CROSS BARS IN GO AROUND
20 AUG 10
Applicable to: ALL
S13472
INDICATING/RECORDING SYSTEMS-ANCILLARY
EQUIPMENT-INSTALL COCKPIT CLOCK CAPABLE OF
GPS TIME (AIR PRECISION)
20 AUG 10
Applicable to: ALL
S13495
LANDING GEAR - ALTERNATE BRAKING - REPLACE
BRAKE HYD PRESSURE INDICATOR
20 AUG 10
Applicable to: ALL
S13617
COMMUNICATION - SATCOM - ACTIVATE COCKPIT
VOICE WITH COLLINS SATCOM AVIONICS
20 AUG 10
Applicable to: ALL
S13629
HYDRAULIC POWER - MAIN HYDRAULIC POWERINTRODUCE PUSH BUTTON SWITCHES AND
SWITCHGUARDS ON HYDRAULIC CONTROL PANEL
20 AUG 10
Applicable to: ALL
S13632
OXYGEN - PORTABLE OXYGEN - INSTALL SCOTT
AVIATION P/N 802300-14 IN COCKPIT
20 AUG 10
Applicable to: ALL
S13634
NAVIGATION - ADF - INSTALL ADF RECEIVER
COLLINS 900 P/N 822-0299-020
20 AUG 10
Applicable to: ALL
S13661
NAVIGATION- ADF - INSTALL SECOND ADF
RECEIVER
20 AUG 10
Applicable to: ALL
S13669
NAVIGATION - MMR - INSTALL COLLINS
MULTI-MODE RECEIVERS PROVIDING ILS (FM
IMMUNE) AND GPS PRIMARY FUNCTION
20 AUG 10
ENGINE FUEL AND CONTROL - INCORPORATE
A330/GE DERATED CLIMB MODIFICATION
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S13796
20 AUG 10 AUTOFLIGHT-FCU-DEFINE LONG RANGE VERSION
OF MODULAR F.C.U.
Applicable to: ALL
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 17/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S13810
Linked SB
Incorp. Date
Title
20 AUG 10
Applicable to: ALL
S13829
FLIGHT CONTROLS-EFCS CONTROL INPUTS AND
POWER-INTRODUCE VISUAL AND AURAL INDIC.
FOR SIMULTANEOUS SIDE STICK ACTION
27 JUN 14
Applicable to: ALL
S13893
ELECTRICAL POWER -BATTERY DC GENERATORINSTALL NEW BCL STANDARD 6
20 AUG 10
Applicable to: ALL
S13916
OXYGEN - CREW OXYGEN - INSTALL A 115 CU.FT
COMPOSITE OXYGEN CYLINDER
20 AUG 10
ICE AND RAIN PROTECTION - WINDSHIELD RAIN
PROTECTION - REACTIVATE THE RAIN REPELLENT
SYSTEM
25 NOV 11
NAVIGATION - ADIRS - INTRODUCE HONEYWELL
ADIRU 4MCU STD HG 2030AD10
20 AUG 10
Applicable to: ALL
S14029
EQUIPMENT/FURNISHINGS - COCKPIT - APPLY
CABIN ATTENDANT SEAT DEFINITION TO FOURTH
OCCUPANT SEAT
20 AUG 10
Applicable to: ALL
S14071
AUTO FLIGHT - MCDU - INSTALL 2ND GENERATION
FMS MCDU (HONEYWELL)
20 AUG 10
Applicable to: ALL
S14080
NAVIGATION-ATC/MODE S-ATC/TCAS CONTROL
PANEL SEXTANT P/N C12404AB02-CORRECT ATC
CODE AT ELECTRICAL POWER TRANSFER
20 AUG 10
Applicable to: ALL
S13948
Applicable to: B-18355
S13998
34-3165 01
34-4166 01
ENGINE FUEL AND CONTROL-CONTROLLINGPROVIDE DERATED CLIMB FACILITY FOR CFMI
ENGINES
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14135
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS - DISPLAY
MANAGEMENT COMPUTER - INSTALL NEW DMC
SOFTWARE V510X
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14162
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS - DISPLAY
MANAGEMENT COMPUTER - INSTALL NEW DMC
SOFTWARE V110X
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 18/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S14174
Linked SB
Incorp. Date
Title
INDICATING/RECORDING SYSTEMS - CENTRAL
WARNING SYSTEMS - INSTALL NEW FWC
STANDARD K3-0
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14181
20 AUG 10 INDICATING/RECORDING SYSTEMS - FWC - INSTALL
NEW FWC STANDARD L7-0
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14196
20 AUG 10 FLIGHT CONTROLS - FCDC - INSTALL FCDC
STANDARD L15/M12
Applicable to: ALL
S14216
20 AUG 10 NAVIGATION - GPWS - INSTALL ENHANCED GPWS
Applicable to: ALL
S14218
20 AUG 10 NAVIGATION - GPWS - ACTIVATE ENHANCED GPWS
Applicable to: ALL
S14259
20 AUG 10 INDICATING/RECORDING SYSTEMS - MWS SYSTEM
- MODIFY WIRING BETWEEN "CTR TANK TRANSFER
P/B MAN" AND SDAC
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14273
20 AUG 10 AUTO FLIGHT - FMGEC - INSTALL FMGEC P1-B7 FOR
GE ENGINES
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14274
18 FEB 14 AUTO FLIGHT - FMGEC - INSTALL FMGEC P1-A8 FOR
CFMI ENGINES
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14282
20 AUG 10 AUTO FLIGHT - FCU - INTRODUCE FCU P/N -608
Applicable to: ALL
S14291
20 AUG 10 AIR CONDITIONING-AVIONICS EQUIPMENT GROUND
COOLING-IMPROVE GRU LOGICS
Applicable to: ALL
S14294
20 AUG 10 INDICATING/RECORDING SYSTEMS - FWC - INSTALL
FWC STANDARD K3.1
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14327
31-3034 11
20 AUG 10 INDICATING/RECORDING SYSTEMS-CENTRAL
31-4071 10
WARNING SYSTEMS-PROVIDE NEW AUTO
CALL-OUT CALLED "V1"
Applicable to: ALL
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 19/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S14334
Applicable to: ALL
S14440
Linked SB
Incorp. Date
20 AUG 10
Title
FIRE PROTECTION-PORTABLE FIRE
EXTINGUISHER-INSTALL WALTER KIDDE P/N 898052
IN AVIONICS COMPARTMENT
NAVIGATION-ILS-INSTALL SEXTANT MMR
PROVIDING ILS FM IMMUNE AND GPS C1
FUNCTIONS
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14445
20 AUG 10 AUTO FLIGHT MANAGEMENT-GUIDANCE AND
ENVELOPE COMPUTER-ACTIVATE AUTOFLIGHT
MODE SEQUENCE ALERTNESS
Applicable to: ALL
S14482
20 AUG 10 INFORMATION SYSTEMS - AIR TRAFFIC AND
INFORMATION MANAGEMENT SYSTEM - ACTIVATE
ATSU
Applicable to: ALL
S14521
20 AUG 10 NAVIGATION-TCAS-INSTALL ALLIED SIGNAL
CHANGE 7 P/N 066-50000-2220
Applicable to: ALL
S14561
20 AUG 10 INDICATING/RECORDING SYSTEM - FWC - INSTALL
NEW FWC STANDARD K3.2
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14566
07 APR 11 ELECTRICAL POWER - BATTERY DC GENERATION INTRODUCE NEW TECHNOLOGY
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
S14649
20 AUG 10 NAVIGATION - MMR - INSTALL COLLINS
MULTI-MODE RECEIVERS P/N 822-1152-121
Applicable to: ALL
S14666
20 AUG 10 ICE AND RAIN PROTECTION - WINDSHIELD
ANTI-ICING AND DEFOGGING - REPLACE THE RAIN
REPELLENT GAGE ASSY
Applicable to: ALL
S14682
20 AUG 10 FLIGHT CONTROLS -FLIGHT CONTROL PRIMARY
COMPUTER - INTRODUCE FCPC M12 FOR A330-300
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 20/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S14683
Linked SB
Incorp. Date
Title
FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY
COMPUTER - INTRODUCE FCPC P4/M12 FOR A330
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14722
34-3184 00
20 AUG 10 NAVIGATION - GPWS - MODIFY EGPWS VISUAL
34-4171 00
WARNING AND CAUTION INDICATIONS
Applicable to: ALL
S14736
20 AUG 10 AUTO FLIGHT - FMGEC - INSTALL A NEW STANDARD
FMGEC L9B6 FOR GE ENGINE
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14749
20 AUG 10 COMMUNICATIONS - HF SYSTEM - INSTALL A
"GROUND HF DATA LINK" PUSHBUTTON SWITCH
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14785
20 AUG 10 NAVIGATION-STANDBY NAVIGATION SYSTEMSINSTL SYST.PROV. FOR A SEXTANT AVIONICS
INTEGRATED STDBY INSTRUMENT SYST.(ISIS)
Applicable to: ALL
S14786
20 AUG 10 NAVIGATION-STANDBY NAVIGATION SYSTEMSINSTALL SEXTANT AVIONICS INTEGRATED
STANDBY INSTRUMENT SYSTEM (ISIS)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14800
20 AUG 10 NDICATING/RECORDING SYSTEMS-DFDRSRE-INSTALL WIRING PROVISIONS FOR QAR FOR
A340 A/C
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14804
20 AUG 10 ENGINE FUEL AND CONTROL - CONTROLLING INSTALL FADEC SOFTWARE STD C3G
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14838
20 AUG 10 ICE AND RAIN PROTECTION - WINDSHIELD
ANTI-ICE AND DEFFOGING - INSTALL A NEW RAIN
REPELLENT FLUID GAGE ASSY
Applicable to: ALL
S14847
20 AUG 10 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL NEW FWC
STANDARD L8-0
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 21/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S14859
Linked SB
Incorp. Date
Title
INDICATING/RECORDING SYSTEMS-ELECTRONIC
INSTRUMENT SYSTEM - INSTALL NEW DISPLAY
SYSTEM (EIS2) EQTS (DMC/DU/DISKETTES)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14942
20 AUG 10 INDICATING/RECORDING SYSTEMS - FWC
- ACTIVATE FUEL LEAK WARNING BY PIN
PROGRAMMING
Applicable to: ALL
S14947
20 AUG 10 OIL - STORAGE - A340 CFM56-5C - INTRODUCE
A NEW ENGINE OIL TANK COMMON WITH A320
CFM56-5A AND 5B
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S14950
23-4174 02
20 AUG 10 COMMUNICATIONS - RADIO MANAGEMENT INTRODUCE RMP STANDARD 2
Applicable to: ALL
S14956
20 AUG 10 ELECTRICAL POWER-GENERAL-INSTALL
ADDITIONAL ELECTRICAL OUTLETS IN COCKPIT
(110V/60HZ)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S14975
20 AUG 10 NAVIGATION-INTEGRATED STANDBY INDICATION
SYSTEM (ISIS)- ACTIVATE BARO-SETTING IN INCH
HG
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S15551
07 APR 11 INDICATING/RECORDING SYSTEMS - EIS ACTIVATE PREDICTIVE WINDSHEAR FUNCTION BY
PIN PROGRAMMING ON DMC
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S15556
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS ACTIVATE FUEL FLOW / DELTA ISA FUNCTION BY
PIN PROGRAMMING ON DMC.
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 22/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S15891
Applicable to: ALL
S16019
Linked SB
34-3188 00
34-4176 00
Incorp. Date
20 AUG 10
Title
NAVIGATION - EGPWS - USE LATERAL GPS
POSITION WITH AUTOMATIC DESELECTION
NAVIGATION-STANDBY NAVIGATION
SYSTEMS-PROVIDE DISPLAY OF METRIC ALTITUDE
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16061
20 AUG 10 AUTO FLIGHT - FMGEC - INSTALL FMGEC P1A9 FOR
CFMI ENGINES
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S16107
20 AUG 10 INFORMATION SYSTEMS - GENERAL - CERTIFY
FANS A CONFIGURATIONS
Applicable to: ALL
S16115
20 AUG 10 ENGINE FUEL AND CONTROL - FADEC SYSTEM INTRODUCE ECU E1L S/W ON CF6-80E1
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16200
34-4175 00
20 AUG 10 NAVIGATION - EGPWS - ACTIVATE GEOMETRIC
ALTITUDE FUNCTION
Applicable to: ALL
S16258
20 AUG 10 FUSELAGE - NOSE FORWARD FUSELAGE INTRODUCE STRUCTURAL PROVISIONS IN E/E BAY
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
S16262
34-4174 00
20 AUG 10 NAVIGATION - EGPWS - ACTIVATE OBSTACLE
FUNCTION
Applicable to: ALL
S16263
34-4174 00
20 AUG 10 NAVIGATION - EGPWS - ACTIVATE PEAKS
FUNCTION
Applicable to: ALL
S16279
20 AUG 10 FLIGHT CONTROLS - ELECTRICAL FLIGHT CONTROL
SYSTEM (EFCS) - INSTALL RUDDER FLY-BY WIRE
ON A330/A340
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 23/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S16286
Linked SB
Incorp. Date
Title
INDICATING/RECORDING SYSTEMS - FWC - INSTALL
NEW STANDARD K7
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16318
20 AUG 10 ELECTICAL POWER - GENERAL - INSTALL
EMERGENCY POWER CENTER 743 VU IN SECT
11/12
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16326
07 APR 11 ELECTRICAL POWER-GENERAL-INSTALL NEW
GAPCU STANDARD "4.3"
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16349
20 AUG 10 INDICATING/RECORDING SYSTEM - DMC - INSTALL
NEW DMC SOFTWARE V511X
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16354
20 AUG 10 INDICATING/RECORDING SYSTEMS - FWC REPLACE THE EXISTING STANDARD FWC BY A NEW
STD K6 FOR A330 - FAR 121-344
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16355
31-4067 01
20 AUG 10 INDICATING/RECORDING SYSTEMS - FWC REPLACE THE EXISTING STANDARD FWC BY A NEW
STD L9 FOR A340 - FAR 121-344
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S16400
46-3013 12
20 AUG 10 INFORMATION SYSTEMS - ATIMS - UPGRADE
A/C INTERFACE SOFTWARE FOR FANS A+
IMPLEMENTATION
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16420
34-3172 02
20 AUG 10 NAVIGATION-WEATHER RADAR SYSTEM-INSTALL
HONEYWELL DUAL CONTROL PANEL CAPABLE OF
THE AUTOTILT AND PWS FUNCTIONS
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 24/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S16499
Applicable to: B-18807
S16501
Linked SB
Incorp. Date
20 AUG 10
Title
NAVIGATION - ATC - INSTALL REMOTE ATC
CONTROL BOX
FLIGHT CONTROLS - FCPC - INTRODUCE NEW
P6/M14 SOFTWARE STD ON FCPC HARDWARE 2K1
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16538
29-4066 00
20 AUG 10 HYDRAULIC POWER - GREEN MAIN HYDRAULIC
POWER - INTRODUCE A NEW STD HYDRAULIC
SYSTEM MONITORING UNIT (HSMU STD-6)
Applicable to: ALL
S16544
20 AUG 10 ONBOARD MAINTENANCE SYSTEMS-UP AND DOWN
DATA LOADING SYSTEM - INSTALL DLS/DLRB AND
DLRB DISK BASIC CONFIGURATION
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16606
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS - INTALL
NEW EIS2 STANDARD L4 ON A330/A340 ENHANCED
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16620
20 AUG 10 FUSELAGE - GENERAL- ADAPT COCKPIT DOOR
REINFORCEMENT TO BASIC LR
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
S16635
20 AUG 10 NAVIGATION - ADF - REMOVE ADF SYSTEM 1 AND 2
(RECEIVERS AND ANTENNAS)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16651
22-4035 01
20 AUG 10 AUTO-FLIGHT - FMGEC - INSTALL FMGEC P2A10
FOR CFM ENGINES
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S16653
20 AUG 10 AUTO-FLIGHT - FMGEC - INSTALL FMGEC P2B7 FOR
GE ENGINES
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 25/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S16701
Linked SB
Incorp. Date
Title
NAVIGATION - ADF - INSTALL ADF1 900 COLLINS
RECEIVER
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16702
20 AUG 10 NAVIGATION - ADF - INSTALL ADF2 900 COLLINS
RECEIVER
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16729
25 NOV 11 ENGINE FUEL AND CONTROL - FUEL DISTRIBUTION
SYSTEM - INTRODUCE NEW FUEL FILTER ON
CFM56-5C ENGINES - CNF CFM 150
Applicable to: B-18807
S16753
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS - INSTALL
NEW EIS2 STANDARD L4-1 CAPABLE OF ALL LONG
RANGE AIRCRAFT
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16762
34-3165 01
20 AUG 10 NAVIGATION - ADIRS- INSTALL 4MCU ADIRS
34-4166 01
HONEYWELL (AE21)
Applicable to: ALL
S16795
20 AUG 10 FLIGHT CONTROL - FCPC - INTRODUCE NEW
SOFTWARE FCPC STANDARD P6A/M14A ON A330
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16804
34-3287 01
30 MAY 13 NAVIGATION - ADIRS - ACTIVATE IMPROVEMENT
34-4268 01
FUNCTION ON ADIRU
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359,
B-18360, B-18361, B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S16812
23-4174 02
20 AUG 10 COMMUNICATIONS-RADIO MANAGEMENT-INSTALL
NEW RMP STANDARD 2A
Applicable to: ALL
S16877
20 AUG 10 FLIGHT CONTROL - FLIGHT CONTROL PRIMARY
COMPUTER - INTRODUCE NEW FCPC STD "P7/M16"
FOR A330 ENHANCED
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 26/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S16961
Applicable to: ALL
S16975
Linked SB
Incorp. Date
22-3049 01
20 AUG 10
34-3184 00
34-4171 00
20 AUG 10
Title
NAVIGATION - EGPWS - INSTALL NEW EGPWC
AUTO-FLIGHT - FMGEC - INSTALL NEW FMGEC
STANDARD P2B8 (A330GE)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16983
46-3017 18
20 AUG 10 INFORMATION SYSTEMS - GENERAL - CERTIFY
FANS A+ CONFIGURATIONS (OVERALL
MODIFICATION)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S16985
00-3049 00
20 AUG 10 GENERAL-TECHNICAL INFO ,WEIGHT AND GC 00-4045 00
INCREASE MAXIMUM OPERATING ALTITUDE FROM
41100 TO 41450 FEET
Applicable to: ALL
S17202
20 AUG 10 ON BOARD MAINTENANCE SYSTEMS - CMC INSTALL NEW CMC STANDARD L6B
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S17467
34-3167 01
20 AUG 10 NAVIGATION - MMR - INSTALL A HONEYWELL MMR
(-1161) AND ASSOCIATED PGS ANTENNAS FOR
A340-500/600
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S17480
07 APR 11 NAVIGATION - ILS - INSTALL MMR COLLINS
A340-500/600 CERTIFICATION STANDARD (130)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S17489
27 JUN 14 ELECTRICAL POWER-BATTERY DC GENERATION INSTALL NEW BCL STANDARD 8
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 27/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S17494
Linked SB
Incorp. Date
Title
INDICATING/RECORDING SYSTEM - EIS - INSTALL
NEW EIS2 STANDARD L3-1 (DMC, DU AND DISKS)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S17765
20 AUG 10 HYDRAULIC POWER - GENERAL - IMPROVE THE
HSMU POWER SUPPLY ON GROUND SERVICING
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18807
S17826
25 NOV 11 PNEUMATIC - LEAK DETECTION - INSTALL A
SECOND LEAK SYSTEM DETECTION LOOP ON THE
APU BLEED AIR SYSTEM ON A330
Applicable to: B-18307, B-18308, B-18309, B-18310, B-18311, B-18312, B-18315, B-18316, B-18317, B-18351,
B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S17828
36-3030 01
20 AUG 10 PNEUMATIC - LEAK DETECTION - INSTALL BMC "M4"
STANDARD ON A330 A/C
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S17830
31-3066 00
20 AUG 10 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER - INSTALL NEW FWC
STANDARD K8 ON A330
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S17880
31-3069 01
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS INSTALL NEW EIS2 STD L5 TO INCREASE SYSTEM
ROBUSTNESS AND MATURITY
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S17889
07 APR 11 AUTO FLIGHT - FLIGHT CONTROL UNIT (FCU) ACTIVATE THE PIN PROGRAMMING FOR BARO
EXTENSION AT "1100PHA"
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S17964
29-3092 00
20 AUG 10 HYDRAULIC POWER-GROUND INTERNAL LEAK
29-4071 00
TEST SYSTEM - IMPROVE LEAK MEASUREMENT
VALVE WARNING SYSTEM ON A330, A340 A/C
Applicable to: ALL
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 28/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S18004
Linked SB
Incorp. Date
Title
NAVIGATION - STANDBY NAVIGATION SYSTEM INSTALL NEW ISIS STANDARD POST ISE
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18015
20 AUG 10 ENGINE FUEL AND CONTROL - FADEC SYSTEMINTRODUCE NEW ECU S/W STD "E1N" ON A330 A/C
WITH GE CF6-80E1 ENGINES
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18076
20 AUG 10 NAVIGATION - TCAS - INSTALL A NEW HONEYWELL
TCAS TPA 100A
Applicable to: B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311, B-18312, B-18315, B-18316,
B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S18084
34-3165 01
20 AUG 10 NAVIGATION-ADIRS : INSTALL NEW HONEYWELL
34-4166 01
ADIRU STANDARD - AE22
Applicable to: ALL
S18094
20 AUG 10 FLIGHT CONTROL - FLIGHT CONTROL PRIMARY
COMPUTER (FCPC) - INTRODUCE TRIM SETTING
AUTOMATIC FUNCTION
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S18144
34-3213 04
20 AUG 10 NAVIGATION-ADIRS-INTRODUCE AIR DATA
34-4213 02
MONITORING FUNCTION
Applicable to: ALL
S18168
20 AUG 10 AUTO-FLIGHT - MCDU - INSTALL 3 LCD MCDU
HONEYWELL
Applicable to: B-18317, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S18201
27-3148 01
07 APR 11 FLIGHT CONTROL-FLIGHT CONTROL PRIMARY
COMPUTER - INTRODUCE NEW FCPC STD P9/M18
ON 2K2 FOR A330
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18214
20 AUG 10 EQUIPMENT/FURNISHINGS -COCKPIT-INSTALL
SWITCH GUARD FOR 27 MQ ON 271VU
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18222
20 AUG 10 NAVIGATION - SWITCHING AND INDICATING REMOVE DDRMI INDICATORS
Applicable to: B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
20 AUG 10
PLP-LOM P 29/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S18244
Linked SB
Incorp. Date
Title
NAVIGATION - SWITCHING AND INDICATING REMOVE DDRMI PROVISION
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S18261
21-3112 01
20 AUG 10 FWC-ACQUISITION/INTERFACE CONNECT FWC
21-4121 01
TO RPWS TO PREVENT DOOR OPENING WITH
RESIDUAL CABIN PRESSURE
Applicable to: ALL
S18334
31-3087 00
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS - INSTALL
NEW EIS2 SOFTWARE L6
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18365
30 MAY 12 INDICATING/RECORDING SYSTEMS - SDAC INSTALL NEW SDAC STANDARD C8-0
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S18422
34-3192 00
20 AUG 10 NAVIGATION - ATC - CERTIFY EHS FUNCTION
34-4181 00
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360,
B-18361, B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
S18479
20 AUG 10 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER - DE-ACTIVE PIN PROG
ACTIVATED BY PM S13589
Applicable to: B-18306, B-18307, B-18308, B-18309, B-18310, B-18311, B-18312, B-18351, B-18353, B-18355
S18568
31-3104 02
20 AUG 10 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER - INSTALL FWC STANDARD
K9-486 ON A330
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18659
20 AUG 10 CERTIFICATION DOCUMENTS - GENERAL - CERTIFY
THE FLEX TEMPERATURE EXTENTION FOR A330
Applicable to: B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S18711
07 APR 11 AUTO-FLIGHT - MCDU - INSTALL NEW MCDU LCD
HONEYWELL (REBOND STANDARD)
Applicable to: B-18317, B-18353, B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S18714
22-3069 00
20 AUG 10 AUTO-FLIGHT - FMGEC - INSTALL NEW STANDARD
P3B8 (A330 GE)
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
07 APR 11
PLP-LOM P 30/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S18776
Linked SB
Incorp. Date
Title
31-3160 00
20 AUG 10 INDICATING/RECORDING SYSTEM - FWC 31-4143 00
ACTIVATE STATIC PRESSURE MONITORING
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361, B-18802, B-18803, B-18805, B-18806, B-18807
S18779
34-3219 31
20 AUG 10 NAVIGATION - ATC/MODE S (SELECT) CERTIFY
34-4223 18
ADS-B OUT CAPABILITY THROUGH EXTENDED
SUITTER 1090 MHZ
Applicable to: ALL
S18817
31-3104 02
20 AUG 10 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD T1-0
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18882
34-3204 01
20 AUG 10 NAVIGATION - DME - RELOCATE DME1 POWER
SUPPLY TO PROVIDE POWER IN EMERGENCY FOR
A330
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S18949
07 APR 11 INFORMATION SYSTEMS - AIRCRAFT INFORMATION
NETWORK SYSTEM - ACTIVATE SIU V5 STANDARD
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S19020
22-3056 01
20 AUG 10 AUTO FLIGHT - FMGEC - INSTALL NEW HONEYWELL
22-3081 00
PERFORMANCE DATA BASE (-905)
22-4049 01
Applicable to: ALL
S19212
20 AUG 10 NAVIGATION - RADIO MAGNETIC INFORMATION
SWITCHING AND INDICATING - RE-INSTALL DDRMI
P/N 63534-253-4
Applicable to: B-18353, B-18355
S19224
07 APR 11 EQUIPMENT/FURNISHINGS - COCKPIT - INTRODUCE
NEW 272VU AND NEW 275VU IN THE COCKPIT
OVERHEAD PANEL
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S19417
31-3125 01
20 AUG 10 INDICATING / RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INSTALL FWC
STANDARD T2-0.
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 31/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S30118
Linked SB
Incorp. Date
Title
AUTO FLIGHT - FMGEC - INSTALL NEW ENVE
HONEYWELL FMGEC STANDARD P3G0 BASED ON
NEW "GENEPI" HARDWARE ON A330 GE ENG.
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S30194
07 APR 11 INDICATING / RECORDING SYSTEMS - EIS - INSTALL
NEW EIS2 STANDARD L7.
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S30201
15 FEB 13 COMMUNICATIONS - AUDIO MANAGEMENT INSTALL NEW TEAM ACP SATCOM ACP2788AE01
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S30373
07 APR 11 NAVIGATION - TCAS - INSTALL TCAS HONEYWELL
TPA-100B CHANGE 7.1 CAPABLE OF ATSAW
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S30572
07 APR 11 ONBOARD MAINTENANCE SYSTEMS - CENTRAL
MAINTENANCE COMPUTER (CMC) - REMOVE CMC2
FROM LR BASIC CONFIG.
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S30619
31-3125 01
07 APR 11 INDICATING/RECORDING SYSTEMS - FWC ACTIVATE ON A330 A/C ENGINE FEEDLINE BURST
MONITORING FUNCTION ON FWC T2
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S30653
12 MAR 13 INDICATING/RECORDING SYSTEMS - DMC - INSTALL
ENHANCED DU INSTEAD OF EIS2 LCDU
Applicable to: B-18359, B-18360, B-18361
S30672
31-3146 02
20 AUG 10 INDICATING/RECORDING SYSTEMS - FWC - INSTALL
FWC STANDARD T3-0 ON LR A/C
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S30676
31-3140 01
07 APR 11 INDICATING/RECORDING SYSTEMS - SDAC /
31-4133 01
INTERFACE - INSTALL NEW STANDARD SDAC C9
Applicable to: ALL
S30716
27 JUN 14 ELECTRICAL POWER-BATTERY DC GENERATIONINSTALL NEW BCL (BATTERY CHARGE LIMITER)
STANDARD
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S30840
18 FEB 14 FLIGHT CONTROLS - FLIGHT CONTROL DATA
CONCENTRATOR (FCDC) - INSTALL NEW FCDC STD
L21 FOR ENHANCED LR
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
Continued on the following page
CAL A330/A340 FLEET
FCOM
18 FEB 14
PLP-LOM P 32/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
S30877
Linked SB
Incorp. Date
Title
COMMUNICATIONS - COCKPIT VOICE RECORDER
(CVR) - TRANSFER SSCVR POWER SUPPLY ON
28VDC
Applicable to: B-18355, B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S30945
30 MAY 12 INFORMATION SYSTEMS - ATIMS - INSTALL NEW
ATC FANS A+ APPLICATIONS FOR FANS A+ AND
DATALINK RECORDING FUNCTIONS
Applicable to: B-18358, B-18359, B-18360, B-18361
S30954
18 FEB 14 AUTO FLIGHT-FLIGHT MANAGEMENT,GUIDANCE
AND ENVELOPE COMPUTER (FMGEC) RE-INTRODUCE P3B8 STD GE
Applicable to: B-18355
S30958
04 OCT 11 INDICATING/RECORDING SYSTEMS - FWC INTRODUCE NEW FWC STANDARD T4 ON LR A/C
Applicable to: B-18356, B-18357, B-18358, B-18359, B-18360, B-18361
S31353
31-3154 00
07 APR 11 INDICATING RECORDING SYSTEMS - FWC 31-4141 00
ACTIVATE MONITORING OF ATC/XPDR FAULTS
Applicable to: ALL
S31639
30 MAY 13 COMMUNICATIONS - COCKPIT VOICE RECORDER
(CVR) - ACTIVATE DATALINK RECORDING
FUNCTION ON ATSU/SSCVR
Applicable to: B-18360, B-18361
S31661
27-3175 01
04 OCT 11 FLIGHT CONTROLS - FLIGHT CONTROL DATA
CONCENTRATOR (FCDC) - INSTALL NEW FCDC STD
L21 (LOW SPEED) FOR ENHANCED LR
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S31924
73-3055 01
30 MAY 12 ENGINE FUEL AND CONTROL - FADEC SYSTEMINST NEW ECU "E1P" SOFTWARE STANDARD ON
CF6 80-E1 ENGINES
Applicable to: B-18301, B-18302, B-18303, B-18305, B-18306, B-18307, B-18308, B-18309, B-18310, B-18311,
B-18312, B-18315, B-18316, B-18317, B-18351, B-18352, B-18353, B-18355, B-18356, B-18357, B-18358,
B-18359, B-18360, B-18361
S32159
18 FEB 14 INDICATING/RECORDING SYSTEMS - FLIGHT
WARNING COMPUTER (FWC) - INTRODUCE NEW
FWC STANDARD T5
Applicable to: B-18361
21-4143 02
30 MAY 12 AIR CONDITIONING - PACK CONTROL AND
INDICATING - INTRODUCE NEW PACK CONTROLLER
B-02
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806
Continued on the following page
CAL A330/A340 FLEET
FCOM
07 APR 11
PLP-LOM P 33/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
21-4144 01
Linked SB
Incorp. Date
Title
30 MAY 12
Applicable to: B-18807
21-4153 01
AIR CONDITIONING - PACK CONTROL AND
INDICATING - INTRODUCE NEW PACK CONTROLLER
C-05
18 FEB 14
Applicable to: B-18806
22-4053 02
AIR CONDITIONING - AVIONICS EQUIPMENT
GROUND COOLING - REMOVE THE GROUND
REFRIGERATION UNIT (GRU)
20 AUG 10
AUTO-FLIGHT - FMGEC - ACTIVATE A/C TYPE 2 FOR
A340-300B.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
22-4054 01
20 AUG 10 AUTO-FLIGHT - FMGEC - INSTALL NEW STANDARD
P3A11 (A340 CFMI).
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
27-4102 00
20 AUG 10 FLIGHT CONTROLS - FCPC - INTRODUCE NEW L16
SOFTWARE STD ON FCPC HARDWARE 2K1
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806
27-4117 01
20 AUG 10 FLIGHT CONTROL - FCPC - INTRODUCE NEW
SOFTWARE FCPC STANDARD L16-A2K1
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
27-4131 00
20 AUG 10 FLIGHT CONTROLS - FCPC - INTRODUCE NEW L18
SOFTWARE STD ON FCPC HARDWARE 2K0 OR 2K1.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
27-4144 00
20 AUG 10 FLIGHT CONTROLS - FLIGHT CONTROL PRIMARY
COMPUTER - INTRODUCE NEW FCPC STANDARDS
L20 2K0 AND L20 2K1.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
27-4168 01
28 NOV 12 FLIGHT CONTROLS - FLIGHT CONTROL DATA
CONCENTRATOR (FCDC) - INSTALL NEW FCDC STD
L20 FOR BASIC AIRCRAFT.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
27-4174 00
30 MAY 12 FLIGHT CONTROLS - FCPC - INTRODUCE FCPC L22A
2K1 OR FCPC L22A 2K0 FOR A340-200/300 BASIC A/C
WITH MECHANICAL RUDDER
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
31-4083 01
20 AUG 10 INDICATING/RECORDING SYSTEM - FWS - INSTALL
FWC PN LA2E0060D100000 (STD L10) (A340) WITH
386 CPU BOARD
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
31-4099 01
20 AUG 10 INDICATING/RECORDING SYSTEMS - EIS - INSTALL
NEW EIS1 STANDARD V111X ON A340.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
Continued on the following page
CAL A330/A340 FLEET
FCOM
PLP-LOM P 34/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
(1)
M
Continued from the previous page
MODIFICATION
31-4111 00
Linked SB
Incorp. Date
07 APR 11
Title
INDICATING/RECORDING SYSTEMS - FWC - INSTALL
NEW FWC STANDARD L10-1/386.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
31-4125 02
07 APR 11 INDICATING/RECORDING SYSTEMS - FWC - INSTALL
NEW FWC STANDARD L11-0 ON A340.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
31-4134 00
26 JUL 11 INDICATING/RECORDING SYSTEM - FWC - INSTALL
NEW FWC STANDARD L12
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
34-4158 00
20 AUG 10 NAVIGATION - ATC/MODES - DEACTIVATE RATC
FUNCTION.
Applicable to: B-18807
34-4198 01
20 AUG 10 NAVIGATION - DME - RELOCATE DME1 POWER
SUPPLY TO KEEP POWER SUPPLY IN CASE OF
TOTAL ENGINE FLAME OUT.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
36-4028 01
20 AUG 10 PNEUMATIC - LEAK DETECTION - INSTALL BMC "L6"
STANDARD ON A340 A/C.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
38-4046 05
20 AUG 10 WATER/WASTE - TOILET SYSTEM - DELETE THE
WASTE TANK BALANCING SYSTEM FOR A/C WITH
THREE TANKS.
Applicable to: B-18801, B-18802, B-18803, B-18805
38-4050 01
20 AUG 10 WATER/WASTE - TOILET SYSTEM - REMOVE
OPTIONAL THIRD WASTE TANK SYSTEM INCLUDING
BALANCING
Applicable to: B-18806, B-18807
73-4016 00
20 AUG 10 ENGINE FUEL AND CONTROL - FADEC - INTRODUCE
NEW ECU STANDARD C3J FOR CFM56-5C AND -5C/P
ENGINES
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
73-4017 00
20 AUG 10 ENGINE FUEL AND CONTROL - FADEC SYSTEM INTRODUCE NEW FADEC SOFTWARE STANDARD
"C3K" ON CFM56-5C ENGINES.
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
73-4020 00
20 JAN 15 ENGINE FUEL AND CONTROL - FADEC SYSTEM INTRODUCE NEW FADEC SYS SOFTWARE STD C3N
ON CFM56-5C ENGINES
Applicable to: B-18801, B-18802, B-18803, B-18805, B-18806, B-18807
(1) Evolution code : N=New, R=Revised, E=Effectivity
CAL A330/A340 FLEET
FCOM
PLP-LOM P 35/36
20 JAN 15
PRELIMINARY PAGES
LIST OF MODIFICATIONS
A330/A340
FLIGHT CREW
OPERATING MANUAL
Intentionally left blank
CAL A330/A340 FLEET
FCOM
PLP-LOM P 36/36
20 JAN 15
GENERAL INFORMATION
Intentionally left blank
GENERAL INFORMATION
PRELIMINARY PAGES
A330/A340
FLIGHT CREW
OPERATING MANUAL
TABLE OF CONTENTS
Main FCOM Changes..............................................................................................................................................A
FCOM Purpose........................................................................................................................................................ B
List of Effective Sections/Subsections (LESS) - Paper Only.................................................................................. C
List of Effective Operations Engineering Bulletins (LEOEB)...................................................................................D
List of Effective Documentary Units (LEDU) - Paper Only..................................................................................... E
List of Effective Temporary Documentary Units (LETDU) - Paper Only................................................................. F
Aircraft Allocation Table (AAT) - Paper Only..........................................................................................................G
List of Modifications (LOM) - Paper Only............................................................................................................... H
FCOM Use and Organization................................................................................................................................... I
FCOM Revisions...................................................................................................................................................... J
FCOM Format and Style Information - Paper Only................................................................................................ K
Abbreviations............................................................................................................................................................ L
CAL A330/A340 FLEET
FCOM
GEN-PLP-TOC P 1/2
30 JUN 15
GENERAL INFORMATION
PRELIMINARY PAGES
A330/A340
FLIGHT CREW
OPERATING MANUAL
TABLE OF CONTENTS
Intentionally left blank
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GENERAL INFORMATION
PRELIMINARY PAGES
A330/A340
SUMMARY OF HIGHLIGHTS
FLIGHT CREW
OPERATING MANUAL
Localization
Title
Toc
Index
ID
Reason
B
1
L
2
GEN
Abbreviations
L
3
GEN
Abbreviations
L
4
Remove the Flight Crew Bulletin (FCB) reference.
Documentation update: Deletion of text.
Remove the List of Effective Flight Crew Bulletin (LEFCB)
abbreviation.
Documentation update: Deletion of information.
Documentation update: Deletion of information.
Update of the "Abbreviations" list
The abbreviation "PNF" is replaced by "PM" (Pilot Monitoring). No
other technical change.
Deletion of the Product Structure Level (PSL) abbreviation.
Update of the "Abbreviations" list
GEN
FCOM Purpose
GEN
Abbreviations
CAL A330/A340 FLEET
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GENERAL INFORMATION
PRELIMINARY PAGES
A330/A340
FLIGHT CREW
OPERATING MANUAL
SUMMARY OF HIGHLIGHTS
Intentionally left blank
CAL A330/A340 FLEET
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GENERAL INFORMATION
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FLIGHT CREW
OPERATING MANUAL
MAIN FCOM CHANGES
Ident.: GEN-00013886.0001001 / 08 FEB 13
Applicable to: ALL
The purpose of the Main FCOM Changes is to provide Operators with general information about the
most significant changes that are introduced in the current revision of the manual.
The main FCOM changes are available on the Airbus World portal under the Flight Operations
community channel - Flight Operations Manuals - Main FCOM / FCTM / MMEL changes.
In addition, every revised Documentary Unit (DU) has a revision highlight (HL) that:
‐ Indicates the change(s) made to the DU
‐ Can be found in the associated “Preliminary Pages – Summary of Highlights” subchapter.
In addition to the Main FCOM Changes, the Modification Operational Impact (MOI) documents
available on the Airbus World portal (Flight Operations community channel - Operational Material Modification Operational Impact MOI) provide the operational impact linked to a MOD number.
FCOM PURPOSE
Ident.: GEN-00012540.0001001 / 20 JAN 15
Applicable to: ALL
FCOM PURPOSE
The Flight Crew Operating Manual (FCOM) is the support documentation for flight crews. It
provides them with the necessary information about the operational, technical, procedural,
and performance characteristics of the Long Range aircraft family, to ensure safe and efficient
operations of the aircraft during normal and abnormal/emergency situations, that may occur on
ground, or in flight.
The manual is not designed to provide basic jet aircraft piloting techniques, or information, that are
considered as basic airmanship for trained flight crews that are familiar with that type of aircraft
and with its general handling characteristics.
The FCOM is intended to be used:
‐ Directly as flight crew operating manual or to provide operators with a basis for their
development of a customized airline operations manual, in accordance with applicable
requirements
‐ As a comprehensive reference guide during initial and refresher Fight Crew Training.
Practical and training-oriented information is addressed in the Flight Crew Training Manual
(FCTM). Refer to FCTM/OP01-Introduction. Moreover, the FCOM is not intended to be used for
teaching basic piloting skills.
The Flight Crew Operating Manual complements the approved Airplane Flight Manual (AFM).
If the data contained in this manual differs from the data in the AFM, the AFM remains the
reference.
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30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
For any questions or comments related to this manual, the Operator’s Flight Operations
Management may contact the Airbus Flight Operations & Training support department.
1
FCOM CONTENTS
The contents of the FCOM are organized in the following four parts:
‐ System Descriptions (DSC, organized by ATA)
‐ Procedures
PRO ABN
: Abnormal/Emergency
PRO NOR SOP : Normal
PRO NOR SRP : System Related
PRO SPO
: Special Operations
PRO SUP
: Supplementary
‐ Limitations (LIM)
‐ Performance (PER, organized by phase of flight)
‐ Operations Engineering Bulletins (OEB)
DOCUMENTARY UNITS
The FCOM is made of Documentary Units (DU). The DU is the smallest part of information with a
technical content.
The DUs are listed on a separate "List of Effective Documentary Units" (LEDU). Refer to the
General section.
Note:
1. DUs can be grouped into Group of DU (GDU)
2. Temporary information may be provided via Temporary DU (TDU).
IDENTIFICATION STRIP
Below the title of the DU, the identification strip provides:
‐ The list of MSN the DU is applicable to
‐ For TDU, the reference to the DU impacted by the TDU.
LIST OF EFFECTIVE SECTIONS/SUBSECTIONS (LESS) - PAPER ONLY
Ident.: GEN-00013869.0001001 / 24 MAR 11
Applicable to: ALL
The List of Effective Sections/Subsections (LESS) summarizes all the sections and subsections
contained in the FCOM. For each revision, a new LESS is issued when at least one DU of the
section/subsection is changed.
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
The LESS consists of:
‐ The "M" field that may provide the following evolution code:
•
•
•
•
The "N" letter indicates a new section introduced by the revision
The "R" letter indicates a section in which the content has been revised
The "E" letter indicates an aircraft validity change within the section
The "M” letter indicates a section that have move within the FCOM
‐ The “Localization” field that allows localizing the section within the manual with the product
structure
‐ The “Subsection title” field
‐ The “Rev. Date” field that indicated the date at which the section was changed.
LIST OF EFFECTIVE OPERATIONS ENGINEERING BULLETINS (LEOEB)
Ident.: GEN-00013870.0001001 / 23 NOV 11
Applicable to: ALL
Refer to OEB-GEN Cross Reference Between the Former and New OEB Identifications
LIST OF EFFECTIVE DOCUMENTARY UNITS (LEDU) - PAPER ONLY
Ident.: GEN-00013872.0001001 / 24 MAR 11
Applicable to: ALL
For each revision, a new List of Effective Documentary Units (LEDU) is issued at the section level.
The LEDU provides information about the DU localization, applicability, identification and issue date.
The LEDU consists of:
‐ The "M" field that may provide the following Evolution Code:
• The "N" letter indicates a new DU introduced by the revision
• The "R" letter indicates a revised DU: The content of the DU is updated by the revision. A
vertical line in the margin of the DU locates the modified part
• The "E" letter indicates an aircraft validity change for the DU: The list of MSNs for which the DU
is effective has been changed compared to the previous LEDU, by addition or deletion of one or
several MSN
‐ The “Localization” field that allows localizing the DU in the manual with the product structure of the
manual
‐ The "T" field (Temporary Information) that contains a cross if the associated DU is a TDU
‐ The "DU title" that provides the title of the DU
‐ The “DU identification” that identifies the DU with its identification number or the GDU with its
code.
‐ The “DU date” that indicates when the DU has been released
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
‐ The DU criteria which lists the technical or operational criteria for which the DU and solution is
applicable to.
‐ The “Applicable to” which provides the list of aircraft this DU and solution is applicable to
‐ The "Impacted by TDU" which is the identification of the TDU superseding the DU
LIST OF EFFECTIVE TEMPORARY DOCUMENTARY UNITS (LETDU) - PAPER ONLY
Ident.: GEN-00013887.0001001 / 29 MAR 11
Applicable to: ALL
The List of Effective Temporary Documentary Units (LETDU) provides a summary of the Temporary
DU impacting the section.
The LETDU consists of:
‐ The "M" field that may provide the following Evolution Code:
• The "N" letter indicates a new TDU introduced by the revision
• The "R" letter indicates a revised TDU: The content of the TDU is updated by the revision. A
vertical line in the margin of the TDU locates the modified part
• The "E" letter indicates an aircraft validity change for the TDU: The list of MSNs the TDU is
applicable to has been changed compared to the previous LETDU, by addition or deletion of
one or several MSN
‐ The “Localization” field that allows localizing the TDU in the manual with the product structure of
the manual
‐ The “TDU Title” that provides the title of the TDU
‐ The “TDU identification” that identifies the TDU with its identification number with its own unique
code
‐ The “TDU date” that indicates when the TDU has been released
‐ The TDU criteria which lists the technical or operational criteria, the it is applicable to
‐ The “Applicable to” which provides the list of aircraft this TDU is applicable to
‐ The “Impacted DU” which is the Identification of DU superseded by the TDU
‐ The “Reason for issue” of the TDU
Note:
1. TDU is displayed on a yellow background.
2. Within the QRH the TDU replaces the impacted DU.
AIRCRAFT ALLOCATION TABLE (AAT) - PAPER ONLY
Ident.: GEN-00013888.0001001 / 24 MAR 11
Applicable to: ALL
The Aircraft Allocation Table (AAT) provides a view of the fleet covered in the FCOM. For each
aircraft, the AAT provides its MSN, its registration number and the model.
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
LIST OF MODIFICATIONS (LOM) - PAPER ONLY
Ident.: GEN-00013889.0001001 / 25 MAR 11
Applicable to: ALL
The List of Modifications (LOM) lists the criteria (Modification Proposal (MP) or Service Bulletins
(SB)) which the installation on the aircraft affects the FCOM.
Note:
Each MP has one or more associated MODs. The MP/MOD correlation is available in
AirN@v / Engineering.
The LOM also indicates:
‐ The title of the criteria
‐ The date of incorporation of the criteria in the FCOM
‐ The list of aircraft that have the criteria
‐ The "M" field that may indicate the following evolution code:
‐ The "E" letter indicates an aircraft validity change of the criteria. The list of aircraft to which the
criteria applies has changed compared to the previous FCOM revision, by addition or deletion of
one or several aircraft.
‐ The "N" letter indicates new criteria added by this FCOM revision
‐ The "R" letter indicates a change in the criteria title or associated SB.
FCOM USE AND ORGANIZATION
Ident.: GEN-00012542.0001001 / 24 MAR 11
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.
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
INFORMATION TYPE AND LAYERS
The FCOM has technical information that may be used for:
‐ Flight crew operations in flight, or on ground
‐ Airlines operations on ground
‐ Training.
To take the above-noted objectives into account, the FCOM is organized in three layers as follows:
‐ Layer 1: "Need to know"
Layer 1 presents information that is necessary in the cockpit.
‐ Layer 2: "Nice to know"
Layer 2 presents information that is used as a reference, in order to fully understand the logic of
the aircraft and pilot interfaces.
‐ Layer 3: Detailed information
Layer 3 provides more detailed explanations, that are not necessarily needed in flight.
Note:
For paper only, the following examples show the visual characteristics of each kind of
layer
EXAMPLE
L2
EXAMPLE
L3
EXAMPLE
L1
EXAMPLE
‐ Text in layer 1
Layer 1 is the default layer. No symbology when not following layer 2 or layer 3
information.
‐ Text in layer 2
‐ Text in layer 3
‐ Text in layer 1 (as this text follows a text in layer 2 or 3, symbology "L1")
OPTIONAL EQUIPMENT
The legend  (if installed) indicates that a paragraph or a schematic is applicable only if the
related equipment is installed.
FCOM REVISIONS
Ident.: GEN-00012546.0001001 / 20 JAN 15
Applicable to: ALL
FCOM REVISION
FCOM revisions are issued to add, update, or revise information. The Operator determines the
revision periodicity.
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GEN P 6/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
When necessary, a revision may be issued in between the defined periodicity (e.g. need for urgent
update).
A vertical bar appears to the left of all revised parts of the manual.
TEMPORARY INFORMATION
Some FCOM sections may need a temporary update (e.g. to explain a system behavior that will
be modified by a future standard). In such cases, the applicable FCOM section is updated with a
Temporary Documentary Unit (TDU).
Information contained in the TDU is highlighted in the manual and the initial content of the FCOM
remains available for consultation and comparison and is highlighted (identification strip) as being
impacted by the TDU.
A List of Effective Documentary Units (LEDU) is provided in the FCOM.
OPERATIONS ENGINEERING BULLETINS
Operations Engineering Bulletins (OEB) are issued, when it is necessary, to rapidly transmit
technical and procedural information.
The OEB chapter provides a list of all applicable OEBs.
FCOM FORMAT AND STYLE INFORMATION - PAPER ONLY
Ident.: GEN-00013880.0001001 / 20 JAN 15
Applicable to: ALL
TABLE OF CONTENTS
Each TOC entry has an alphabetical index that identifies this TOC entry within its subsection. The
manual user can easily find a TOC entry content within the manual thanks to this alphabetical
index and the subsection identification. Both are indicated in the TOC and both cross-refer to the
paper page footer (see the TOC indexing part below).
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
HEADER AND FOOTER
CAL A330/A340 FLEET
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←K→
GEN P 8/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
1. Airline logo
2. Aircraft types and manual
3. Level 2 chapter (Section level 2 : GEN, DSC, PRO, LIM, OEB, PER)
4. Level 3 chapter
5. Level 4 chapter
6. Revision mark
7. Key product (document identification and aircraft designation)
8. Key product (manual code)
9. Page index
10. Last evolution date
11. Identification strip (list of impacted aircraft)
12. Section path
REVISION MARK
In the paper format, a vertical bar in the margin of the DU identifies the modified part. Each
vertical bar has a numerical index that refers to the associated reason of the change in the
Summary of Highlight.
This Summary of Highlight lists all the changes and associated reasons of the change (if
necessary) that the revision has introduced.
TOC INDEXING
In the paper page footer, the TOC indexing is of the following type:
A
: The paper page contains the whole "A" TOC entry content
A to B
: The paper page contains the whole "A" and "B" TOC entries contents
A→
: The "A" TOC entry content starts on this paper page and continues on
the following paper page
←A
: The "A" TOC entry content starts on a previous paper page and finishes
on this paper page
←A→
: The "A" TOC entry content starts on a previous paper page and
continues on the following paper page
A to C→
: The paper page contains the whole "A" and "B" TOC entries contents
but the "C" TOC entry content starts on this paper page and continues
on the following paper page
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
← A to C
:
← A to C →
:
Note:
The paper page contains the whole "B" and "C" TOC entries contents
but the "A" TOC entry content starts on a previous paper page and
finishes on this paper page
The paper page contains the whole "B" TOC entry content but the "A"
TOC entry content starts on a previous paper page and finishes on this
paper page and the "C" TOC entry content starts on this paper page and
continues on the following paper page
1. The indexes follow the alphabetical order: A, B, C, ..., Z, AA, AB, AC, ..., AZ, BA,
BB, BC, ...
2. For each subsection, the index starts again from A.
3. When a TOC entry content continues on the following paper page, the text
"Continued on the following page" is also indicated.
ABBREVIATIONS
Ident.: GEN-00012475.0001001 / 20 JAN 15
Applicable to: ALL
A
Abbreviation
A
A/BRK
A/C
A/P
AP
A/S
A/SKID
A/THR
AA
AAP
AAR
AAT
AB
ABN
ABV
AC
ACARS
ACAS
ACC
ACCEL
ACCU
Term
Amber
Autobrake
Aircraft
Autopilot
Autopilot
Airspeed
Anti-skid
AutoThrust
Airworthiness Authorities
Aft Attendant Panel
Air to Air Refueling
Aircraft Allocation Table
Abort
Abnormal
Above
Alternating Current
ARINC Communication Addressing and Reporting System
Airborne Collision Avoidance System
Active Clearance Control
Acceleration
Accumulator
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GEN P 10/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
ACMS
ACP
ACQ
ACT
ADF
ADIRS
ADIRU
ADM
ADR
ADS
ADS-B
ADV
AEVC
AFIS
AFM
AFS
AGL
AIDS
AIL
AIME
AINS
AIP
AIRB
ALT
ALTN
AMI
AMJ
AMU
ANSU
ANT
AOA
AOC
APP
APPR
APPU
APU
AR
ARINC
ARN
ARPT
Term
Aircraft Condition Monitoring System
Audio Control Panel
Acquire
Additional Center Tank
Automatic Direction Finder
Air Data Inertial Reference System
Air Data Inertial Reference Unit
Air Data Module
Air Data Reference
Air Data System
Automatic Dependance Surveillance - Broadcast
Advisory
Avionic Equipment Ventilation Controller
Airbus in-Flight Information Services
Airplane Flight Manual
Auto Flight System
Above Ground Level
Aircraft Integrated Data System
Aileron
Autonomous Integrity Monitoring Extrapolation
Aircraft Information Network System
Attendant Indication Panel
Airborne
Altitude
Alternate
Airline Modifiable Information
Advisory Material Joint
Audio Management Unit
Aircraft Network Server Unit
Antenna
Angle Of Attack
Airline Operational Control
Approach
Approach
Assymetry Position Pick-off Unit
Auxiliary Power Unit
Authorization Required
Aeronautical Radio Incorporated
Aircraft Registration Number
Airport
CAL A330/A340 FLEET
FCOM
←L→
Continued from the previous page
Continued on the following page
GEN P 11/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
ARS
ASAP
ASI
ATA
ATC
ATIS
ATSAW
ATSU
ATT
AUTO
AVNCS
AWY
Automatic Retraction System
As Soon As Possible
Air Speed Indicator
Air Transport Association of America
Air Traffic Control
Airbus Technical Information System
Airborne Traffic Situational Awareness
Air Traffic Service Unit
Attitude
Automatic
Avionics
Airway
Term
Continued from the previous page
B
Abbreviation
B/C
BARO
BAT
BBAND
BCL
BCM
BCRC
BCU
BEFPR
BITE
BMC
BNR
BRG
BRK
BRT
BSCU
BTC
BTL
Term
Back Course
Barometric
Battery
Broadband
Battery Charge Limiter
Back-up Control Module
Bulk Crew Rest Compartment
Backup Control Unit
Break-Even Fuel Price Ratio
Built-In Test Equipment
Bleed Monitoring Computer
Binary
Bearing
Brake
Bright
Braking Steering Control Unit
Bus Tie Contactor
Bottle
C
C/B
CB
CCD
C/L
Abbreviation
Term
Circuit Breaker
Circuit Breaker
Cursor Control Device
Checklist
CAL A330/A340 FLEET
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Continued on the following page
←L→
GEN P 12/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
CL
CAB
CAM
CAPT
CAS
CAT
CBMU
CCOM
CCRC
CDL
CDLS
CDSS
CDU
CED
CF
CG
CHG
CHK
CI
CIDS
CINS
CKPT
CLB
CLR
CLSD
CM1
CM2
CMC
CMD
CMM
CMPTR
CMS
CMS
CNTOR
CO
CO RTE
COM
COND
CONF
CONT
Checklist
Cabin
Cabin Assignment Module
Captain, Capture
Calibrated Airspeed
Category
Circuit Breaker Monitoring Unit
Cabin Crew Operating Manual
Cabin Crew Rest Compartment
Configuration Deviation List
Cockpit Door Locking System
Cockpit Door Surveillance System
Control Display Unit
Cooling Effect Detector
Cost of Fuel
Center of Gravity
Change
Check
Cost Index
Cabin Intercommunication Data System
Cabin Information Network System
Cockpit
Climb
Clear
Closed
Crewmember 1 (left seat)
Crewmember 2 (right seat)
Central Maintenance Computer
Command
Calibration Memory Module
Computer
Central Maintenance System
Constant Mach Segment
Contactor
Company
Company Route
Communication
Conditioning
Configuration
Continuous
CAL A330/A340 FLEET
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Term
Continued from the previous page
Continued on the following page
GEN P 13/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
CPC
CPCS
CPCU
CRC
CRG
CRS
CRT
CRZ
CSAS
CSM/G
CSTR
CT
CTL
CTL PNL
CTLR
CTR
CUDU
CVR
Cabin Pressure Controller
Cabin Pressure Control System
Cabin Pressure Controller Unit
Continuous Repetitive Chime
Cargo
Course
Cathode Ray Tube
Cruise
Conditioned Service Air System
Constant Speed Motor/Generator
Constraint
Cost of Time
Control
Control Panel
Controller
Center
Current Unbalance Detection Unit
Cockpit Voice Recorder
Term
Continued from the previous page
D
Abbreviation
DA
DAR
DC
DCDU
DCLB
DDRMI
DECEL
DES
DEST
DET
DEU
DFDR
DH
DIR
DIR TO
DISC
DISCH
DIST
DMC
Drift Angle
Digital AIDS Recorder
Direct Current
Datalink Control and Display Unit
Derated Climb
Digital Distance and Radio Magnetic Indicator
Deceleration
Descent
Destination
Detection
Decoder/Encoder Unit
Digital Flight Data Recorder
Decision Height
Direction
Direct To
Disconnect
Discharge
Distance
Display Management Computer
CAL A330/A340 FLEET
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←L→
Term
Continued on the following page
GEN P 14/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
DME
DMU
DN
DSCS
DSDL
DTG
DTMS
DTO
DU
DU
Distance Measuring Equipment
Data Management Unit (Aids)
Down
Door Slide Control System
Dedicated Serial Data Link
Distance To Go
Damage Tolerance Monitoring System
Derated Takeoff
Display Unit
Documentary Unit
Term
Continued from the previous page
E
Abbreviation
E/WD
EWD
EBCU
ECAM
ECAS
ECB
ECMU
ECON
ECP
ECS
ECU
EDP
EEC
EFB
EFCS
EFIS
EFOB
EGPWS
EGT
EIS
EIU
EIVMU
ELAN
ELEC
ELEV
ELMU
ELT
Term
Engine/Warning Display
Engine/Warning Display
Emergency Braking Control Unit
Electronic Centralized Aircraft Monitoring
Emergency Cockpit Alerting System
Electronic Control Box (APU)
Elec Contactor and Management Unit
Economic
ECAM Control Panel
Environmental Control System
Engine Control Unit
Engine-Driven Pump
Engine Electronic Control
Electronic Flight Bag
Electronic Flight Control System
Electronic Flight Instruments System
Estimated Fuel On Board
Enhanced Ground Proximity Warning System
Exhaust Gas Temperature
Electronic Instruments System
Engine Interface Unit
Engine Interface and Vibration Monitoring Unit
Ethernet Local Area Network
Electricity
Elevator, Elevation
Electrical Load Management Unit
Emergency Locator Transmitter
CAL A330/A340 FLEET
FCOM
←L→
Continued on the following page
GEN P 15/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
EMER
EMER GEN
ENG
EO
EPE
EPGS
EPR
EPU
EPU
EROPS
ESS
EST
ETA
ETE
ETOPS
ETP
ETT
EXT PWR
EXTN
Term
Continued from the previous page
Emergency
Emergency Generator
Engine
Engine-Out
Estimated Position Error (equal to EPU)
Electrical Power Generation System
Engine Pressure Ratio
Emergency Power Unit
Estimated Position Uncertainty (equal to EPE)
Extended Range Operation
Essential
Estimated
Estimated Time of Arrival
Estimated Time Enroute
Extended Twin Operations
Equal Time Point
Estimated Time for Takeoff
External Power
Extension
F
Abbreviation
F
FAA
FAP
F/C
F/D TEMP CTL
F/O
FO
FADEC
FAF
FAP
FAR
FAV
FCDC
FCMC
FCMS
FCOM
FCRC
FCTM
Fuel
Federal Aviation Administration
Forward Attendant Panel
Flight Crew
Flight Deck Temperature Control
First Officer
First Officer
Full Authority Digital Engine Control System
Final Approach Fix
Forward Attendant Panel
Federal Aviation Regulations
Fan Air Valve
Flight Control Data Concentrator
Fuel Control and Monitoring Computer
Fuel Control and Monitoring System
Flight Crew Operating Manual
Flight Crew Rest Compartment
Flight Crew Training Manual
CAL A330/A340 FLEET
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←L→
Term
Continued on the following page
GEN P 16/30
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GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
FCU
FD
FDIU
FDU
FE
FEP
FF
FG
FIDS
FL
FLHV
FLP
FLRS
FLS
FLT
F/CTL
FLT CTL
FLX TO
FM
FMA
FMGC
FMGEC
FMGES
FMGS
FMS
FOB
FOM
FPA
F-PLN
FPPU
FPD
FPR
FPV
FQI
FREQ
FRV
FSV
FU
FWC
FWD
FWS
Term
Continued from the previous page
Flight Control Unit
Flight Director
Flight Data Interface Unit
Fire Detection Unit
Flight Envelope
Final End Point
Fuel Flow
Flight Guidance
Fault Isolation and Detection System
Flight Level
Fuel Lower Heating Value
Flap
Flap Load Relief System
FMS Landing System
Flight
Flight Control
Flight Control
Flexible Take-Off
Flight Management
Flight Mode Annunciator
Flight Management and Guidance Computer
Flight Management Guidance and Envelope Computer
Flight Management Guidance and Envelope System
Flight Management and Guidance System
Flight Management System
Fuel On Board
Figure Of Merit
Flight Path Angle
Flight Plan
Feedback Position Pick-off Unit
Flight Path Director
Fuel Price Ratio
Flight Path Vector
Fuel Quantity Indication
Frequency
Fuel Return Valve
Fuel Shutoff Valve
Fuel Used
Flight Warning Computer
Forward
Flight Warning System
CAL A330/A340 FLEET
FCOM
←L→
GEN P 17/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
G
Abbreviation
G/S
GA
GAPCU
GCU
GDU
GE
GEN
GES
GLC
GLS
GMT
GND
GPCU
GPIRS
GPRS
GPS
GPSSU
GPU
GPWC
GPWS
GRND
GRU
GRVTY
GS
GSM
GW
Term
Glideslope
Go-Around
Ground and Auxiliary Power Control Unit
Generator Control Unit
Group of Documentary Unit
General Electric
Generator
Ground Earth Station
Generator Line Contactor
GNSS Landing System
Greenwich Mean Time
Ground
Ground Power Control Unit
Global Positioning and Inertial Reference System
General Packet Radio Service
Global Positioning System
Global Positioning System Sensor Unit
Ground Power Unit
Ground Proximity Warning Computer
Ground Proximity Warning System
Ground
Ground Refiguration Unit
Gravity
Ground Speed
Global System for Mobile Communication
Gross Weight
H
Abbreviation
HCU
HDG
HDG/S
HF
HI
HIL
HLD
HM
HMU
HP
Hydraulic Control Unit
Heading
Heading Selected
High Frequency
High
Hold Item List
Hold
Holding Pattern with a Manual Termination
Hydrau-Mechanical Unit
High Pressure
CAL A330/A340 FLEET
FCOM
←L→
Term
Continued on the following page
GEN P 18/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
HPA
HPTCC
HPV
HSMU
HUD
HYD
Hectopascal
High Pressure Turbine Clearance Control
High Pressure Valve
Hydraulic System Monitoring Unit
Head Up Display
Hydraulic
Term
Continued from the previous page
I
Abbreviation
I/O
I/P
IAS
IATA
ICAO
IDENT
IDG
IFE
IFR
IGGS
IGN
ILS
IMM
INB
INBO
INCREM
INIT
INOP
INR
INST
INTCP
INV
IP
IPPU
IR
IRS
ISA
ISO
ISOL
ISPSS
ISPSU
ITP
Inputs/Outputs
Input or Intercept Profile
Indicated Airspeed
International Air Transport Association
International Civil Aviation Organization
Identification
Integrated Drive Generator
In Flight Entertainment
Instrument Flight Rules
Inert Gas Generation System
Ignition
Instrument Landing System
Immediate
Inbound
Inboard
Increment
Initialization
Inoperative
Inner
Instrument
Intercept
Inverter
Intermediate Pressure
Instrumentation Position Pick-off Unit
Inertial Reference
Inertial Reference System
International Standard Atmosphere
International Organization for Standardization
Isolation
In Seat Power Supply System
In-Seat Power Supply Unit
In Trail Procedure
CAL A330/A340 FLEET
FCOM
←L→
Term
GEN P 19/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
J
JAR
Abbreviation
Joint Airworthiness Requirements
Term
K
2
Abbreviation
Term
Abbreviation
L
L/G
LAF
LAN
LAT
LAT REV
LAV
LCD
LCN
LD
LDA
LDG
LED
LEDU
LEOEB
LESS
LF
LGCIU
LH
LIB
LIM
LK
LO
LOC
LONG
LP
LPC
LPTCC
LRU
LS
LSK
LT
Term
Left
Landing Gear
Load Alleviation Function
Local Area Network
Latitude
Lateral Revision
Lavatory
Liquid Crystal Display
Load Classification Number
Lower Deck
Localizer Directional Aid
Landing
Light Emiting Diode
List of Effective Documentary Units
List of Effective Operations Engineering Bulletins
List of Effective Section/Subsections
Low Frequency
Landing Gear Control and Interface Unit
Left-Hand
Loudspeaker and Indicator Box
Limitation
Lock
Low
Localizer
Longitude
Low Pressure
Low Pressure Compressor
Low Pressure Turbine Clearance Control
Line Replaceable Unit
Loudspeaker
Line Select Key
Light
L
CAL A330/A340 FLEET
FCOM
←L→
Continued on the following page
GEN P 20/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
LTS
LVL
LVL/CH
LVR
LW
Term
Load and Trim Sheet
Level
Level Change
Lever
Landing Weight
Continued from the previous page
M
Abbreviation
MABH
MAC
MAG
MAG DEC
MAG VAR
MAINT
MAN
MAP
MAX
MAX CLB
MAX DES
MAX END
MC
MCDU
MCT
MD
MDA
MDCC
MDDU
MDH
MEA
MECH
MED
MEL
MFA
MIN
MKR
MLA
MLS
MLW
MMEL
MMO
Minimum Approach Break-off Height
Mean Aerodynamic Chord
Magnetic
Magnetic Declination
Magnetic Variation
Maintenance
Manual
Missed Approach Point
Maximum
Maximum Climb
Maximum Descent
Maximum Endurance
Master Caution
Multipurpose Control and Display Unit
Maximum Continuous Thrust
Main Deck
Minimum Descent Altitude
Main Deck Cargo Compartment
Multifunction Disk Drive Unit
Minimum Descent Height
Minimum En Route Altitude
Mechanic
Medium
Minimum Equipment List
Memorized Fault Annunciator
Minimum
Marker
Maneuver Load Alleviation
Microwave Landing System
Maximum Landing Weight
Master Minimum Equipment List
Maximum Operating Mach
CAL A330/A340 FLEET
FCOM
←L→
Term
Continued on the following page
GEN P 21/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
MMR
MN
MNPS
MORV
MPFAP
MSA
MSG
MSL
MTBF
MTOW
MW
MZFW
Term
Continued from the previous page
Multi Mode Receiver
Mach number
Minimum Navigation Performance Specification
Mixer Overpressure Relief Valve
Multi Purpose Flight Attendant Panel
Minimum Safe Altitude
Message
Mean Sea Level
Mean Time Between Failure
Maximum Takeoff Weight
Master Warning
Maximum Zero Fuel Weight
N
N/A
NA
N1
Abbreviation
N2
N3
NACA
NAV
NAVAID
NBPT
NCD
ND
NDB
NORM
NW
NWS
Term
Not Applicable
Not Applicable
Low Pressure Rotor Speed (in %)
Intermediate Pressure Rotor Speed (in %) for Rolls Royce Engines
High Pressure Rotor Speed (in %) for Other Engines
High Pressure Rotor Speed (in %) for Rolls Royce Engines
National Advisory Committee for Aeronautics
Navigation
Navigation Aid
No Break Power Transfer
Non Computed Data
Navigation Display
Non Directional Beacon — Nav Database
Normal
Nosewheel
Nosewheel Steering
O
Abbreviation
O/P
OANS
OAT
OBRM
OEB
OFF/R
Output
On-board Airport Navigation System
Outside Air Temperature
On Board Replaceable Module
Operations Engineering Bulletin
Off Reset
CAL A330/A340 FLEET
FCOM
←L→
Term
Continued on the following page
GEN P 22/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
OFST
OIS
OIT
OMTS
OP
OPP
OPS
OPT
OUTB
OUTR
OVBD
OVHD
OVHT
OVRD
OVSPD
OXY
3
Offset
Onboard Information System
Onboard Information Terminal
On-Board Mobile Telephony System
Open
Opposite
Operations
Optimum
Outbound
Outer
Overboard
Overhead
Overheat
Override
Overspeed
Oxygen
Term
Continued from the previous page
P
Abbreviation
P/N
PN
PA
P-ALT
PAX
PBE
P-CLB
P-DES
PDB
PED
PERF
PES
PF
PFD
PHC
PIM
P-MACH
PMV
PM
PNL
POB
Part Number
Part Number
Passenger Address
Profile Altitude
Passenger
Protective Breathing Equipment
Profile Climb
Profile Descent
Performance Data Base
Pedestal
Performance
Passenger Entertainment System
Pilot Flying
Primary Flight Display
Probes Heat Computer
Programming and Indication Module
Profile Mach
Pressure Maintenance Valve
Pilot Monitoring
Panel
Pressure Off Brake
CAL A330/A340 FLEET
FCOM
←L→
Term
Continued on the following page
GEN P 23/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
POS
PPOS
PR
PRAM
PRED
PRESS
PRIM
PROC
PROC T
PROF
PROG
PROT
PRV
PSCU
P-SPEED
PT
PTLU
PTT
PVI
PW
PWR
PWS
Position
Present Position
Pressure
Prerecorded Announcement and Music
Prediction
Pressure, Pressurization
FLT CTL Primary Computer (FCPC)
Procedure
Procedure Turn
Profile
Progress
Protection
Pressure Regulating valve
Proximity Switch Control Unit
Profile Speed
Point
Pedal Travel Limiter Unit
Push To Talk
Paravisual Indicator
Pratt & Whitney
Power
Portable Water System
Term
Continued from the previous page
Q
Abbreviation
QAR
QCCU
QFE
QFU
QNE
QNH
QRH
QT
QTY
Term
Quick Access Recorder
Quantity Calculation and Control Unit
Field Elevation Atmosphere Pressure
Runway Heading
Sea Level Standard Atmosphere Pressure (1013 hPa)
Sea Level Atmosphere Pressure
Quick Reference Handbook
Quart (US)
Quantity
R
R
R/I
RA
Abbreviation
Term
Right
Radio/Inertial
Radio Altimeter
CAL A330/A340 FLEET
FCOM
Continued on the following page
←L→
GEN P 24/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
RA
RACSB
RAD
RAIM
RAT
RATC
RCDR
RCL
RCVR
REAC
REC
RED
REF
REG
REL
REV
RH
RMI
RMP
RNAV
RNG
RNP
RPCU
RPLNT
RPM
RPTG
RQRD
RR
RSV
RSVR
RTE
RTL
RTO
RTOW
RUD
RVSM
RWY
Resolution Advisory
Rotor Active Clearance Control Start Bleed
Radio
Receiver Autonomous Integrity Monitoring
Ram Air Turbine
Remote ATC Box
Recorder
Recall
Receiver
Reactive
Recovery, Recommended
Reduction
Reference
Regulation
Release
Reverse
Right-Hand
Radio Magnetic Indicator
Radio Management Panel
Area Navigation
Range
Required Navigation Performance
Residual Pressure Control Unit
Repellent
Revolution Per Minute
Repeating
Required
Rolls Royce
Reserves
Reservoir
Route
Rudder Travel Limit
Rejected Takeoff
Regulatory Takeoff Weight
Rudder
Reduced Vertical Separation Minimum
Runway
CAL A330/A340 FLEET
FCOM
←L→
Term
Continued from the previous page
GEN P 25/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
S
Abbreviation
S
S/C
S/D
S/D
S/F
S/N
SN
SAAAR
SAE
SAT
SATCOM
SC
SCP
SD
SDAC
SDCU
SDF
SEC
SFCC
SFE
SID
SIM
SIU
SLFT (-PM)
SLT
SPD
SPD LIM
SPLR
SRS
SSM
STAB
STAR
STAT
STAT INV
STBY
STD
STEER
STRG
STS
Term
South
Step Climb
Shut Down
Step Descent
Slats/Flaps
Serial Number
Serial Number
Special Aircrew and Aircraft Authorization Required
Society of Automotive Engineers
Static Air Temperature
Satellite Communication
Single Chime
Software Control Panel
System Display
System Data Acquisition Concentrator
Smoke Detection Control Unit
Smoke Detection Function, Simplified Directional Facility
FLT CTL Secondary Computer (FCSC)
Slat/Flap Control Computer
Seller-Furnished Equipment
Standard Instrument Departure
Simulation
Server Interface Unit
Sea Level Feet (-per minute)
Slat
Speed
Speed Limit
Spoiler
Speed Reference System
Sign Status Matrix
Trimmable Horizontal Stabilizer
Standard Terminal Arrival Route
Static
Static Inverter
Standby
Standard
Steering
Steering
Status
CAL A330/A340 FLEET
FCOM
←L→
Continued on the following page
GEN P 26/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
SWTG
SYNC
SYS
4
Term
Switching
Synchronize
System
Continued from the previous page
T
Abbreviation
T. TK
T.O.
T/O
TO
T/C
T/D
T.O
TA
TACAN
TACS
TACT
TAS
TAT
TAU
TAWS
TBC
TBD
TBV
TCAS
TDU
TEMP
TFTS
TGT
THR
THS
TK
TK
TKE
TLA
TLU
TMR
TOGA
TOGW
TOW
Trim Tank
Takeoff
Takeoff
Takeoff
Top of Climb
Top of Descent
Take Off
Traffic Advisory
Tactical Air Navigation
Taxi Aid Camera System
Tactical
True Air Speed
Total Air Temperature
Time to intercept
Terrain Awareness and Warning System
To Be Confirmed
To Be Determined
Transient Bleed Valve
Traffic Alert and Collision Avoidance System
Temporary Documentary Unit
Temperature
Terrestrial Flight Telephon System
Target
Thrust
Trimmable Horizontal Stabilizer
Tank
Track angle
Track Angle Error
Throttle Lever Angle
Travel Limitation Unit
Timer
Takeoff - Go-Around
Takeoff Gross Weight
Takeoff Weight
CAL A330/A340 FLEET
FCOM
←L→
Term
Continued on the following page
GEN P 27/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
T-P
TPIS
TR
T-R
TRANS
TRK
TROPO
TRV
TSM
TTG
TVMC
TWLU
TWY
Turn Point
Tire Pressure Indicating System
Transformer Rectifier Unit
Transmitter-Receiver
Transition
Track
Tropopause
Travel
Trouble Shooting Manual
Time to Go
Minimum Control Speed Temperature
Terminal Wireless LAN Unit
Taxiway
Term
Continued from the previous page
U
Abbreviation
ULB
UNLK
UP
USB
UTC
Term
Underwater Locator Beacon
Unlock
Up, Upper
Universal Serial Bus
Universal Coordinated Time
V
Abbreviation
V/S
V1
V2
VAPP
VBV
VC
VCC
VDEV
VEL
VENT
VERT
VERT REV
VFE
VFEN
VFTO
VHF
Vertical Speed
Decision Speed
Takeoff Safety Speed
Approach Speed
Variable Bypass Valve
Ventilation Controller
Video Control Center
Vertical Deviation
Velocity
Ventilation
Vertical
Vertical Revisor
Maximum Speed for each Flap configuration
VFE Next
Final Takeoff Speed
Very High Frequency
CAL A330/A340 FLEET
FCOM
←L→
Term
Continued on the following page
GEN P 28/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
Abbreviation
VHV
VIB
VIP
VLE
VLS
VLV
VM
VMAX
VMCA
VMCG
VMCL
VMCL-2
VMIN
VMO
VMU
VOR
VOR-D
VR
VREF
VS
VSA
VSI
VSV
Term
Continued from the previous page
Very High Voltage
Vibration
Vertical Intersection Point
Maximum Landing Gear Extended Speed
Lowest Selectable Speed
Valve
Maneuvering Speed
Maximum Allowable Speed
Minimum Control Speed in the Air
Minimum Control Speed on Ground
Minimum Control Speed at Landing
Minimum control speed at landing with 2 engines inop on one wing
Minimum Operating Speed
Maximum Operating Speed
Minimum Unstick Speed
VHF Omnidirectional Range
VOR-DME
Rotation Speed
Landing Reference Speed
Reference Stalling Speed
Visual Separation on Approach
Vertical Speed Indicator
Variable Stator Vane
W
Abbreviation
WARN
WBC
WBM
WBS
WHC
WNDW
WPT
WS
WSHLD
WT
WTB
WXR
Term
Warning
Weight and Balance Computer
Weight and Balance Manual
Weight and Balance System
Window Heat Computer
Window
Waypoint
Wireless System
Windshield
Weight
Wing Tip Brake
Weather Radar
CAL A330/A340 FLEET
FCOM
←L→
GEN P 29/30
30 JUN 15
GENERAL INFORMATION
A330/A340
FLIGHT CREW
OPERATING MANUAL
X
Abbreviation
XCVR
XFR
XMTR
XPDR
XTK
Term
Transceiver
Transfer
Transmitter
Transponder
Crosstrack Error
Y
Abbreviation
Term
Z
Abbreviation
ZFCG
ZFW
ZFWCG
Zero Fuel Center of Gravity
Zero Fuel Weight
Zero Fuel Weight Center of Gravity
CAL A330/A340 FLEET
FCOM
←L
Term
GEN P 30/30
30 JUN 15