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AUTO FLIGHT - FLIGHT ENVELOPPE
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A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
PRELIMINARY PAGES - TABLE OF CONTENTS
A330/A340 FLEET DSC-22_40-PLP-TOC P 1/2
FCOM 19 AUG 10
DSC-22_40-PLP PRELIMINARY PAGES
TABLE OF CONTENTS......................................................................................................................................1/2
DSC-22_40-10 GENERAL
GENERAL............................................................................................................................................................1/2
DSC-22_40-20 ACQUISITION/MONITORING
ACQUISITION/MONITORING.............................................................................................................................1/2
DSC-22_40-30 CHARACTERISTIC SPEEDS COMPUTATION
CHARACTERISTIC SPEEDS COMPUTATION....................................................................................................1/2
DSC-22_40-40 WEIGHT AND CENTER OF GRAVITY COMPUTATION
WEIGHT AND CENTER OF GRAVITY COMPUTATION.....................................................................................1/2
DSC-22_40-50 AFT CG MONITORING
AFT CG MONITORING...................................................................................................................................... 1/2
DSC-22_40-60 WINDSHEAR DETECTION
WINDSHEAR DETECTION.................................................................................................................................1/2
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
PRELIMINARY PAGES - TABLE OF CONTENTS
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A330/A340 FLEET DSC-22_40-PLP-TOC P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
GENERAL
A330/A340 FLEET DSC-22_40-10 P 1/2
FCOM 19 AUG 10
GENERAL
Applicable to: ALL
The Flight Envelope (FE) part of the FMGS performs the following functions :
Acquisition and monitoring of parameters ‐ used by FE and FG parts.
‐ Characteristic speeds computation.
‐ Back-up weight and CG computation.
‐ Aft CG monitoring.
‐ Windshear detection.
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
GENERAL
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A330/A340 FLEET DSC-22_40-10 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
ACQUISITION/MONITORING
A330/A340 FLEET DSC-22_40-20 P 1/2
FCOM 19 AUG 10
ACQUISITION/MONITORING
Applicable to: ALL
Acquisition and monitoring of buses common to FM, FG or FE are performed by the FE. Only ARINC
buses specific to the FM part are acquired by the FM itself.
Dialogue between FM, FG and FE is achieved through common memories.
The FE function generates the following information :
‐ Flight/ground conditions (LGCIU/SFCC).
‐ Flap/slat configuration (SFCC).
‐ Engine configuration (FADEC).
‐ ADR/IR parameters after filtering and consolidation (used by the control laws).
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
ACQUISITION/MONITORING
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A330/A340 FLEET DSC-22_40-20 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
CHARACTERISTIC SPEEDS COMPUTATION
A330/A340 FLEET DSC-22_40-30 P 1/2
FCOM 19 AUG 10
CHARACTERISTIC SPEEDS COMPUTATION
Applicable to: ALL
FE part computes the characteristic speeds and sends them to :
The FG which uses ‐ them as limits for guidance modes.
‐ The EFIS for display on the PFD speed scale.
The following speeds are computed :
Minimum speeds
‐ VLS
(Refer to PRO-SUP-10 Characteristic Speeds)
‐ Manoeuvring speeds F, S, O (Green Dot)
(Refer to PRO-SUP-10 Characteristic Speeds)
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
CHARACTERISTIC SPEEDS COMPUTATION
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A330/A340 FLEET DSC-22_40-30 P 2/2
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
AIRCRAFT SYSTEMS
AUTO FLIGHT - FLIGHT ENVELOPPE
WEIGHT AND CENTER OF GRAVITY COMPUTATION
A330/A340 FLEET DSC-22_40-40 P 1/2
FCOM 19 AUG 10
WEIGHT AND CENTER OF GRAVITY COMPUTATION
Applicable to: ALL
The FMGC uses the weight and center of gravity from the FCMC (Fuel Computer) when available.
　
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