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Applicable to: ALL
This table shows how the FMGC responds to failures in other parts of the system.
FAILURE CASE AP/FD A/THR LANDING
CAPACITIES
FIRST IRS FAILURE NO EFFECT NO EFFECT CAT 3 SINGLE
SECOND IRS FAILURE TOTAL LOSS TOTAL LOSS RAW DATA
FIRST ADC FAILURE (1)NO EFFECT NO EFFECT CAT 3 SINGLE
SECOND ADC FAILURE TOTAL LOSS TOTAL LOSS RAW DATA ONLY
FIRST LGCIU FAILURE NO EFFECT NO EFFECT NO EFFECT
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
AUTO FLIGHT - FMGES RESET AND OTHER ABNORMAL PROCEDURES
A330/A340 FLEET PRO-SUP-22-10 P 10/12
FCOM 19 AUG 10
Continued from previous page
FAILURE CASE AP/FD A/THR LANDING
CAPACITIES
SECOND LGCIU FAILURE NO EFFECT NO EFFECT NO EFFECT
LOSS OF ONE FMS
COMPUTATION
LOSS OF ONE AP/FD/ATS EXCEPT
IN APPR mode BELOW 700 ft AND
GO AROUND MODES
NO EFFECT
BELOW 700 ft
FIRST SFCC FAILURE NO EFFECT NO EFFECT NO EFFECT
SECOND SFCC FAILURE NO EFFECT NO EFFECT NO EFFECT
FIRST RADIO ALTIMETER
FAILURE NO EFFECT NO EFFECT CAT 2
SECOND RADIO ALTIMETER
FAILURE
TOTAL LOSS OF
ILS APPR MODE NO EFFECT ILS APPR(3)
MODE INOP
TOTAL LOSS OF THE FCU
TOTAL LOSS
EXCEPT IN LAND
AND GO
AROUND
TOTAL LOSS
RAW DATA
EXCEPT IN LAND
MODE
(CAT 2 MAX)
FIRST ILS RECEIVER FAILURE NO EFFECT NO EFFECT CAT 1
SECOND ILS RECEIVER FAILURE
TOTAL LOSS IN
APPR
mode (ILS)
NO EFFECT (ILS) APPR
MODE INOP
FIRST/SECOND PRIM FAILURE(2)NO EFFECT NO EFFECT CAT 3 single
TOTAL PRIM FAILURE NO EFFECT NO EFFECT CAT 1
FCMC FAILURE NO EFFECT NO EFFECT NO EFFECT
FIRST YAW DAMPER OR
RUDDER TRIM FAILURE NO EFFECT NO EFFECT CAT 3 SINGLE
SECOND YAW DAMPER OR
RUDDER TRIM FAILURE
TOTAL LOSS OF
AP EXCEPT IN
LAND MODE
BELOW 200 ft
AND BEFORE
ROLL OUT
NO EFFECT
CAT 1
NO EFFECT
BELOW 200 ft
if previously
CAT 2/3
FIRST BSCU FAILURE NO EFFECT NO EFFECT NO EFFECT
SECOND BSCU FAILURE NO EFFECT NO EFFECT CAT 3 SINGLE
FIRST FWC FAILURE NO EFFECT NO EFFECT CAT 3 SINGLE
SECOND FWC FAILURE NO EFFECT NO EFFECT CAT 1
LOSS OF PFD DATA ON
ONE SIDE NO EFFECT NO EFFECT CAT 1
TOTAL LOSS OF ONE FMGC LOSS OF ONE
AP/FD
LOSS OF ONE
ATS CAT 3 SINGLE
To be continued on next page
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
AUTO FLIGHT - FMGES RESET AND OTHER ABNORMAL PROCEDURES
A330/A340 FLEET PRO-SUP-22-10 P 11/12
FCOM 19 AUG 10
Continued from previous page
FAILURE CASE AP/FD A/THR LANDING
CAPACITIES
SINGLE HYDRAULIC FAILURE NO EFFECT NO EFFECT CAT 3 SINGLE
DOUBLE HYDRAULIC FAILURE TOTAL LOSS
OF AP NO EFFECT CAT 1
(1) The FMGC internal test may eliminate one ADR. In this case, the FMGC no longer checks this ADR until autopilot
reengagement. If CAT III DUAL is lost on the FMGC in command without failure, the pilot may recover it by changing
the autopilot in command.
(2) One SEC must also be available. The autopilot is lost if PRIM2 and SEC2 are lost, due to ailerons uplift.
(3) LOC mode can be armed through the LOC pb.
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
AUTO FLIGHT - FMGES RESET AND OTHER ABNORMAL PROCEDURES
Intentionally left blank
A330/A340 FLEET PRO-SUP-22-10 P 12/12
FCOM 19 AUG 10
A330/A340 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SUPPLEMENTARY PROCEDURES
AUTO FLIGHT - FMS SPECIFICITIES
A330/A340 FLEET PRO-SUP-22-20-10 P 1/2
FCOM 19 AUG 10
FMS1 Honeywell Specificities
DUAL FMS RESET AFTER A "CLEAR FROM" IN THE F-PLN
Applicable to:
A dual FMS reset, with loss of all pilot-entered data, may occur when the following conditions are
met:
2 steps ‐ (at least) are defined in the active F-PLN, and the first step is defined at the current “TO”
waypoint
‐ The flight crew clears the “FROM” waypoint (or “PPOS”) on the active F-PLN (by a CLR action on
1L key on the F-PLN page), to force a F-PLN sequencing.
A step defined at the “TO” waypoint can be identified by the flight crew:
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A330/A340机组操作手册 FLIGHT CREW OPERATING MANUAL FCOM 11(64)
