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L2With FAC 1 + 2 inoperative, the rudder travel limit system, rudder trim control, yaw damper and
PFD characteristic speeds are lost.
L12
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
F/CTL normal laws are lost. All protections, except maneuver protections, are lost.
L1MAX SPEED .....................................................................................................................320 KT
L2 Speed is limited, due to the loss of high-speed protections.
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 34/62
FCOM 19 AUG 10
AUTO FLT FAC 1 + 2 FAULT (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
RUD WITH CARE ABV 160 KT
APPR PROC
FOR LDG...................................................................USE FLAP 3
GPWS LDG FLAP 3................................................................. ON
Displayed, when flaps in CONF 3.
APPR SPD............................................................. VREF + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or Refer to 99 Duref Cible FCOM.
ALTN LAW : PROT LOST
WHEN L/G DN : DIRECT LAW
See (1)
INOP SYS
REAC W/S DET
F/CTL PROT
FAC 1 + 2
AP 1 + 2
A/THR
CAT 2
(1) AL2t landing gear extension, control reverts to direct law in pitch, as well as in roll (Refer to
00000610 **Not found** DIRECT LAW procedure).
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 35/62
FCOM 19 AUG 10
AUTO FLT FAC 1 + 2 FAULT
Applicable to: MSN
RUD WITH CARE ABV 160 KT
L2 Depending on when the failure occurs, the rudder travel limiter system may not be in the correct
position for the flight speed. Therefore, to prevent damage to the aircraft structure, use the rudder
with care, when the speed is above 160 kt.
At slats’ extension, full rudder travel authority is recovered.
L1 FAC 1 ......................................................................................................................... OFF THEN ON
FAC 2.......................................................................................................................... OFF THEN ON
IF UNSUCCESSFUL:
FAC 1 + 2..............................................................................................................................OFF
L2With FAC 1 + 2 inoperative, the rudder travel limit system, rudder trim control, yaw damper and
PFD characteristic speeds are lost.
L12
ASSOCIATED PROCEDURES
F/CTL ALTN LAW
(PROT LOST)
F/CTL normal laws are lost. All protections, except maneuver protections, are lost.
L1MAX SPEED .....................................................................................................................320 KT
L2 Speed is limited, due to the loss of high-speed protections.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
AUTO FLIGHT
A318/A319/A320/A321 FLEET PRO-ABN-22 P 36/62
FCOM 19 AUG 10
AUTO FLT FCU 1 + 2 FAULT
Applicable to:
PFD BARO REF: STD ONLY
L2With both FCU channels failed, the barometer reference automatically goes to 1 013 hPa.
Use standby altimeter, and change this to the actual barometer setting.
Do not insert the MDA (MDH) value on the MCDU PERF APPR Page (because the PFD altitude is
referenced to STD, and not to the correct barometric value).
The PNF must then perform the standard callouts (“HUNDRED ABOVE” and “MINIMUM”), using
the STBY altimeter.
In addition:
All ‐ FCU controls are inoperative.
‐ A/THR, AP 1 + 2, and FD 1 + 2 are not available.
(Except in LAND or GO AROUND mode where only A/THR is lost).
‐ On PFD:
• Altitude alert is inoperative.
• ILS deviation scales are displayed.
• Flight path vector is displayed.
• Mach indication is inoperative.
• FMA is lost except in LAND or GA mode.
‐ On ND:
• ROSE NAV mode with map (80 nm range) is displayed.
• VOR/ADF needles:
Needle 1 is related to VOR1 only.
Needle 2 is related to ADF2 only (ADF1 if ADF2 not installed).
(VOR selection on DDRMI is not affected)
(ADF selection on DDRMI (if available) is not affected).
• The weather radar image may be lost. If the image remains displayed it must be disregarded.
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 8(102)
