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LGCIU 1 C/B (C09).............................................................................................................PULL
EMER ELEC PWR........................................................................................................ MAN ON
CAUTION Minimum speed is 180 kt instead of 140 kt given by ECAM.
During deceleration (before reaching 200 kt) :
LGCIU 1 C/B (C09)............................................................................................................PUSH
Emergency generator will be deactivated.
Minimum speed is 140 kt.
ABN AND EMER PROCEDURES (CONT'D)
In case of go-around, when above 200 kt
LGCIU 1 C/B (C09).............................................................................................................PULL
EMER ELEC PWR........................................................................................................ MAN ON
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PROCEDURES
A318/A319/A320/A321 FLEET PRO-SPO-25-30 P 3/4
FCOM 19 AUG 10
FAILURE OF BOTH ENGINES
When both engines are failed, to ease the handling of all the different ECAM procedures resulting
from this all engine flame out situation, it is recommended to use the ENG DUAL FAILURE QRH
paper procedure, and if time permits, to clear the ECAM.
Follow all the steps of the QRH paper procedure, except those that are modified by the procedure
below :
If APU is available : perform an assisted relight when below FL 200.
If APU is not available
Do not attempt to start ‐ the APU (APU start is inhibited in this configuration)
‐ Windmilling relight can be performed, as long as the speed is above 300 kt (corresponding
N2 above 12 %). In this case, increase aircraft speed and disregard VMO warning.
‐ Flight controls are in direct laws. Use manual pitch trim as necessary (not indicated on PFD
if APU GEN not available).
‐ Do not use LGCIU 1 C/B.
‐ In approach, set CONF 1 at or above 200 kt. Do not select flaps/slats below 200 kt.
AVIONICS SMOKE
If smoke persists more than 5 min, the LGCIU 1 C/B (C09 on 49 VU) must be pulled before RAT
extension. Minimum speed is 180 kt (instead of 140 kt given by ECAM).
During approach :
GEN 2..........................................................................................................................................ON
EMER ELEC GEN 1 LINE............................................................................................................ ON
LGCIU 1 C/B (C09 on 49 VU)..................................................................................................PUSH
ABN AND EMER PROCEDURES
Applicable to:
,
,
MSN
FLIGHT CONTROLS
Failure cases, which would normally lead to ALTN law, will degrade F/CTL laws down to DIRECT
law, if the landing gear is extended.
FAILURE OF BOTH ENGINES
When both engines are failed, to ease the handling of all the different ECAM procedures resulting
from this all engine flame out situation, it is recommended to use the ENG DUAL FAILURE QRH
paper procedure, and if time permits, to clear the ECAM.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - PROCEDURES
A318/A319/A320/A321 FLEET PRO-SPO-25-30 P 4/4
FCOM 19 AUG 10
Follow all the steps of the QRH paper procedure, except those that are modified by the procedure
below :
If APU is not available
‐ Attempt an APU start
‐ . If APU start is unsuccessful, a windmilling relight can be performed, as long as the speed
is above 300 kt (corresponding N2 above 12 %). In this case, increase the aircraft speed
and disregard VMO warning.
If APU is available : perform an assisted relight, when below FL 200.
‐ Flight controls are in direct laws. Use manual pitch trim as necessary (not indicated on PFD
if APU GEN not available).
‐ In approach, set CONF 1 at or above 200 kt. Do not select flaps/slats below 200 kt.
ABN AND EMER PROCEDURES
Applicable to: MSN
4566,,,
FLIGHT CONTROLS
Failure cases, which would normally lead to ALTN law, will degrade F/CTL laws down to DIRECT
law, if the landing gear is extended.
FAILURE OF BOTH ENGINES
When both engines are failed, to ease the handling of all the different ECAM procedures resulting
from this all engine flame out situation, it is recommended to use the ENG DUAL FAILURE QRH
paper procedure, and if time permits, to clear the ECAM.
Follow all the steps of the QRH paper procedure, except those that are modified by the procedure
below :
If APU is not available
‐ Attempt an APU start
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A320机组操作手册FLIGHT CREW OPERATING MANUAL 14(18)
