曝光臺 注意防騙 網(wǎng)曝天貓店富美金盛家居專營店坑蒙拐騙欺詐消費(fèi)者

FCOM 19 AUG 10
F/CTL STABILIZER JAM (Cont'd)
L12
STATUS
MAX SPEED............................................................ 320 KT
APPR PROC:
FOR LDG...................................................................USE FLAP 3
Do not select configuration FULL, so as not to degrade the
handling qualities.
GPWS LDG FLAP 3................................................................. ON
Will be displayed when flaps in CONF 3
�� IF MAN TRIM NOT AVAIL:
�� WHEN CONF 3 AND VAPP:
L/G................................................................................DN
Landing gear extension is delayed, in order to delay the
switching to direct law.
APPR SPD:............................................................ VREF + 10 KT
LDG DIST PROC................................................................APPLY
Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible
FCOM.
ALTN LAW: PROT LOST
WHEN L/G DN: DIRECT LAW
At landing gear extension, control reverts to direct law in pitch, as
well as in roll. Refer to PRO-ABN-27-J F/CTL DIRECT LAW.
INOP SYS
F/CTL PROT
STABILIZER
ELAC PITCH
AP 1 + 2
CAT 2
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 137/146
FCOM 19 AUG 10
STABILIZER JAM
Applicable to: ALL
L2 The ELACs may not detect a stabilizer jam when the pitch trim wheel is jammed.
The flight control normal law remains active in this case and there is no ECAM warning.
Apply the following procedure.
L1 AP................................................................................................................................................ OFF
MAN PITCH TRIM................................................................................................................... CHECK
L2 The pitch trim wheel may not be fully jammed, the force needed may be higher than pre-takeoff
manual setting.
L1�� IF MAN TRIM AVAIL:
TRIM FOR NEUTRAL ELEV
L2 If manual pitch trim is available, trim to maintain the elevator at the zero position (indications on
F/CTL SD page).
L1APPR PROC
�� IF MAN TRIM NOT AVAIL:
FOR LDG.............................................................................................................. USE FLAP 3
L2 Do not select configuration full so as not to degrade the handling qualities.
L1GPWS LDG FLAP 3.............................................................................................................ON
CAT 2 INOP
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
FLIGHT CONTROLS
A318/A319/A320/A321 FLEET PRO-ABN-27 P 138/146
FCOM 19 AUG 10
F/CTL RUDDER JAM
Applicable to: ALL
L2 Rudder jamming may be detected by undue (and adverse) pedal movement during rolling
maneuvers.
This is because the yaw damper orders can no longer be sent to the rudder, but are fed back to the
pedals.
Use F/CTL SD page for a visual check of the rudder position.
L1FOR APPROACH
AVOID LANDING WITH CROSSWIND from the side where the rudder is deflected.
MAX CROSSWIND for LDG 15 kt
AUTO BRK................................................................................................................ DO NOT USE
L2 Do not use the autobrake, so as not to delay the application of differential braking at landing roll.
L1 FOR LDG...................................................................................................... USE NORMAL CONF
SPEED AND TRAJECTORY............................................................................... STABILIZE ASAP
LDG DIST PROC..................................................................................................................APPLY
L2 Refer to 99 Duref Cible QRH, or to the Refer to 99 Duref Cible FCOM.
L1ON GROUND
DIFFERENTIAL BRAKING.............................................................................................USE ASAP
L2 Do not use asymmetric reverse thrust.
Use Nosewheel Steering below 70 kt.
NON-RETRACTION OF SPEEDBRAKES
Applicable to: ALL
L2Non-retraction of speedbrakes may be detected, if there is no flight parameter change after the
selection of speedbrake retraction.
Use the F/CTL SD page for a visual check of the speedbrakes. Speedbrakes will automatically
retract upon selection of CONF FULL for the A319/A320 or upon selection of CONF 3 or FULL for
A321.
Note: Fuel consumption is increased by about 1.6 % , when flying with the speedbrakes
extended.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
　
中國航空網(wǎng) m.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320機(jī)組操作手冊FLIGHT CREW OPERATING MANUAL 9(111)