曝光台 注意防骗
网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者
‐ Disregard FM fuel predictions. Other predictions should also be disregarded (altitude, speed and
time), except time predictions at waypoints when in cruise.
‐ Do not use managed speed (except in approach) and CLB and DES autopilot modes.
‐ ALTITUDE ALERT is not available.
‐ The APU must run during the whole flight. APU GEN must be available.
LIMITATIONS
Applicable to:
,
,
MSN,,,,
‐ Do not fly into expected icing conditions.
‐ Ditching with the landing gear down has not been demonstrated.
‐ Disregard FM fuel predictions. Other predictions should also be disregarded (altitude, speed and
time), except time predictions at waypoints when in cruise.
‐ Do not use managed speed (except in approach) and CLB and DES autopilot modes.
‐ ALTITUDE ALERT is not available.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
SPECIAL OPERATIONS
FLIGHT WITH GEAR DOWN - LIMITATIONS
Intentionally left blank
A318/A319/A320/A321 FLEET PRO-SPO-25-20 P 2/2
FCOM 19 AUG 10
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 1/4
FCOM 19 AUG 10
PREFLIGHT
Applicable to:
• VMO/MMO with the landing gear down is 235 kt/M .60. In the avionics compartment, on 188 VU,
the VMO-MMO switch must be set to the "L/G DOWN" position.
• The check of ELAC 2 standby power supply availability, in case of BLUE hydraulic pressure loss
must be performed during cockpit preparation, if not already done by maintenance. This ensures
that, if the crew forgets to reset the LGCIU 1C/B during approach in EMER ELEC configuration,
ELAC 2 will be supplied by Battery 2, should the RAT stall during flare.
YELLOW ELEC PUMP......................................................................................................................ON
PTU..................................................................................................................................Check AUTO
BLUE PUMP OVRD.......................................................................................................................... ON
LGCIU 1 C/B (C09)....................................................................................................................... PULL
LGCIU/SYS 1/GND SPLY (Q34 if installed)..................................................................................PULL
This simulates the L/G in retracted position.
Check that the “ELAC 2” indication is green on the ECAM F/CTL page.
ELAC 2/NORM/SPLY (R20 on rear panel)................................................................................... PULL
Check that the ELAC 2 indication changes to amber.
THS ACTR/MOT 1 (Q16 on rear panel)........................................................................................PULL
This simulates the EMER ELEC configuration.
Check that the ELAC 2 indication is again green for about 30 s, and that it then changes to amber.
BLUE ELEC PUMP OVRD..............................................................................................................OFF
This simulates a RAT stall in EMER ELEC configuration.
• BLUE hydraulic system is depressurized.
• Check ELAC 2 indication changes to green.
C/Bs...........................................................................................................................................RESET
Reset LGCIU 1 C/B : C09,
Q34 (if installed)
ELAC 2 C/B : R20
THS ACTR/MOT 1 C/B : Q16
YELLOW ELEC PUMP....................................................................................................................OFF
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 2/4
FCOM 19 AUG 10
PREFLIGHT
Applicable to:
,
,
MSN,,,,
VMO/MMO with the landing gear down is 235 kt/M .60. In the avionics compartment, on 188 VU, the
VMO-MMO switch must be set to the "L/G DOWN" position.
NORMAL PROCEDURES
Applicable to:
After engine start :
APU................................................................................................................................ KEEP ON
Keep the APU running for the duration of the flight.
ABN AND EMER PROCEDURES
Applicable to:
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.
ALL GENERATOR FAILURE
The aircraft is supplied by batteries only.
To recover the emergency generator
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：
A320机组操作手册FLIGHT CREW OPERATING MANUAL 14(17)
