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
Aircraft stopped
Consider positioning the aircraft to keep any possible fire away from the fuselage.
REVERSE................................................................ STOWED ATC.......................................................................INFORM
PARKING BRAKE........................................................APPLY EMER EVAC checklist......................................... LOCATE
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 6/22
FCOM 19 AUG 10
REJECTED TAKEOFF (Cont'd)
CAPT F/O
Set parking brake ON after aircraft stops.
PA call........................."ATTENTION CREW! AT STATIONS"
CALL.........................................................."ECAM ACTIONS" ECAM ACTIONS..................................................INITIATE
The aircraft should remain stationary while the crew evaluates the situation.
Evacuation phase
If required, Refer to QRH/ABN-80 EMERGENCY
EVACUATION Checklist for evacuation. Inform ATC of intention and required assistance.
REVERSERS : Full reverse may be used until coming to a complete stop. But, if there is
enough runway available at the end of the deceleration, it is preferable
to reduce reverse thrust when passing 70 kt. The use of full reverse until
complete stop must be reported in the logbook for maintenance action.
Note: 1. If the brake response does not seem appropriate for the runway condition, FULL
manual braking should be applied and maintained. If IN DOUBT, TAKE OVER
MANUALLY. Do not attempt to clear the runway, until it is absolutely clear that an
evacuation is not necessary and that it is safe to do so.
2. If the autobrake is unserviceable, the Captain simultaneously reduces thrust and
applies maximum pressure on both pedals.
The aircraft will stop in the minimum distance, only if the brake pedals are maintained
fully pressed until the aircraft comes to a stop.
3. If normal braking is inoperative, immediately switch the A/SKID & N/W STRG sw
OFF and modulate brake pressure, as required, at or below 1 000 PSI.
If the brake pedals were fully pressed when switching the A/SKID & N/W STRG sw
OFF, full pressure would be applied to the brakes.
4. After a rejected takeoff, if the aircraft comes to a complete stop using autobrake
MAX, release brakes prior to taxi by disarming spoilers.
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 7/22
FCOM 19 AUG 10
ENG FAILURE AFTER V1 - CONTINUED TAKEOFF
Applicable to:
,
,
MSN,,,,
If an engine fails after the aircraft passes V1, the takeoff must be continued.
Use rudder conventionally to stay on the runway centerline.
At VR, rotate the aircraft smoothly using a continuous pitch rate to a pitch attitude of 12.5 °. After
lift-off, follow the Speed Reference System (SRS).
When airborne with a positive rate of climb, select the landing gear up.
Use rudder to prevent yaw. Shortly after lift-off, β target will appear. Adjust rudder position to zero
the β target. Control heading conventionally with bank, keeping the β target at zero with rudder.
Consider the use of TOGA thrust.
Consider the use of autopilot.
At 400 ft minimum, apply the ECAM procedure.
At acceleration height, level off and allow the speed to increase.
• At F speed select CONF 1.
• At S speed select CONF 0.
When the flaps lever is at zero, β target reverts to sideslip indication: Center the sideslip
indication conventionally.
At green dot speed (engine-out operating speed in clean configuration):
Resume the climb using maximum continuous thrust and maintain green dot speed.
(If already in the FLX/MCT gate, move to CL and back to MCT).
MAXIMUM TAKEOFF THRUST IS ONLY ALLOWED FOR 10 min.
ENGINE FAILURE DURING INITIAL CLIMB-OUT
Proceed as above. However, if the failure occurs above V2 maintain the SRS commanded
attitude (or the speed reached after recovery). In any case, the minimum speed must be equal to
V2.
ENGINE OPERATION AT MAX T.O. THRUST IS LIMITED TO 10 min
To be continued on next page
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
OPERATING TECHNIQUES
A318/A319/A320/A321 FLEET PRO-ABN-10 P 8/22
FCOM 19 AUG 10
ENG FAILURE AFTER V1 - CONTINUED TAKEOFF (Cont'd)
A318/A319/A320/A321 FLIGHT CREW
OPERATING MANUAL
PROCEDURES
ABNORMAL AND EMERGENCY PROCEDURES
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 8(64)
