CAUTION : DO NOT OPEN LGCIU CIRCUIT BREAKERS 1GA, 2GA, AND 52GA. IF
_______ YOU DO THIS, AIRCRAFT BRAKING THROUGH BRAKE PEDALS DOES NOT OPERATE.
(a) On the landing gear control and indicating panel 402VU:
- Make sure that the A/SKID & N/WSTRG selector switch 5GG is ON.
(b) Push and hold the brake pedals at the full limit position.
(c) On the RUD TRIM/PARKING BRK panel 110VU:
- Set the PARKING BRAKE control switch to OFF.
(3) Set the opposite engine that you must hot test to 60 percent N1.
(4) When the parameters become stable, move suddenly the throttle control levers from 30 percent N1 to the FLEX/MCT detent.
(5) Start the chronometer at throttle control lever movement.
(6) Stop the chronometer when N1 reaches the FLEX T/O target minus 5 percent that you recorded in step 3.B.(5).
F 『 EEFF : ALL E Page 59171-00-00
E E Aug 01/05 ERE
ECES E (7) Record the accel time in seconds. The guideline for this time equals
F 『
E C F M E
E E
E 56-5B E
E E
7.5 seconds.
NOTE : If the time is higher than the guideline, make sure that:
____ - on the AIR COND panel 30VU the OFF legend of the ENG 1(2) BLEED is on - on the ELEC panel 35VU the OFF legend of the GEN 1(2) is on.
NOTE : If you have these conditions, do the troubleshoot
____
(8) Move back the throttle control levers to the idle detent for the two engines.
(9) Put the aircraft in the "parking-brake applied" configuration:
(a) On the RUD TRIM PARKING BRK panel 110VU:
- Set the parking brake control switch to ON.
(b) Release the brake pedals.
(10) Let the engines become stable for 3 minutes before shutdown.
(11) Stop the engines (Ref. TASK 71-00-00-710-028).
5. Close-up
________ Subtask 71-00-00-869-110
A. Close-up
(1) On the AIR COND panel 30VU:
(a) Release the ENG 1(2) BLEED pushbutton switch (the OFF legend goes off).
(2) On the ELEC panel 35VU:
(a) Release the GEN 1(2) pushbutton switch (the OFF legend goes off). Subtask 71-00-00-862-065
B. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002).
F 『 EEFF : ALL E Page 59271-00-00
E E Aug 01/05 ERE
ECES E
F 『
E C F M E
E E
E 56-5B E
E E
TASK 71-00-00-710-028
Engine Shutdown
1. Reason for the Job
__________________
Self Explanatory
2. Job Set-up Information
______________________
Not Applicable
3. Job Set-up
__________
Subtask 71-00-00-869-189
A. Not applicable
4. Procedure
_________
Subtask 71-00-00-710-136
A. Stop the engine CAUTION : MAKE SURE THAT THE ENG/MASTER 1(2) CONTROL SWITCH IS FULLY
_______
ENGAGED IN THE OFF DETENT AFTER SHUTDOWN.
(1) Before you stop the engine, operate it at or near idle for 3 minutes before shutdown to thermally stabilize the engine hot section.
NOTE : You can use taxi time at or near idle as part of the 3 minutes
____
cool down time.
(2) Put the throttle control lever in the idle position.
(3) Set the ENG/MASTER 1(2) control switch to OFF.
(4) Monitor the EGT, N2 and fuel flow during shutdown to confirm fuel shutoff.
CAUTION : BE PREPARED TO DRY MOTOR THE ENGINE WITH THE STARTER IF
_______ THERE IS A POST-SHUTDOWN FIRE INDICATION. ENGINE DAMAGE CAN BE CAUSED.
(a) Make sure that the EGT and N2 rpm decrease when the fuel is shut off. If a steady decrease in the EGT does not occur after shutdown, do a dry motoring until the fire is extinguished.
F 『 EEFF : ALL E Page 59371-00-00
E E Aug 01/05 ERE ECES E
F 『
E C F M E
E E
E 56-5B E
E E
NOTE : After engine shutdown is completed, and all of the
____ rotation has stopped, the EGT will normally slowly increase. This is caused by normal temperature soak-back.
(5) On the HYD/FUEL panel 40VU:
(a) Release all the FUEL/PUMPS pushbutton switches (the OFF legends of these pushbutton switches come on).
(6) On the overhead control and indicating panel 25VU:
(a) Set the EXT LT/BEACON switch to OFF.
Subtask 71-00-00-865-092
B. Remove the safety clip(s) and the tag(s) and close this(these) circuit breaker(s): 1DA1, 1DA2, 2DA1, 2DA2, 2DA3, 3DA1, 3DA2, 3DA3, 4DA1, 4DA2, 4DA3, 5DA1, 5DA2, 5DA3, 1DB1, 1DB2, 4DG1, 4DG2.
中国航空网 www.aero.cn
航空翻译 www.aviation.cn
本文链接地址：A320飞机维护手册 AMM 动力装置 POWER PLANT 1(62)
