- The ON legend of this
 pushbutton switch comes on.

 2. On the upper ECAM display unit:
 - Make sure that there is no
 indication related to the N2
 speed sensor.

 F 『 EEFF : ALL E Page 52078-31-00
 E E May 01/05 ERE
ECES  E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
3. On the overhead maintenance panel  - The ON legend of this pushbutton 50VU: switch goes off.
 - Push the ENG/FADEC GND PWR/1(2)
 pushbutton switch.

 Subtask 78-31-00-860-057
 D. Do the EIS Stop Procedure: (Ref. TASK 31-60-00-860-002)
 Subtask 78-31-00-410-050
 E. Close Access
 (1) Make sure that the work area is clean and clear of tool(s) and other items.

 (2) Close the fan cowl doors (Ref. TASK 71-13-00-410-040):
 FOR 1000EM1
 437AL, 438AR
 FOR 1000EM2
 447AL, 448AR

 Subtask 78-31-00-862-051
 F. De-energize the aircraft electrical circuits (Ref. TASK 24-41-00-862-002)
 Subtask 78-31-00-865-053
 G. 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, 4DG1, 4DG2, 1DG1, 1DG2
 F 『 EEFF : ALL E Page 52178-31-00
 E E May 01/05 E E ECES E

 F  『
 E  C F M  E
 E  E

 E 56-5B E E E TASK 78-31-00-710-043- 01

 Operational Test of the Thrust Reverser without CFDS - Engine Running
 1. Reason for the Job

__________________
 Self Explanatory

 2. Job Set-up Information

______________________
 A. Referenced Information
 -------------------------------------------------------------------------------REFERENCE DESIGNATION -------------------------------------------------------------------------------
71-00-00-710-003 Engine Automatic Start 71-00-00-710-028 Engine Shutdown
 3. Job Set-up
__________ Subtask 78-31-00-710-053
 A. Start the engine 1(2) and let it become stable at ground idle (Ref. TASK 71-00-00-710-003).
 4. Procedure
_________ Subtask 78-31-00-710-054
 A. Do this test: CAUTION : CAREFULLY MONITOR THE ECAM DISPLAY UNIT FOR A POSSIBLE STALL
_______ WARNING DURING THE DEPLOYMENT OF THE THRUST REVERSERS. STOP THE ENGINE IF THERE IS A STALL WARNING OR IF THE EGT INCREASES TO 725 DEG.C.
 F 『 EEFF : ALL E Page 52278-31-00
 E E May 01/05 E E ECES E

 F  『
 E  C F M  E
 E  E
 E  56-5B  E
 E  E

 -------------------------------------------------------------------------------ACTION RESULT -------------------------------------------------------------------------------
1. Set the thrust reverser control lever of the engine 1(2) to the reverse idle position (detent).

2. Set the throttle control lever of the engine 1(2) to the idle stop position (the zero mark on the graduated scale).

5. Close-up
________
 Subtask 78-31-00-710-055On the upper ECAM display unit:
- The amber REV indication comes intoview in the N1 indication of the engine 1(2) during the deployment.

 - The REV indication changes to green when the blocker doors are deployed and locked.

On the upper ECAM display unit:

- The REV indication in the N1indication of the engine 1(2) changesto amber during the stowage of the blocker doors.

 - The REV indication goes out of view when the blocker doors are stowed and locked.

 A. Shut down the engine (Ref. TASK 71-00-00-710-028).

 F 『 EEFF : ALL E Page 52378-31-00
 E E May 01/05 E E ECES E

 F 『
 E C F M E
 E E
 E 56-5B E
 E E

 THRUST REVERSER CONTROL AND INDICATING - INSPECTION/CHECK
_________________________________________________________
 TASK 78-31-00-210-041
 Visual Inspection of the Primary Latch Mechanism
 1. Reason for the Job
__________________
 Refer to the MPD TASK: 783100-C7
 2. Job Set-up Information
______________________
 A. Fixtures, Tools, Test and Support Equipment
 -------------------------------------------------------------------------------
　
中國航空網(wǎng) www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：A320飛機維護手冊 AMM EXHAUST 1(38)