747-400 AMM 飞机维护手册 EXHAUST 1(66)

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(2)  S 415-061-N00Install the access panel for the rod end of the applicable locking actuator.
 (3)  S 415-062-N00Close the fan cowl panels (AMM 71-11-04/201).
 (4)  S 955-063-N00Remove the DO-NOT-OPERATE tags from the reverse thrust levers.
 (5)  S 445-064-N00Do the activation procedure for the thrust reverser (AMM 78-31-00/201).
 (6)  S 715-065-N00Do an operational test of the thrust reverser system (AMM 78-31-00/501).

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 78-31-00
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
THRUST REVERSER - REMOVAL/INSTALLATION
______________________________________
 1.  General
_______
 A.  This procedure has two tasks:
 (1)  
Remove the L (R) thrust reverser half.

 (2)  
Install the L (R) thrust reverser half.

 B.  
You must not open, extend or lift the thrust reverser if more than six cascade vane segments are removed. You must install a minimum of three cascade vane segments in each thrust reverser half. The empty space between these three cascade vane segments must be equivalent. There must not be more than two adjacent empty spaces between the three cascade vane segments which are installed.

 C.  
You can change the left left and right thrust reverser halves between the left and right engines if the cascade vane segments are installed in the specified locations (AMM 78-31-16/401).

 D.  
When you change the engine, thrust reverser, or strut, it is necessary to adjust the thrust reverser shims (AMM 78-31-01/501).

 TASK 78-31-01-004-001-N00
 2.  Remove the Thrust Reverser
__________________________
 A.  General
 CAUTION: DO NOT LIFT OR MOVE THE THRUST REVERSER HALF WITH MORE THAN SIX
_______ CASCADE VANE SEGMENTS REMOVED. IF YOU DO NOT HAVE A MINIMUM OF THREE CASCADE VANE SEGMENTS, YOU CAN CAUSE DAMAGE TO THE THRUST REVERSER STRUCTURE.
 (1)  
You must not open, extend or lift the thrust reverser if more than six cascade vane segments are removed. You must install a minimum of three cascade vane segments in each thrust reverser half. The empty space between these three cascade vane segments must be equivalent. There must not be more than two adjacent empty spaces between the three cascade vane segments which are installed.

 (2)  
You can change the left and right thrust reverser halves between the left and right engines if the cascade vane segments are installed in the specified locations (AMM 78-31-16/401).

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(3)  
When you change the engine, thrust reverser, or strut, it is necessary to adjust the thrust reverser shims (AMM 78-31-01/501).

 B.
Special Tools and Equipment

 (1)  
A71002-48 - Sling, Thrust Reverser

 (2)  
A78002-4 - Protector, Thread

 C.
References

 (1)  
AMM 27-62-00/201, Speed Brake Control System

 (2)  
AMM 27-81-00/201, Leading Edge Flap System

 (3)  
AMM 54-62-00/201, Strut Fairings

 (4)  
AMM 71-11-04/401, Fan Cowl Panels

 (5)  
AMM 71-11-06/401, Core Cowl Panels

 (6)  
AMM 78-31-03/401, Fan Duct Vee Band Anchor

 (7)  
AMM 78-31-00/201, Thrust Reverser System

 (8)  
AMM 78-31-06/401, Thrust Reverser Cowl Opening Actuators

 (9)  
AIPC 78-31-01, Fig. 1

 (10)
 AIPC 78-31-01, Fig. 5

 D.
Access

 (1)  
Location Zone
 415 and 416 Engine 1 - Thrust Reverser Halves
 425 and 426 Engine 2 - Thrust Reverser Halves
 435 and 436 Engine 3 - Thrust Reverser Halves
 445 and 446 Engine 4 - Thrust Reverser Halves

 (2)  
　
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