S 024-065-N00

 (13)
 Lower the thrust reverser on the pallet.

 S 434-071-N00

 (14)
 Attach the center and aft hinge bearings in the strut hinge fitting with the plastic or wire ties to make sure the bearings do not fall out.

 S 034-023-N00

 (15)
 If you must remove the link (14), remove the bolt (12), washer (13) and nut (9).

 S 024-080-N00

 (16)
 If necessary, repeat the above procedure for the remaining thrust reverser half.

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
TASK 78-31-01-404-024-N00
 3. Install 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 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).

 (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.
Consumable Materials

 (1)  
D00015 Grease, Aircraft Ball and Roller Bearing, BMS 3-24

 D.
Parts

 ~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 3 | Thrust Reverser - LH | 78-31-01 | 01 | 1 | | | 3 | Thrust Reverser - RH | | | 5 | | | 4 | Fairing - LH | | 05 | 240 | | | 4 | Fairing - RH | | | 245 | | | 5 | Bolt | | | 280 | | | 7 | Bolt Assembly | | 01 | 50 | | | 8 | Washer | | | 65 | | | 9 | Nut | | | 70 | | | 10 | Bolt Assembly | | | 55 | | | 11 | Bolt Assembly | | | 45 | | | 12 | Bolt Assembly | | | 60 | | | 14 | Link | | | 75 | 2.....….........…...................................…..........…......…........1
 E. References
 (1)  
AMM 24-22-00/201, Manual Control

 (2)  
AMM 27-62-00/201, Speed Brake Control System

 (3)  
AMM 27-81-00/201, Leading Edge Flap System

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
(4)  
AMM 71-11-04/401, Fan Cowl Panels

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

 (6)  
AMM 78-31-00/201, Thrust Reverser System

 (7)  
AMM 78-31-00/501, Thrust Reverser System

 (8)  
AMM 78-31-01/501, Thrust Reverser

 (9)  
AMM 78-31-02/401, Fan Duct Vee-Groove Latch Bands

 (10)
 AMM 78-31-06/401, Thrust Reverser Hydraulic Cowl Opening Actuators

 F.
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
　
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