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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
THRUST REVERSER - ADJUSTMENT/TEST
_________________________________
1. General
_______
A. The adjustment of the thrust reverser is necessary for the correct compression of the fire and drain seals and the fit of the thrust reverser halves with the points on the engine and strut that touch. You must also correctly adjust the thrust reverser to correctly adjust the tension latches and latch ring for the thrust reverser.
TASK 78-31-01-825-045-N00
2. Adjustment - Thrust Reverser
____________________________
A. References
(1)
AMM 24-22-00/201, Electrical Power - Control
(2)
AMM 27-62-00/201, Speed Brake Control System
(3)
AMM 71-11-04/401, Fan Cowl Panels
(4)
AMM 71-11-06/401, Core Cowl Panels
(5)
AMM 78-31-00/201, Thrust Reverser System
(6)
AMM 78-31-02/501, Thrust Reversor Tension Latches
(7)
AMM 78-31-04/501, Thrust Reversor Tension Latches
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
B. Parts
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 501 | 1 | Shim | 78-31-01 | 01 | 95 | | | 2 | Screw | | | 100 | | | 3 | Shim | | | 105 | | | 4 | Screw | | | 115 | | | 5 | Shim | | | 120 | | | 6 | Screw | | | 125 | | | 7 | Shim | | | 150 | | | 8 | Screw | | | 155 | | | 9 | Screw | | | 160 | | | 10 | Washer | | | 165 | | | 11 | Nut | | | 170 | | | 12 | Shim | | | 175 | | | 13 | Bolt | | | 180 | | | 14 | Washer | | | 185 | | | 15 | Nut | | | 190 | | | 16 | Shim | | | 110 | | | 17 | Shim | | | 130 | | | 18 | Screw | | | 135 | | | 19 | Shim | | | 195 | | | 20 | Spacer | | | 215 | | | 21 | Screw | | | 200 | | | 22 | Washer | | | 205 | | | 23 | Nut | | | 210 | | | 24 | Shim | | | 220 | | | 25 | Spacer | | | 240 | | | 26 | Screw | | | 225 | | | 27 | Washer | | | 230 | | | 28 | Nut | | | 235 | | | 29 | Shim | | | 140 | | | 30 | Screw | | | 145 | 2.....….........…...................................…..........…......…........1
C. Consumable Materials
(1) G02020 - Modeling Clay
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
(2)
D00250 - Petroleum Jelly, White
(3)
G02039 - Transfer Dye, HYSPOT 107
(4)
B00135 - Naphtha
(5)
C00535 Primer - BMS 10-11, Type 1
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)
Access Panel
413 and 414 Fan Cowl Panels - Engine 1
417 and 418 Core Cowl Panels - Engine 1
423 and 424 Fan Cowl Panels - Engine 2
427 and 428 Core Cowl Panels - Engine 2
433 and 434 Fan Cowl Panels - Engine 3
437 and 438 Core Cowl Panels - Engine 3
443 and 444 Fan Cowl Panels - Engine 4
447 and 448 Core Cowl Panels - Engine 4
E.
Prepare for the Adjustment of the Thrust Reverser
S 045-033-N00
WARNING: DO THE DEACTIVATION PROCEDURE FOR THE SPEED BRAKE CONTROL
_______ SYSTEM. THE ACCIDENTAL MOVEMENT OF THE SPOILERS CAN CAUSE INJURIES TO PERSONS OR DAMAGE TO EQUIPMENT.
(1)
Do the deactivation procedure for the speed brake control system (AMM 27-62-00/201).
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本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊 EXHAUST 1(74)
