2......…........…...................................…...........….....…........1
C. References
(1)
AMM 12-13-03/301, Engine - Servicing
(2)
AMM 71-00-00/501, Power Plant
(3)
AMM 71-11-04/201, Fan Cowl Panels
(4)
AMM 71-11-06/201, Core Cowl Panels
(5)
AMM 78-31-00/201, Thrust Reverser System
(6)
AMM 79-21-10/401, Magnetic Chip Detector
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79-21-04
ALL ú ú N02 Page 414 ú Feb 15/99
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
D. Access
(1)
Location Zone
412 Engine 1 - Main Gearbox Aft Face 6 o'clock
422 Engine 2 - Main Gearbox Aft Face 6 o'clock
432 Engine 3 - Main Gearbox Aft Face 6 o'clock
442 Engine 4 - Main Gearbox Aft Face 6 o'clock
(2)
Access Panel
415 and 416 Thrust Reverser Halves - Engine 1
425 and 426 Thrust Reverser Halves - Engine 2
435 and 436 Thrust Reverser Halves - Engine 3
445 and 446 Thrust Reverser Halves - Engine 4
E.
Prepare for the Installation
S 214-046-N00
(1) Examine the clearance between the lubrication and scavenge oil
pump (7) and the inner diameter of the main gearbox housing
(Fig. 401).
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