72-62-01
ALL ú ú N03 Page 420 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 402 | 37A | Fan Exit Liner Segment | 72-34-03 | 05 | 55 | | | 37B | Bolt | | | 6 | | | 37C | Fan Exit Case Flange | 72-34-00 | 05 | 60 | | | 38 | Key | | | 55 | | 403 | 11 | Angle Gearbox Housing | 72-62-01 | 10 | 10 | | | 18 | Packing | | | 5 | | | 24 | Washer | 72-62-01 | 30 | 10 | | | 27 | Support Bracket | 72-34-00 | 05 | 30 | | | 28 | Bolt (PRE-PW-SB 72-438) | | | 20 | | | 28A | Bolt (POST-PW-SB 72-438) | | | 22 | | | 28B | Keywasher (POST-PW-SB 72-438) | | | 5 | | | 28C | Pin Stop | 72-62-51 | 01 | 10 | | | 28D | Bolt | | | 5 | | | 29 | Radial Driveshaft | 72-32-01 | 05 | 25 | | | 30 | Retaining Ring | 72-62-01 | 15 | 50 | | | 31 | Plug | | | 55 | | | 32 | Packing | | | 60 | | | 33 | Retaining Ring | 72-32-01 | 05 | 20 | | | 34 | Packing | 72-62-01 | 15 | 20 | | | 35 | Plug | | | 15 | | | 36 | Bolt | | | 5 | 2.....….........…...................................…..........…......…........1
D. References
(1)
AMM 71-00-00/501, Power Plant
(2)
AMM 71-11-04/201, Fan Cowl Panels
(3)
AMM 71-11-06/201, Core Cowl Panels
(4)
AMM 72-00-00/201, N2 Rotor Manual Turn Procedure
(5)
AMM 72-34-03/401, Fan Exit Liner Segment
(6)
AMM 78-31-00/201, Thrust Reverser System
E.
Access
(1)
Location Zone
412 Engine 1 - Intermediate Case 6 o'clock
422 Engine 2 - Intermediate Case 6 o'clock
432 Engine 3 - Intermediate Case 6 o'clock
442 Engine 4 - Intermediate Case 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
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
72-62-01
ALL ú ú N02 Page 421 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
////////////////////////A / PW4000 SERIES /747-400 / ENGINES/MAINTENANCE MANUAL ////////////////////////
F. Procedure
S 424-093-N00
(1)
Install the drive shaft (20) and the drive shaft housing (5) in the
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本文链接地址:747-400 AMM 飞机维护手册 发动机 ENGINE 2(174)