27-51-39
ALL ú ú 01 Page 424 ú Feb 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
B. Parts
~.............................................................................. | AMM | | AIPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 28 | Washer (Tracks No. 3 and 6) | 27-51-39 | 04 | 510 | | | | Washer (Tracks No. 4 and 5) | | 01 | 495 | | | 29 | Nut (Tracks No. 3 and 6) | | 04 | 515 | | | | Nut (Tracks No. 4 and 5) | | 01 | 500 | | | 30 | Upstop Support Assy (Track No. 3) | | 04 | 590 | | | | Upstop Support Assy (Track No. 4) | | 01 | 575 | | | | Upstop Support Assy (Track No. 5) | | | 580 | | | | Upstop Support Assy (Track No. 6) | | 04 | 595 | | | 31 | Washer (Tracks No. 3 and 6) | | | 545 | | | | Washer (Tracks No. 4 and 5) | | 01 | 530 | | | 32 | Nut (Tracks No. 3 and 6) | | 04 | 550 | | | | Nut (Tracks No. 4 and 5) | | 01 | 535 | | | 33 | Upstop Roller Assy (Tracks No. 3 | | 04 | 570 | | | | and 6) | | | | | | | Upstop Roller Assy (Tracks No. 4 | | 01 | 555 | | | | and 5) | | | | | | 34 | Lub Fitting (Tracks No. 3 and 6) | | 04 | 555 | | | | Lub Fitting (Tracks No. 4 and 5) | | 01 | 540 | | | 35 | Bolt Assy (Tracks No. 3 and 6) | | 04 | 525 | | | | Bolt Assy (Tracks No. 4 and 5) | | 01 | 510 | | | 36 | Bushing (Tracks No. 3 and 6) | | 04 | 575 | | | | Bushing (Tracks No. 4 and 5) | | 01 | 560 | | | 37 | Upstop Support Assy (Track No. 3) | | 04 | 580 | | | | Upstop Support Assy (Track No. 4) | | 01 | 565 | | | | Upstop Support Assy (Track No. 5) | | | 570 | | | | Upstop Support Assy (Track No. 6) | | 04 | 585 | | | 38 | Bolt (Tracks No. 3 and 6) | | | 505 | | | | Bolt (Tracks No. 4 and 5) | | 01 | 490 | | | 39 | Bolt (Tracks No. 3 and 6) | | 04 | 500 | | | | Bolt (Tracks No. 4 and 5) | | 01 | 485 | 2......…........…...................................…..........….....….........1
C. References
(1)
AMM 27-51-01/401, Inboard Flaps
(2)
AMM 27-51-39/601, Inboard Aftflap Drive Mechanism
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-39
ALL ú ú 01 Page 425 ú Oct 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL
D. Access
(1) Location Zone 563 Outboard Flap Track Fairing, Inboard Flap, LH (Track No. 3) 561 Inboard Flap Track Fairing, Inboard Flap, LH (Track No. 4) 661 Inboard Flap Track Fairing, Inboard Flap, RH (Track No. 5)
663 Outboard Flap Track Fairing, Inboard Flap, RH (Track No. 6)
E. Procedure
S 224-063
(1)
If you will install used parts, do this task: "Aftflap Drive Mechanism Inspection" (AMM 27-51-39/601).
S 424-064
(2)
Assemble the upstop fitting if it is necessary (Section E-E, Fig. 401):
(a)
Apply a layer of the grease on the bolt (35), bushing (36), and upstop roller (33).
(b)
Put the bushing in the roller.
(c)
Install the bolt through the upstop supports (37 and 30), the lubrication fitting (34), and the bushing (36).
(d)
Install the washer (31) and the nut (32).
(e)
Tighten the nut to 270-300 pound-inches (31-34 N-m).
(f)
Install the cotter pin in the nut.
S 424-065
(3)
Install the upstop fitting:
(a)
Put the upstop fitting (21) on the main carriage.
1) Attach the upstop fitting with bolts (38 and 39), washers (28) and nuts (29).
NOTE: Make sure the bolt heads are in the correct
____ direction.
(b) Tighten the two nuts (29) to 480-600 pound-inches (54-68 N-m).
TASK 27-51-39-404-066
13. Geneva Cam Installation
_______________________
A. Consumable Materials
(1)
D00633 Grease - BMS 3-33 (recommended)
(2)
D00013 Grease - MIL-G-23827 (alternative)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú
27-51-39 中國(guó)航空網(wǎng) www.k6050.com 航空翻譯 www.aviation.cn 本文鏈接地址：747-400 AMM 飛機(jī)維護(hù)手冊(cè) 飛行操縱 FLIGHT CONTROLS 5(91)
