27-51-05
 ALL  ú ú 01 Page 403 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
1. FOREFLAP
12. NUT (290-410 POUND- FITTING

C-C

MIDFLAP SUPPORT TRACK

MIDFLAP
0.35 INCH
(0.89 cm)
MINIMUM WING TRAILING EDGE

CLEARANCE
D-D
Outboard Foreflap Installation
Figure 401 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-05
 ALL  ú ú 01 Page 404 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 (b)  Install two strongback parts on the foreflap (Fig. 402).
 NOTE: There are 4 different part numbers for the strongbacks.
____ The correct part number is determined by the location where the strongback attaches to the foreflap. The attach holes will not align if a strongback is used in the incorrect location. The correct strongback locations are as follows:
 14ME65B00116-1 Left Wing Inboard 14ME65B00116-2 Right Wing Inboard 14ME65B00116-3 Left Wing Outboard 14ME65B00116-4 Right Wing Outboard
 (c)  Do these steps to attach the spreader bar and the load positioner to the strongbacks (Fig. 402): 1) Follow the instructions on the instruction plate on the
 spreader bar to put the adjust-a-leg sling into the correct
 position. 2) Move the counter weight to make the spreader bar level. 3) Attach the load positioner and spreader bar to the
 strongbacks.
 S 024-009
 (2)  
Remove the outboard foreflap:

 (a)  
Remove the bolts (2), washers (3 and 5) and nuts (6) which attach the foreflap lever (7) to the four midflap tracks.

 NOTE: While you remove the bolt from each track, remove the
____ bushing (4). Hold the track or it will fall into the midflap.
 (b)  
Remove the bolts (10), washers (9 and 11), and nuts (12) which attach the foreflap to the sequence carriage (Fig. 401).

 (c)  
Remove the bushings (8) from the sequence carriages.

 (d)  
Lift the foreflap from the airplane.

 NOTE: Make sure that the foreflap is held tightly during the
____ removal. The foreflap weighs approximately 175 pounds (80 kg).
 S 094-010
 (3)  Remove the support equipment from the foreflap if it is necessary.
 TASK 27-51-05-404-011
 3.  Outboard Foreflap Installation______________________________
 A. Special Tools and Equipment
 (1)  
10OHME65B00116, Trailing Edge Flap Spreader Bar

 (2)  
14ME65B00116, Outboard Foreflap Strongback (Part of Outboard Trailing Edge Flap Strongback Kit 19ME65B00116).

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-05
 ALL  ú ú 01 Page 405 ú Jun 18/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

A

Outboard Foreflap Installation Tools
Figure 402

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-05
 ALL  ú ú 01 Page 406 ú Feb 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (3)  
G27032-8 (preferred), G27032-1 (optional) Outbd Spoiler Actuator Lock

 B.
Standard Tools and Equipment

 (1)  
Load Positioner LL-5-3, Permadur Industries, P.O. Box 1032, Somerville, New Jersey 08876

 C.
Consumable Materials

 (1)  
C00259, Enamel - Primer, Green, BMS 10-11

 (2)  
A00247, Sealant - Chromate, BMS 5-95

 D.
Parts

 ~.............................................................................. | MM | | IPC | ................. ............................ | FIG | ITEM | NOMENCLATURE | SUBJECT | FIG | ITEM | ................................................................................ | 401 | 2 | Bolt | 27-51-04 | 05 | 20 | | | 3 | Washer | | | 25 | | | 4 | Bushing | | | 40 | | | 5 | Washer | | | 30 | | | 6 | Nut | | | 35 | | | 8 | Bushing (Tracks No. 1 and 8) | | 01 | 200 | | | | Bushing (Tracks No. 2 and 7) | | | 175 | | | 9 | Washer (Tracks No. 1 and 8) | | | 185 | | | | Washer (Tracks No. 2 and 7) | | | 160 | | | 10 | Bolt (Track No. 1 and 8) | | | 180 | | | | Bolt (Tracks No. 2 and 7) | | | 155 | | | 11 | Washer (Tracks No. 1 and 8) | | | 190 | | | | Washer (Tracks No. 2 and 7) | | | 165 | | | 12 | Nut (Tracks No. 1 and 8) | | | 195 | | | | Nut (Tracks No. 2 and 7) | | | 170 | 2......…........…...................................…..........….....….........1
　
中國航空網 www.k6050.com
航空翻譯 www.aviation.cn
本文鏈接地址：747-400 AMM 飛機維護手冊 飛行操縱 FLIGHT CONTROLS 4(115)