C.  
Access

 (1)  
Location Zone
 522 Variable Camber Flap, LH
 523 Variable Camber Flap, LH
 524 Variable Camber Flap, LH
 525 Variable Camber Flap, LH
 526 Variable Camber Flap, LH
 532 Variable Camber Flap, LH
 533 Variable Camber Flap, LH
 534 Variable Camber Flap, LH
 535 Variable Camber Flap, LH
 536 Variable Camber Flap, LH
 537 Variable Camber Flap, LH
 622 Variable Camber Flap, RH
 623 Variable Camber Flap, RH
 624 Variable Camber Flap, RH
 625 Variable Camber Flap, RH
 626 Variable Camber Flap, RH
 632 Variable Camber Flap, RH
 633 Variable Camber Flap, RH
 634 Variable Camber Flap, RH
 635 Variable Camber Flap, RH
 636 Variable Camber Flap, RH
 637 Variable Camber Flap, RH

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-08
 ALL  ú ú 01 Page 601 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

B 
A 
B 
A 

VARIABLE CAMBER FLAP
Variable Camber Flap Actuating Linkage Wear Limits
Figure 601 (Sheet 1)

 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-08
 ALL  ú ú 01 Page 602 ú Jun 10/88
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 747-400 MAINTENANCE MANUAL
1. BEARING/TORQUE TUBE

B-B

Variable Camber Flap Actuating Linkage Wear Limits
Figure 601 (Sheet 2)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-08
 ALL  ú ú 01 Page 603 ú Jun 10/96
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

INDEX NO.  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  REPLACE WORN PART  REPAIR WORN PART  REPAIR INSTR 
DIAMETER  DIM. WEAR MITTED PER- DIA MAX CLEAR-ANCE
MIN  MAX 
1  BEARING  ID  2.6239  2.6250  2.6279  0.0045  X 
TORQUE TUBE  OD  2.6229  2.6334  2.6194  X 
1 2  BUSHING  ID  0.7725  0.7735  0.7780  0.0055  X 
SPACER  OD  0.7710  0.7725  0.7670  X 
2 2  BUSHING  ID  0.7495  0.7505  0.7550  0.0055  X 
SPACER  OD  0.7480  0.7495  0.7440  X 
3  BEARING  ID  0.5620  0.5625  0.5680  0.0065  X 
BOLT  OD  0.5610  0.5615  0.5555  X 
4  BUSHING  ID  0.5625  0.5640  0.5665  0.0050  X 
BOLT  OD  0.5610  0.5615  0.5575  X 
5  SPACER  ID  0.5620  0.5650  0.5680  0.0065  X 
BOLT  OD  0.5610  0.5615  0.5555  X 

FLAPS NO. 1E-5 AND 22-26E
FLAPS NO. 6-10 AND 17-21

Variable Camber Flap Actuating Linkage Wear Limits
Figure 601 (Sheet 3)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-81-08
 ALL  ú ú 01 Page 604 ú Oct 10/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 D. Do a Check of the Variable Camber Flap Actuating Linkage
 S 026-005
 (1)  
Do this task: "Variable Camber Flap Actuating Linkage Removal" (AMM 27-81-08/401).

 S 226-003

 (2)  
Do a check of the actuating linkage (Fig. 601):
　
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 7(142)