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时间:2011-04-10 10:01来源:蓝天飞行翻译 作者:航空
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 S 426-004
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 27-51-02
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400 MAINTENANCE MANUAL
FOREFLAP
AFTFLAP
SEE A
MIDFLAP
FWD

FOREFLAP
MIDFLAP
FWD
A
FOREFLAP BOLT
LEVER
A
MIDFLAP TRACK (3 LOCATIONS)
A
Inboard Foreflap Wear Limits Figure 601 (Sheet 1)
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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

747-400
MAINTENANCE MANUAL


2. FLANGED
LEVER
BUSHING/BOLT
NO. 1 INDEX  BOLT BUSHING OD ID PART NAME DIM.  (1.269) (1.270) (1.267) (1.269) 0.4995 0.5000 0.4990 0.4995 DESIGN LIMITS (cm)(cm) MINIMUM INCHES INCHES MAXIMUM DIAMETER  (1.252) (1.283) 0.493 0.505 WEAR LIMITS (cm) INCHES DIMENSION WEAR PERMITTED  (0.015) 0.0060 (cm) INCHES CLEARANCE DIAMETER MAXIMUM  REPLACE WORN PART X  REPAIR WORN PART INSTR REPAIR 

2  FLANGED BUSHING ID BOLT OD  (1.269) (1.270) (1.267) (1.269) 0.4995 0.5000 0.4990 0.4995  (1.252) (1.283) 0.493 0.505  (0.015) 0.0060  X 

Inboard Foreflap Wear Limits
Figure 601 (Sheet 2)

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BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400 MAINTENANCE MANUAL
 INBOARD AFTFLAP - REMOVAL/INSTALLATION
______________________________________
 1.  General_______
 A.  There are two tasks in this procedure. There is one task for the removal and one task for the installation of the inboard aftflap.
 (1)
The removal procedure has these parts:

 (a)
The extension of the trailing edge flaps

 (b)
The installation of the support equipment

 (c)
The removal of the aftflap.

 (2)
The installation procedure has these parts:

 (a)
A check of the parts which attach the aftflap for worn areas

 (b)
The installation of the aftflap

 (c)
The adjustment of the aftflap

 (d)
The lubrication of the aftflap.

 B.  
You can remove and install an inboard aftflap, together with the midflap, or independently of the midflap.

 C.  
Some of the aftflap is finished with an abrasion resistant teflon layer. If repair to the teflon layer is necessary, see Abrasion Resistant Teflon Finish - Cleaning/Painting, 51-24-04.


 TASK 27-51-03-004-001
 2.  Inboard Aftflap Removal_______________________
 A.  Special Tools and Equipment
 (1)
10OHME65B00116 Trailing Edge Flap Spreader Bar and Sling

 (2)  
12ME65B00116 Inboard Aftflap Strongback (part of 18ME65B00116 -Inboard Trailing Edge Flap Strongback Kit)

 B.  
Standard Tools and Equipment

 (1)
Load Positioner (for 290 pounds (130 kg)), 3100T21, McMaster-Carr


 P.O.
 Box 54960, Los Angeles, California 90054

 C.  
References


 (1)
29-11-00/201, Main Hydraulic Supply System

 (2)
IPC 27-51-01, Fig. 5

 (3)
IPC 27-51-39, Fig. 1

 (4)
IPC 27-51-39, Fig. 4

 D.  
Access

 (1)  
Location Zone
 578 Inboard Flap Aftflap, LH
 678 Inboard Flap Aftflap, RH

 

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