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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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3 2  OD ID BOLT BUSHING  0.3745 0.376 0.3735 0.375 (0.951)(0.949) (0.955)(0.953)  0.369 0.381 (0.937) (0.968)  0.006 (0.015)  X  X 
4 3  OD ID BOLT BUSHING  0.3745 0.376 0.3735 0.375 (0.951)(0.949) (0.955)(0.953)  0.369 0.381 (0.937) (0.968)  0.006 (0.015)  X  X 
5 3  OD ID BOLT BUSHING  0.3745 0.3750 0.3735 0.3745 (0.951)(0.949) (0.953)(0.951)  0.3715 0.377 (0.944) (0.958)  0.006 (0.008)  X X 

Outboard Foreflap Wear Limits
Figure 601 (Sheet 4)

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 27-51-05
 ALL  ú ú 01 Page 605 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
L33883
A
747-400 MAINTENANCE MANUAL
 OUTBOARD 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 outboard aftflap.
 (1)  
The removal procedure has these parts:

 (a)  
The extension of the flaps

 (b)  
The installation of support equipment

 (c)  
The removal of the aftflap.

 (2)  
The installation procedure has these parts:

 (a)  
An examination of the parts which attach the aftflap for worn areas

 (b)  
The installation of the support equipment

 (c)  
The installation of the aftflap

 (d)  
The removal of the support equipment

 (e)  
An adjustment of the aftflap

 (f)  
The lubrication of the aftflap.

 B.  
You can remove and install an outboard 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 of the teflon layer is necessary, see Abrasion Resistant Teflon Finish - Cleaning/Painting, 51-24-04.


 TASK 27-51-06-004-001
 2.  Outboard Aftflap Removal________________________
 A.  Special Tools and Equipment
 (1)  
10OHME65B00116 Spreader Bar

 (2)  
16ME65B00116 Outboard Aftflap Strongback (part of Outboard Trailing Edge Flap Strongback Kit, 19ME65B00116)

 B.  
Standard Tools and Equipment

 (1)
Load Positioner (for 160 pounds(75 kg)) 3100T22, McMaster-Carr


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

 C.  
References


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

 (2)  
IPC 27-51-04, Fig. 5


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 27-51-06
 ALL  ú ú 01 Page 401 ú Jun 18/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
747-400
MAINTENANCE MANUAL

 (3)  
IPC 27-51-40, Fig. 1

 (4)  
IPC 27-51-40, Fig. 3

 D.
Access

 (1)  
Location Zone
 588 Outboard Flap Aftflap, LH
 688 Outboard Flap Aftflap, RH


 E.
Prepare to Remove the Outboard Aftflap


 S 864-002
 (1)  Pressurize hydraulic system No. 4 (Ref 29-11-00/201).
 S 864-027
 WARNING: MAKE SURE THAT PERSONS AND EQUIPMENT ARE CLEAR OF THE LE AND TE
_______ FLAPS AND FLAP DRIVE MECHANISMS BEFORE YOU MOVE THE FLAP CONTROL LEVER. WITH HYDRAULIC POWER REMOVED, THE FLAPS WILL MOVE AUTOMATICALLY BY ELECTRICAL POWER WHEN YOU MOVE THE FLAP CONTROL LEVER.
 (2)  
Put the flap control lever in the 30-unit detent to extend the flaps.

 S 864-004

 (3)
Release the pressure in hydraulic system No. 4 (Ref 29-11-00/201).

 F.
Remove the Outboard Aftflap


 S 494-005
 (1)  
Install the support equipment (Fig. 401):

 (a)  
Remove the screws from the strongback attach points (Fig. 401).

 (b)  
Install the two strongback parts on the aftflap.
 
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