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时间:2011-04-01 19:17来源:蓝天飞行翻译 作者:航空
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BOLT  OD  0.6230  0.6240  0.6226  X 
3 ROD END  ID  0.8147  0.8157  0.8187  0.0045  X 
BUSHING  OD  0.8132  0.8142  0.8128  X 
4 BUSHING  ID  0.6250  0.6265  0.6295  0.0055  X 
BOLT  OD  0.6230  0.6240  0.6226  X 
5  BEARING  ID  0.6245  0.6250  0.6280  0.0040  X 
BOLT  OD 0.6230  0.6240  0.6226  X 

Elevator Control Linkage Wear Limits
Figure 602 (Sheet 2)

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 27-31-11
 ALL  ú ú 02 Page 606 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (2)  
Access Panels
 3701 Stabilizer Trim Access Door
 3801/3802 Tail Cone Access Door
 3806/3807 Tail Cone Cover Plate
 9105/9205 Access Panel Trailing Edge
 9107/9207 Access Panel Trailing Edge
 9108/9208 Access Panel Trailing Edge
 9109/9209 Access Panel Trailing Edge
 9128/9228 Elevator Hose Cover Lower
 9129/9229 Elevator Hose Cover Upper
 9130/9230 Elevator Hose Cover Lower
 9131/9231 Elevator Hose Cover Upper
 9132/9232 Elevator Hose Cover Lower
 9133/9233 Elevator Hose Cover Upper
 9134/9234 Elevator Hose Cover Lower
 9135/9235 Elevator Hose Cover Upper
 9136/9236 Elevator Hose Cover Lower
 9137/9237 Elevator Hose Cover Upper
 9138/9238 Elevator Hose Cover Lower
 9139/9239 Elevator Hose Cover Upper
 9140/9240 Elevator Hose Cover Lower
 9141/9241 Elevator Hose Cover Upper
 9142/9242 Removable Elevator Leading Edge Lower
 9143/9243 Removable Elevator Leading Edge Upper
 9313/9413 Elevator Mast Fitting Fairing


 F.
Procedure

 (1)  
Do this task: "Elevator Removal" (Ref 27-31-11/401).

 S 216-004

 (2)  
Examine the parts for worn areas:

 (a)  
Use a micrometer or a vernier caliper to measure the parts for the worn areas.

 (b)  
Compare the dimensions you measured with the permitted dimensions shown in Fig. 601 or 602.

 (c)  
Replace the parts that are not in the tolerance.


 S 026-002
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 ALL  ú ú 02 Page 607 ú Jul 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (d)  
If the bearings in Figure 602 need to be replaced, use the bearing retention/removal kit to replace the bearings.

 (e)  
Install the parts.


 S 426-003
 (3)  Do this task: "Elevator Installation" (Ref 27-31-11/401).
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 ALL  ú ú 02 Page 608 ú Mar 15/93
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ELEVATOR POWER CONTROL UNIT - REMOVAL/INSTALLATION
__________________________________________________
 1.  General_______
 A.  This procedure has two tasks, one for the removal and one for the installation of the elevator power control unit (which is referred to as the "PCU"). The procedure has these parts:
 (1)  
The removal of the elevator PCU

 (2)  
The installation of the replacement elevator PCU.


 TASK 27-31-14-004-018
 2.  Elevator Power Control Unit Removal___________________________________
 A.  Special Tools and Equipment
 (1)  Rig Pin (E-5) - 0.309/0.311-inch diameter, 6.7 |0.25 inches long (MS20392-4)
 
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