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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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 ELEVATOR BALANCE PANELS - INSPECTION/CHECK
__________________________________________
 1.  General_______
 A.  This subject has one task. The task is an inspection of the elevator balance panels. The procedure has these parts:
 (1)  
The removal of the elevator balance panels

 (2)  
An inspection of the elevator balance panels

 (3)  
The installation of the elevator balance panels.


 TASK 27-31-41-206-001
 2.  Elevator Balance Panels Wear Limits Inspection (Fig. 601)______________________________________________
 A.  Standard Tools and Equipment
 (1)  
Micrometer - 0-1, 1-2 inches

 (2)  
Vernier Caliper

 B.  
References

 (1)  
27-31-41/401, Elevator Balance Panels

 C.  
Access

 (1)  
Location Zone
 704 Tail Cone
 711 Elevator and Tab, LH
 712 Elevator and Tab, RH


 (2)  
Access Panels
 3801 Tail Cone Access Door, LH
 3802 Tail Cone Access Door, RH
 9107 Access Panel Trailing Edge, LH
 9207 Access Panel Trailing Edge, RH
 9108 Access Panel Trailing Edge, LH
 9208 Access Panel Trailing Edge, RH
 9109 Access Panel Trailing Edge, LH
 9209 Access Panel Trailing Edge, RH


 D.  
Procedure

 (1)  
Do this task: "Elevator Balance Panels Removal" (Ref 27-31-41/401).

 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.


 S 026-002
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 27-31-41
 ALL  ú ú 02 Page 601 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

STABILIZER
REAR SPAR 2. AFT HINGE PIN/


(EXAMPLE)
A-A

INDEX  DESIGN LIMITS  WEAR LIMITS  WORN REPLACE  REPAIR WORN  REPAIR 
DIAMETER  WEAR PERMITTED CLEAR-MAX DIA 

NO. PART NAME  DIM.  MIN  MAX  DIM.  ANCE  PART  PART  INSTR. 
1  FORWARD HINGE HALF  ID  0.0930  0.0980  0.1040  0.0165 4  X 
FORWARD HINGE PIN  OD  0.0890  0.0900  0.0875  X 
2  AFT HINGE HALF  ID  0.1830  0.1880  0.1940  0.0175 5 X 
AFT HINGE PIN  OD 0.1790  0.1800  0.1775  X 


TOTAL PLAY IN JOINT = 0.033 INCH
TOTAL PLAY IN JOINT = 0.035 INCH

Elevator Balance Panel Wear Limits
Figure 601

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 27-31-41
 ALL  ú ú 01 Page 602 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (b)  
Compare the dimensions you measured with the permitted dimensions shown in Fig. 601.

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

 (d)  
Install the parts.


 S 426-003
 (3)  Do this task: "Elevator Balance Panels Installation" (Ref 27-31-41/401).
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 27-31-41
 ALL  ú ú 01 Page 603 ú Jul 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 ELEVATOR SEALS - ADJUSTMENT/TEST
________________________________
 1.  General_______
 A.  This procedure has one task. The task is an adjustment of the elevator seals.
 TASK 27-31-44-825-009
 2.  Adjustment - Elevator Seals___________________________
 
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