Exhaust Gate Actuation Mechanism Wear Limits Figure 601 (Sheet 4)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THREE EXHAUST GATE ú

 27-51-04
 PUSHRODS.  ú CONFIG 1 ú 01 Page 605 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A12094
A 737-300/400/500MAINTENANCE 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 
15  BEARING  ID  0.3743  0.3750  0.3775  0.0030  X
BOLT  OD  0.3735  0.3745  0.3713  X 
16  BUSHING  ID  0.3750  0.3756  0.3787  0.0042  X 
BOLT  OD  0.3735  0.3745  0.3708  X 
17  BUSHING  ID  0.2500  0.2505  0.2535  0.0040  X
BOLT  OD  0.2485  0.2495  0.2460  X 
18  BEARING  ID  0.2495  0.2500  0.2525  0.0030 X 
BOLT  OD  0.2485  0.2495  0.2465  X 
19  BUSHING  ID  0.3750  0.3756  0.3777  0.0032 X 
BUSHING  OD  0.3740  0.3745  0.3718  X 
20  BUSHING  ID  0.2500  0.2505  0.2535  0.0040 X 
BOLT  OD  0.2485  0.2495  0.2460  X 
21  BEARING  ID  0.2495  0.2500  0.2525  0.0030 X 
BOLT  OD  0.2485  0.2495  0.2465  X 
22  BUSHING  ID  0.3750  0.3756  0.3777  0.0032 X 
BUSHING  OD  0.3740  0.3745  0.3718  X 
23  BUSHING  ID  0.2500  0.2505  0.2535  0.0040 X 
BOLT  OD  0.2485  0.2495  0.2460  X 
24  BEARING  ID  0.2495  0.2500  0.2525  0.0030 X 
BOLT  OD  0.2485  0.2495  0.2465  X 
25  BUSHING  ID  0.3750  0.3756  0.3770  0.0032  X
BUSHING  OD  0.3740  0.3745  0.3718  X 
26  BUSHING  ID  0.2500  0.2505  0.2535  0.0040 X 
BOLT  OD  0.2485  0.2495  0.2460  X 
27  BEARING  ID  0.2495  0.2500  0.2525  0.0030 X 
BOLT  OD  0.2485  0.2495  0.2465  X 

Exhaust Gate Actuation Mechanism Wear Limits Figure 601 (Sheet 5)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THREE EXHAUST GATE ú

 27-51-04
 PUSHRODS.  ú CONFIG 1 ú 01 Page 606 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A12095
A
737-300/400/500MAINTENANCE MANUAL
 INBOARD TRAILING EDGE FLAP - INSPECTION/CHECK
_____________________________________________
 1.  General_______
 A.  This procedure contains one task: an inspection of the inboard trailing edge flap. To do this check you measure the diameters of parts of the exhaust gate actuator mechanism.
 TASK 27-51-04-206-001-002
 2.  Inboard Trailing Edge Flap Inspection_____________________________________
 A.  Standard Tools and Equipment
 (1)  
Micrometer - 0 to 1 inch

 (2)  
Micrometer - 1 to 2 inch

 B.  
References

 (1)  
27-51-04/401, Inboard Trailing Edge Flap

 C.  
Access

 (1)  
Location Zone 309, 409 Wing Trailing Edge Inboard Flap and Spoilers

 D.  
Procedure

 S 026-002-002
 (1)  
Do this task: "Inboard Trailing Edge Flap Removal" (Ref 27-51-04/401).

 S 226-003-002

 (2)
Examine the exhaust gate actuator mechanism for worn parts:

 (a)  
Remove the parts to be examined.

 (b)  
Measure the parts.

 NOTE: Use a micrometer to measure the parts.
____
　
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