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A 737-300/400/500MAINTENANCE MANUAL
NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  PART WORN REPLACE  PART WORN REPAIR  INSTR REPAIR 
DIAMETER  PER-MITTED WEAR DIM.  ANCE CLEAR-MAX DIA 
MIN  MAX 
25  BUSHING  ID  0.4375  0.4382  0.4404  0.0034 1 
BUSHING  OD  0.4365  0.4370  0.4341  X 
26  BUSHING  ID  0.3125  0.3130  0.3160  0.0040  X
BOLT  OD  0.3110  0.3120  0.3090  X 
27  BEARING  ID  0.3120  0.3125  0.3150  0.0030 X 
BOLT  OD  0.3110  0.3120  0.3090  X 
28  BUSHING  ID  0.4375  0.4382  0.4404  0.0034 1 
BUSHING  OD  0.4365  0.4370  0.4341  X 
29  BUSHING  ID  0.3125  0.3130  0.3160  0.0040 X 
BOLT  OD  0.3110  0.3120  0.3090  X 
30  BEARING  ID  0.3120  0.3125  0.3150  0.0030 X 
BOLT  OD  0.3110  0.3120  0.3090  X 
31  BUSHING  ID  0.3125  0.3132  0.3164  0.0044 1 
BOLT  OD  0.3110  0.3120  0.3090  X 
32  BUSHING  ID  0.3125  0.3132  0.3164  0.0044 1 
BOLT  OD  0.3110  0.3120  0.3090  X 
33  BEARING  ID  0.3120  0.3125  0.3150  0.0030 X 
BOLT  OD  0.3110  0.3120  0.3090  X 
34  BUSHING  ID  0.3125  0.3130  0.3160  0.0040  X 
BOLT  OD  0.3110  0.3120  0.3090 X 
35  BUSHING  ID  0.4375  0.4382  0.4404  0.0034 1 
BUSHING  OD  0.4365  0.4370  0.4341  X 
36  CAM  X 4  1.005  1.015  1.020  X 

THE WORN PART CAN BE REPAIRED. SEE THE OVERHAUL MANUAL.
REPLACE BEARING KRP144705VT WHEN INTERNAL LINER WEAR ALLOWS 0.005 RADIAL INTERNAL CLEARANCE. SEE SECTION D-D MEASURE DIMENSION Y AT MANY LOCATIONS ALONG THE FULL
LENGTH OF THE CAM.
Exhaust Gate Actuation Mechanism Wear Limits
Figure 601 (Sheet 8)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH TWO EXHAUST GATE ú

 27-51-04
 PUSHRODS.  ú CONFIG 2 ú 01 Page 609 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A12527
A
737-300/400/500MAINTENANCE MANUAL
 EXHAUST GATE ACTUATOR PUSHRODS - REPAIRS
___________________________________________
 1.  General_______
 A.  There is one task in this procedure, a repair of the pushrods for the inboard exhaust gate actuator mechanism. The repair includes the replacement of the rivets that attach the pushrod to the rod end fitting.
 TASK 27-51-04-308-001
 2.  Exhaust Gate Actuator Pushrod Repair (Fig. 801)____________________________________
 A.  Standard Tools and Equipment
 (1)  
Shear Rivets - BACR15BB4D9

 (2)  
Shear Rivets - BACR15BB5D10

 B.  
References

 (1)  
AMM 27-51-04/401, Inboard TE Flap

 C.  
Access

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

 D.  
Procedure

 S 028-002
 (1)  
Remove the pushrod for the exhaust gate actuator mechanism (AMM 27-51-04/401).

 S 358-003

 (2)  
Repair the pushrod:

 WARNING:_______DO NOT MAKE THE RIVET HOLES LARGER. YOU WILL CAUSE DAMAGE TO THE PUSHROD AND THE ROD END FITTING.
 (a)  
Remove the broken parts of the rivets from the holes in the pushrod.

 (b)  
Install the new rivets.

 S 428-004
 (3)  Install the pushrod for the exhaust gate actuator mechanism (AMM 27-51-04/401).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 27-51-04
 ALL  ú ú 01 Page 801 ú Jul 12/99
　
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