(d)  
Replace the parts which are not in the tolerance.

 (e)  
Install the parts.

 S 426-004-002
 (3)  Do this task: "Inboard Trailing Edge Flap Installation" (Ref 27-51-04/401).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH TWO EXHAUST GATE ú

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A 737-300/400/500MAINTENANCE MANUAL

Exhaust Gate Actuation Mechanism Wear Limits
Figure 601 (Sheet 1)

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A11356
A 737-300/400/500MAINTENANCE MANUAL
G

A-A 
BUSHING 1. BUSHING/ 
 6. BEARING/BOLT 5. ROD END/BOLT 
2. BUSHING/BOLT  7. BUSHING/BOLT

Exhaust Gate Actuation Mechanism Wear Limits
Figure 601 (Sheet 2)

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A11411
A 737-300/400/500MAINTENANCE MANUAL

15. BUSHING/BOLT
11. BUSHING/BOLT
14. BUSHING/ BUSHING
13. BEARING/CAM
16. BUSHING/BOLT
17. BEARING/BOLT
18. BUSHING/ BUSHING
20. BUSHING/ BUSHING

Exhaust Gate Actuation Mechanism Wear Limits
Figure 601 (Sheet 3)

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A11454
A 737-300/400/500MAINTENANCE MANUAL

H-H  I-I

Exhaust Gate Actuation Mechanism Wear Limits
Figure 601 (Sheet 4)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH TWO EXHAUST GATE ú

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A12027
A 737-300/400/500MAINTENANCE MANUAL

Exhaust Gate Actuation Mechanism Wear Limits
Figure 601 (Sheet 5)

EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH TWO EXHAUST GATE ú

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A12039
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 
1  BUSHING  ID  0.3766  0.3772  0.3793  0.0032 1 
BUSHING  OD 0.3756  0.3761  0.3734  X 
2 BUSHING  ID  0.2500  0.2515  0.2545  0.0050 X 
BOLT  OD  0.2485  0.2495  0.2465  X 
　
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