(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).
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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)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH TWO EXHAUST GATE ú
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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)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH TWO EXHAUST GATE ú
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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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