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BOLT  OD  0.2495  0.2495  0.2480  X 
21  BEARING  ID  0.2495  0.2500  0.2515  0.0020  X 
BOLT  OD  0.2490  0.2495  0.2475 X 
22  BEARING  ID  0.2500  0.2515  0.2545  0.0050  X 
BOLT  OD  0.2490  0.2495  0.2450  X 
23  BUSHING  ID  0.3750  0.3756  0.3777  0.0032  X 
BUSHING  OD  0.3740  0.3745  0.3718 X 
24  BUSHING ID  0.2500  0.2515  0.2545  0.0050  X 
BOLT  OD  0.2490  0.2495  0.2450 X 
25  BUSHING  ID  0.2500  0.2505  0.2525  0.0030 X 
BOLT  OD  0.2490  0.2495  0.2470  X 
26  BUSHING  ID  0.3750  0.3756  0.3777  0.0032 X 
BUSHING  OD  0.3740  0.3745  0.3718  X 
27  BUSHING  ID  0.2500  0.2515  0.2545  0.0050 X 
BOLT  OD  0.2490  0.2495  0.2450  X 
28  BEARING  ID  0.2495  0.2500  0.2515  0.0020 X 
BOLT  OD  0.2490  0.2495  0.2475 X 

Exhaust Gate Actuation Mechanism Wear Limits Figure 602 (Sheet 5)
EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THREE EXHAUST GATE ú

 27-51-34
 PUSHRODS.  ú CONFIG 1 ú 01 Page 607 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A12097
A 737-300/400/500MAINTENANCE MANUAL
 S 226-006-001
 (5)  
Measure the movement of the midflap carriage:

 (a)  
Manually move the carriage forward and aft.

 (b)  
Measure the axial movement of the carriage.

 NOTE: Make sure the midflap does not move during the
____
 measurement.

 S 226-007-001
 (6)  
If the axial movement is more than 0.005 inch, do this task to replace the carriage bearing: "Outboard Midflap Carriage Removal" (Ref 27-51-44/401).

 S 416-008-001

 (7)  
Install the access panel:

 (a)  
Apply a layer of the sealant between the surfaces of the access panel and the midflap.

 (b)  
Install the access panel with the fasteners.

 S 866-009-001
 (8)  
Do this task to pressurize hydraulic system B: "Supply Hydraulic Power" (Ref 27-51-00/201).

 S 866-015-001

 (9)
Put the flap control lever in the UP detent to retract the flaps.

 S 866-010-001

 (10)
 Do this task to depressurize hydraulic system B:  "Remove Hydraulic Power" (Ref 27-51-00/201).

 TASK 27-51-34-226-011-001
 3. Outboard Trailing Edge Flap Exhaust Gate Actuation Mechanism Inspection
_______________________________________________________________________
 A. Standard Tools and Equipment
 (1)  
Micrometer 0 to 1 inch

 B.
References

 (1)  
27-51-34/401, Outboard Trailing Edge Flap

 C.
Access

 (1)  
Access Panels
 8215, 8715 Exhaust Gate Linkage Access Panel

 D.
Procedure

 S 016-012-001
 (1)  Do this task: "Outboard Trailing Edge Flap Removal" (Ref 27-51-34/401).
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. AIRPLANES WITH THREE EXHAUST GATE ú

 27-51-34
 PUSHRODS.  ú CONFIG 1 ú 02 Page 608 ú Jul 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 226-013-001
 (2)  
Measure the parts on the actuator mechanism for the exhaust gate (Fig. 602):

 (a)  
Remove the parts.

 (b)  
Use a micrometer to measure the parts.

 (c)  
Compare the dimensions you measured with the permitted dimensions shown in Fig. 602.

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