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时间:2011-04-01 19:23来源:蓝天飞行翻译 作者:航空
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Do this task to depressurize hydraulic system B: "Depressurize Hydraulic System A, B, or Standby" (Ref 29-15-00/201).


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 27-51-32
 ALL  ú ú 01 Page 405 ú Nov 15/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 INBOARD FLAP TRACK FAIRINGS - ADJUSTMENT/TEST
_____________________________________________
 1.  General_______
 A.  There is one task in this procedure; an adjustment of the inboard flap track fairing.
 TASK 27-51-32-825-001
 2.  Inboard Flap Track Fairing Adjustment_____________________________________
 A.  References
 (1)  
07-11-11/201, Jack Airplane

 (2)  
24-22-00/201, Manual Control

 (3)  
27-51-00/201, Trailing Edge Flaps

 (4)  
27-51-29/401, Inboard Midflap Seal Plate

 (5)  
29-15-00/201, Hydraulic System A, B, and Standby

 (6)  
32-00-01/201, Ground Lock Assemblies

 (7)  
36-05-00/201, Pneumatic System

 B.  
Access

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

 C.  
Procedure


 S 045-002
 (1)  
Do this task: "Trailing Edge Flap System Deactivation" (Ref 27-51-00/201).

 S 225-003

 (2)  
Measure the clearance between the fairing and the inboard and the aft adjacent structure (Fig. 501).

 (a)  
The clearance must be 0.10 |0.05 inch.

 (b)  
Adjust the fairing if it is necessary.


 S 225-005
 (3)  If you installed a new fairing, measure the clearance between the forward end of the fairing and the shock strut door:
 NOTE:____The clearance must be 0.25 |0.10 inch. You must close the shock strut door to measure this clearance.
 (a)  
Do this task: "Raise Airplane" (Ref 07-11-11/201).

 (b)  
Do this task: "Apply External Power" (Ref 24-22-00/201).

 (c)  
Do this task: "Pressurize Pneumatic System Using Ground Air Source" (Ref 36-05-00/201).

 (d)  
Do this task to pressurize the hydraulic system with a hydraulic test bench: "Pressurize Hydraulic Systems A, B, or Standby" (Ref 29-15-00/201).


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 27-51-32
 ALL  ú ú 02 Page 501 ú Nov 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

SEE A
1. FAIRING
 FWD
SEE C
AA
2. FAIRING  RETAINING NUT SEE B
A
9. SUPPORT PIN 13. SUPPORT PIN 6. SUPPORT PIN  FWD
11. SUPPORT PIN
B
Inboard Flap Track Fairing Adjustment
Figure 501 (Sheet 1)

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 ALL  ú ú 01 Page 502 ú Nov 15/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
10. ATTACH  PLATE

 PIN
8. SERRATED PLATES
NUT
 FWD
4. ECCENTRIC BUSHING
BOLTS
6. SUPPORT
 PIN

C


A-A

Inboard Flap Track Fairing Adjustment
Figure 501 (Sheet 2)

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 27-51-32
 ALL  ú ú 01 Page 503 ú Nov 15/90
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 (e)  
 
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