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时间:2011-04-02 05:43来源:蓝天飞行翻译 作者:航空
曝光台 注意防骗 网曝天猫店富美金盛家居专营店坑蒙拐骗欺诈消费者

 Make sure the No. 4 and 5 ground spoilers align in the limit of 2 degrees.

 E.
Put the Airplane Back to Its Usual Condition


 S 865-029
 (1)  
Move the speed brake lever to the DOWN position to lower the spoilers.

 S 085-031

 (2)  
Remove the protractors and the protractor stands from the spoilers.

 S 865-032

 (3)
Remove the systems A and B hydraulic power (Ref 27-62-00/201).

 S 865-033

 (4)  
Remove the electrical power (Ref 24-22-00/201).


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 27-62-12
 ALL  ú ú 02 Page 506 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 NO. 4 AND 5 GROUND SPOILER - INSPECTION/CHECK
_____________________________________________
 1.  General_______
 A.  There is one task in this procedure, an inspection of the No. 4 and 5 ground spoilers. To do the inspection you measure the diameters of the bolts, bushings, bearings and hinge fittings that attach the ground spoiler panels to the structure.
 TASK 27-62-12-226-001
 2.  No. 4 and 5 Ground Spoiler Inspection_____________________________________
 A.  Standard Tools and Equipment
 (1)  
Micrometer 0 to 1 inch

 B.  
References

 (1)  
27-62-12/401, No. 4 and 5 Ground Spoiler

 C.  
Access

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

 D.  
Procedure


 S 026-002
 (1)  
Remove the ground spoiler (Ref 27-62-12/401).

 S 226-003

 (2)  
Examine the bolts, bushings, bearings and hinge fittings for worn areas (Fig. 601):

 (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. 601.

 (d)  
Repair or replace the parts that are not in the tolerance.

 (e)  
Install the parts.

 (3)  
Install the ground spoiler (Ref 27-62-12/401).


 S 426-004
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 27-62-12
 ALL  ú ú 01 Page 601 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A

737-300/400/500
MAINTENANCE MANUAL

SEE A
SEE C PUSHROD
GROUND SPOILER
SEE B PUSHROD
SEE C
SEE B
FWD
GROUND HINGESPOILER (2 LOCATIONS)ACTUATORS
HINGE (2 LOCATIONS)
A

No. 4 and 5 Ground Spoiler Wear Limits
Figure 601 (Sheet 1)

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 27-62-12
 ALL  ú ú 01 Page 602 ú Nov 15/91
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL

NO. INDEX  PART NAME  DIM.  DESIGN LIMITS  WEAR LIMITS  WORN PART REPLACE  PART WORN REPAIR  INSTR. REPAIR 
DIAMETER  MITTED PER-DIM. WEAR  DIA.MAX ANCE CLEAR-
MIN  MAX 
1  BEARING  ID  0.4995  0.5000  0.5020  0.0025 X 
BOLT  OD  0.4990  0.4995  0.4970  1 
2  BUSHING  ID  0.5000  0.5015  0.5040  0.0040 X 
BOLT  OD  0.4990  0.4995  0.4970  X  1 
3  BEARING  ID  0.2495  0.2500  0.2515  0.0025 X 
BOLT  OD  0.2490  0.2495  0.2475  X  1 
4  BUSHING  ID  0.2500  0.2515  0.2535  0.0040  X 
BOLT  OD  0.2490  0.2495  0.2475  X  1
5  HINGE FITTING  ID  2 0.9019  2 0.9029  0.9050  0.0040 
 
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