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时间:2011-04-03 11:38来源:蓝天飞行翻译 作者:航空
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 (e)  
Install the lockspring (27) in each stop pin.

 (f)  
Do a check of the area that the stop pins hit on the stop fittings. 1) Open the door. 2) Put a piece of clay on each stop fitting. 3) Close and latch the door. 4) Open the door. 5) See that the stop pins hit the stop fittings in the


 dimensions shown in Section A-A of Fig. 501.
 S 825-014-B00
 (9)  
Adjust the snubber (7) on the bottom hinge.

 (a)  
Open the door.

 (b)  
Make the snubber longer if it keeps the door from the fully open position. 1) Remove the four bolts that hold the fitting to the


 structure. 2) Turn the rod end to change the length of the snubber. 3) Attach the fitting to the structure with the four bolts.
 S 435-015-B00
 (10)
 Install the guide pin (5).

 (a)  
Move the adjustable guide on its plate until the guide pin lightly touches the guide track when the door closes.

 (b)  
See that when the door is closed, the guide pin does not have a load on it.


 S 825-016-B00
 (11)
 Make sure the clearance at all edges of the door is correct (Fig. 502).

 (a)  
Remove material from the edge of the door if it is necessary to get the correct dimension.

 (b)  
Remove material from the edge of the gate if it is necessary to get the correct dimension. 1) Replace the finish on the area of the gate you trimmed (AMM


 51-21-51/701).
 NOTE:____The gates are made of magnesium. They will require special treatment if you trim them.
 S 825-017-B00
 (12)
 Make sure the covers on the hinge arms align with the outer contour of the fuselage.

 (a)  
Change the shims below the covers if it is necessary to align them.

 (13)
 Remove the weight from the door.


 S 095-018-B00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-13-00
 ALL  ú ú B02 Page 513 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 415-019-B00
 (14)
 Install the access panel (1) on the door.

 S 415-020-B00

 (15)
 Install the door lining (Ref 52-13-31/401).

 S 415-021-B00

 (16)
 Install the escape slide assembly (Ref 25-61-35/201).

 S 715-022-B00

 (17)
 Do this task: "Aft Entry Door Test".


 TASK 52-13-00-705-023-B00
 4.  Aft Entry Door Adjustment (Soft Unlatching) (Fig. 501)___________________________________________
 A. General
 (1)  
If the latch torque tubes are not adjusted correctly, the door handle can move too easily. This can cause the door to open accidentally (soft unlatching). This task is a special procedure to adjust the door if it opens accidentally (soft unlatching).

 B.
Standard Tools and Equipment

 (1)  
Modeling Clay

 (2)  
Rigging Simulator - Escape Slide, C52006-1

 (3)  
Vaseline

 C.
References

 (1)  
25-61-35/201, Escape Slide Assembly (Door-Mounted)

 (2)  
52-13-31/401, Forward Entry Door Lining and Insulation

 D.
Access

 (1)  
Location Zone
 110 Aft Entry Door


 E.
Procedure

 (1)  
Remove the escape slide assembly (Ref 25-61-35/201).

 (2)  
Remove the door lining (Ref 52-13-31/401).

 (3)  
Remove the access panel (1) from the door.


 S 015-024-B00
 S 015-025-B00
 S 015-026-B00
 EFFECTIVITYùùùùùùùùùùùùùùùùùùùùùùùùùùùùùù. ú

 52-13-00
 ALL  ú ú B02 Page 514 ú Nov 12/00
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 095-027-B00
 (4)  
Attach a 60-pound weight to the door approximately in the middle of the bottom half of the door.
 
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