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

 S 825-024-B00
 (13)
 Adjust the striker pin (Fig. 504).

 (a)  
On a new door, install the striker pin fitting.

 NOTE: New doors do not have the striker pin fitting on them.
____
 1)  Use the hole on the door frame to put the fitting on the frame as shown in Fig. 504. a) Attach the striker pin to the door with a bolt, a
 washer and a self-locking nut. 2) Drill three holes (0.190 + 0.009/-0.000 inch) in the frame through the holes in the fitting. 3) Install the bolts, washers and nuts to hold the fitting to the frame (Fig. 504).
 (b)  Do a check of the adjustment of the striker pin.
 1)  While you slowly close the door, see that the striker pin hits the latch pin lever correctly. a) The striker pin must touch the latch pin lever with a
 0.50 inch overlap (Fig. 504, Section A-A). b) Adjust the latch pin lever if it is necessary to get the correct dimension (Ref 52-61-53/401).
 2)  See that the center of the striker pin is from 1.02 to 1.20 inch from the center of the lever (Fig. 504, Section B-B). a) Make the index hole in the door frame larger (0.15 inch
 maximum) if it is necessary to get the correct dimension.
 S 415-027-B00
 (14)
 Remove the weight from the door.

 (15)
 Install the access panel on the door.

 (16)
 Install the door lining (Ref 52-11-31/401).

 S 415-028-B00
 S 415-029-B00
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 52-11-00
 ALL  ú ú B04 Page 514 ú Mar 15/98
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SCUFF PLATE STRIKER PIN
B
FITTING
0.50 INCH MIN
STRIKER PIN
HEX HEAD BOLT
(NAS1103-3)
FLAT WASHER (AN960D10L) LATCH PIN
SELF-LOCKING NUT
LEVER
(NAS679A3)
DOORWAY
DOOR STRUCTURE FRAME
FWD B
A
A  A-A
LEVER (INTERNAL CONTROL LOCKED)
STRIKER PIN FITTING HOLE (4 LOCATIONS)
HORIZONTALSCUFF REFERENCE LINEPLATE 15` +0.15
1.05 INCH
-0.03 PATH OF PIN INBD STRIKER DOOR FRAME INDEX HOLE PIN LEVER (SLOT HOLE TO 0.15 INCH (INTERNAL CONTROL MAX. IF IT IS NECESSARY) NOT LOCKED)
ROTATED 90` COUNTERCLOCKWISE
B-B

Forward Entry Door Striker Pin Fitting Adjustment
Figure 504

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 52-11-00
 ALL  ú ú B08 Page 515 ú Mar 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 415-030-B00
 (17)
 Install the escape slide assembly (Ref 25-61-35/201).

 S 725-031-B00

 (18)
 Do this task: "Forward Entry Door Test".

 TASK 52-11-00-705-032-B00
 4.  Forward Entry Door Adjustment (Soft Unlatching)_______________________________________________
 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).

 (2)  
The soft unlatching adjustment and the vertical adjustment for the forward entry door are related. When you do the soft unlatching adjustment, it affects the vertical adjustment. Make sure these adjustments are within tolerance before you complete the soft unlatching adjustment procedure.

 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)  
52-11-31/401, Forward Entry Door Lining and Insulation

 D.
Access
　
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