32-13-11
 ALL  ú ú 01 Page 411 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 S 844-044
 (15) Lower the airplane and remove the jacks (AMM 07-11-11/201).
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 32-13-11
 ALL  ú ú 01 Page 412 ú Nov 12/01
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A
737-300/400/500MAINTENANCE MANUAL
 MAIN LANDING GEAR SHOCK STRUT DOORS - INSPECTION/CHECK
______________________________________________________
 1.  General
_______
 A.  This procedure only has an illustrations and wear limits tables which shows the data for wear limits. There are no procedures for access, removal, or installation of the parts. Refer to the Main Landing Gear Shock Strut Doors - Removal/Installation for procedures to do these tasks.
 NOTE: It is possible to remove and install the shock strut doors as an
____ assembly. The inner door are removed and installed separately.
 TASK 32-13-11-206-001
 2.  Wear Limits for the Shock Strut Door of the Main Landing Gear (Fig. 601)
_____________________________________________________________
 A.  Wear Limits for the Shock Strut
 S 226-002
 (1)  Refer to Fig. 601 for the inspection points and the wear limits table.
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 32-13-11
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A 737-300/400/500MAINTENANCE MANUAL
CENTER DOOR
SHOCK STRUT SEE A
HINGE SEE B INNER DOOR
FITTING
FITTING SEE C
A
FWD
PUSHROD
A
A
PUSHRODCENTER DOOR
C
1 (EXAMPLE) INNER DOOR
1
INNER FITTING HINGE
DOOR (2 LOCATIONS)
2
B
A-A
DESIGN LIMITS
WEAR LIMITS MAX
DIAMETER
MAX  DIA  REPLACE  REPAIR 
INDEX  WEAR  CLEAR- WORN  WORN  REPAIR 
NO.  PART NAME  DIM.  MIN  MAX  DIM.  ANCE  PART  PART  INSTR. 

BUSHING
ID 0.2495
0.2505
X 1
0.0040 BOLT
0.2485
0.2495
0.2475
X
OD
BUSHING
ID 0.4370
0.4380
X 2
0.0040 BOLT
0.4360
0.4370
0.4330
X
OD
Main Gear Shock Strut Door Wear Limits Figure 601
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 32-13-11
 ALL  ú ú 01 Page 602 ú Jul 15/92
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A
737-300/400/500MAINTENANCE MANUAL
 MAIN LANDING GEAR WING DOOR - REMOVAL/INSTALLATION
__________________________________________________
 1.  General
_______
 A.  This procedure contains two tasks:
 (1)  
The removal of the wing door on the main landing gear.

 (2)  
The installation of the wing door on the main landing gear.

 B.  
If you cannot remove the wing door easily, retract the main landing gear until you see the joints to disconnect.

 TASK 32-13-21-004-001
 2.  Main Landing Gear Wing Door Removal (Fig. 401)
___________________________________
 A.  Standard Tools and Equipment
 (1)  
Pins - Ground Lock

 B.  
References

 (1)  
AMM 32-00-01/201, Ground Lock Pins

 C.  
Access

 (1)  
Location Zones
 310 Left Main Landing Gear
 410 Right Main Landing Gear

 D.  
Prepare to Remove the Wing Door

 S 844-002
 (1)  
Make sure that the ground lockpin are installed in all landing gear (AMM 32-00-01/201).
　
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