B.
Access
(1)
Location Zones
310 Left Main Landing Gear
410 Right Main Landing Gear
C.
Shock Strut Door Assembly Removal
S 494-001
(1)
Make sure to install the ground lock assemblies in all the landing gears (AMM 32-00-01/201).
S 034-002
(2)
Remove the attached bolts to disconnect the control rod assembly (7) for the inner door.
S 034-003
(3)
Remove the nuts, washers, and bolts to disconnect the upper (3) and the lower (5) door supports of the drag strut from the clamps (1 and 4).
S 824-004
(4)
Hold the strut door assembly.
(a)
Remove the cotter pins, nuts, washers and bolts to disconnect the upper shock strut door support (10) from the clamp (11).
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32-13-11
ALL ú ú 01 Page 401 ú Nov 12/01
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
10. UPPER SHOCK STRUT DOOR
SEE A 1. CLAMPSUPPORT SEE B11. CLAMP 3. UPPER DRAG STRUT
DOOR SUPPORT SEE D
1 16.17
1 19.15
4. CLAMP
9. CLAMP
5. LOWER DRAG STRUT DOOR SUPPORT
1 11.65 HINGE SEE E
8. LOWER SHOCK STRUT DOOR SUPPORT
1 30.02
SEE C
6. CONTROL
ROD SUPPORT SEE F
7. ADJUSTABLEEND OF SHOCK STRUT CONTROLOUTER CYLINDER ROD
INBD FWD
A
OUTER DOOR
DOOR STOP
CENTER
DOOR
0.50 (|0.10) INCH 1 DIMENSIONS FOR INITIAL POSITIONING0.10 (|0.04/0.00) INCH FWD OF DOOR SUPPORT CRADLES ON LANDING GEAR STRUCTURE
B
Main Gear Shock Strut Door Installation
Figure 401 (Sheet 1)
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32-13-11
ALL ú ú 01 Page 402 ú Oct 25/84
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
A 737-300/400/500MAINTENANCE MANUAL
SILICONE
TEE BOLTS RUBBER STRIP
SILICONE
RUBBER STRIP
9. CLAMP
12. ADJUSTABLE
SHIMS LINK
9. SHOCK STRUT DOOR SUPPORT SUPPORT ROD
MOUNTING SCREWS (4 PLACES) BOLT 1. CLAMP
CENTER DOOR NUT ROD END ATTACHMENT BOLT
ROD ATTACHMENT DRAG STRUT DOOR SUPPORT
D
C INBD FWD
CENTER DOOR
BOLT
INNER DOOR COTTER PIN ATTACHMENT BOLT NUT
7. ADJUSTABLE ROD
WASHER
INNER DOOR CONTROL ROD ASSEMBLY INNER DOOR HINGE F E
Main Gear Shock Strut Door Installation
Figure 401 (Sheet 2)
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