32-11-11
ALL ú ú 01 Page 427 ú Mar 12/02
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A
737-300/400/500MAINTENANCE MANUAL
MAIN LANDING GEAR TRUNNION LINK - INSPECTION/CHECK
__________________________________________________
1. General_______
A. This procedure only has illustration and a wear limits table which shows the data for wear limits. There are no procedures for the access, the removal, or the installation of the parts. Refer to the Main Landing Gear Trunnion Link - Removal/Installation for procedures to do these tasks.
TASK 32-11-11-206-001
2. Wear Limits for the Trunnion Link of the Main Landing Gear (Fig./601)__________________________________________________________
A. Wear Limits for the Trunnion Link
S 226-002
(1) Refer to Fig. 601 for the inspection points and the wear limits table.
ACTUATOR BEAM
ASSEMBLY
13. BUSHING/BUSHING
TRUNNION LINK ARM ASSEMBLY ACTUATOR BEAM ASSEMBLY
MAIN LANDING UPPER DRAG STRUT
GEAR SHOCK ATTACH BOLT
TRUNNION LINK
B
STRUT ASSEMBLY ASSEMBLY
A
B
2. BUSHING/BOLT (2 LOCATIONS)A DRAG STRUT
ASSEMBLY
INBD FWDINBD
1. BUSHING/BOLT (2 LOCATIONS)
UPPER DRAG STRUT ASSEMBLY
A-A
Main Landing Gear Trunnion Link Assembly Wear Limits
Figure 601 (Sheet 1)
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32-11-11
ALL ú ú 01 Page 601 ú Nov 15/94
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A 737-300/400/500MAINTENANCE MANUAL
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32-11-11
ALL ú ú 01 Page 602 ú Jul 15/94
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A 737-300/400/500MAINTENANCE MANUAL
12. BUSHING/BOLT
12. BUSHING/BOLT(2 LOCATIONS) BOLT (2 LOCATIONS) BOLT
TRUNNION PIN
FWD
TRUNNION PINASSEMBLY ASSEMBLY
INBD BALL/BOLT
INBD BALL/BOLT
FOR ASSEMBLIES USING 1" DIA BOLT FOR ASSEMBLIES USING 1.25" DIA BOLT D-D
D-D
Main Landing Gear Trunnion Link Assembly Wear Limits
Figure 601 (Sheet 3)
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32-11-11
ALL ú ú 01 Page 603 ú Mar 15/95
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E32706
A
737-300/400/500
MAINTENANCE MANUAL
Main Landing Gear Trunnion Link Assembly Wear Limits
Figure 601 (Sheet 4)
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32-11-11
ALL ú ú 01 Page 604 ú Nov 15/94
BOEING PROPRIETARY - Copyright (C) - Unpublished Work - See title page for details.
E32738
A
737-300/400/500
MAINTENANCE MANUAL
Main Landing Gear Trunnion Link Assembly Wear Limits
Figure 601 (Sheet 5)
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32-11-11
ALL ú ú 01 Page 605 ú Nov 15/94
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E32752
A
737-300/400/500
MAINTENANCE MANUAL
REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION MAXIMUM PLATING BUILD UP 0.010. REFER TO OVERHAUL MANUAL FOR PLATING INFORMATION DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN UPPER DRAG STRUT ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN TRUNNION LINK ASSEMBLY DISTANCE BETWEEN INNER LUG FACES ON SHOCK STRUT OUTER CYLINDER ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN ACTUATOR BEAM ARM ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN SHOCK STRUT OUTER CYLINDER ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN REACTION LINK UNIVERSAL ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN TRUNNION PIN ASSEMBLY USE 69-53852-1 IF AND AS REQUIRED. REMOVE 0.003 LAMINATIONS AS REQUIRED TO OBTAIN
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