(a)
Put the main gear in the down and locked position.
(b)
Make sure that the red paint stripes on the downlock strut lower link (6) and the lower side strut (8) align.
S 844-024
(13)
Install the ground lockpins (AMM 32-00-01/201).
(14)
Lower the airplane and remove the jacks.
(15)
Depressurize the hydraulic system (AMM 29-15-00/201).
S 584-025
S 844-026
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A
737-300/400/500
MAINTENANCE MANUAL
A
8. BUSHING/
BUSHING
UPPER SIDE REACTION LINK
A STRUT BOLT ASSEMBLY
B
B
C
C
2. BUSHING/BOLT UPPER
(2 LOCATIONS) SIDE STRUT ASSEMBLY
1. BUSHING/BOLT FWD
INBD FWD
A-A
UPPER SIDE LOWER STRUT ASSEMBLY DOWNLOCK LINK ASSEMBLY
SIDE STRUT BOLT
5. BUSHING/ BOLT (2 LOCATIONS)
3. BUSHING/BOLT
(2 LOCATIONS) FWD
4. BUSHING/BOLT
(4 LOCATIONS) LOWER SIDE STRUT ASSEMBLY
9.
BUSHING/BUSHING
10.
BUSHING/BUSHING
11.
BUSHING/
B-B
BUSHING ASSEMBLY WASHER
LOWER SIDE STRUT
LOWER SIDE STRUT BOLT
NUT
7. BUSHING/BOLT (2 LOCATIONS)INBD
6. BUSHING/BOLT (2 LOCATIONS)
LOWER SIDE STRUT UNIVERSAL ASSEMBLY
C-C Main Landing Gear Side Strut Wear Limits Figure 601 (Sheet 1)
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A
737-300/400/500
MAINTENANCE MANUAL
Main Landing Gear Side Strut Wear Limits
Figure 601 (Sheet 2)
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E56574
A
737-300/400/500
MAINTENANCE MANUAL
Main Landing Gear Side Strut Wear Limits
Figure 601 (Sheet 3)
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A 737-300/400/500MAINTENANCE MANUAL
NO. INDEX PART NAME DIM. DESIGN LIMITS DIAMETER MIN MAX WEAR LIMITS PER-MITTED WEAR DIM. ANCE CLEAR-MAX DIA PART WORN REPLACE PART WORN REPAIR INSTR REPAIR
11 BUSHING BUSHING 6 4 1.6281.627 1.6261.623 0.015 1.633 1.618 X X
REFER TO OVERHAUL MANUAL FOR REPAIR INFORMATION DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN UPPER SIDE STRUT ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN REACTION LINK ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN LOWER SIDE STRUT ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN LOWER DOWN LOCK LINK ASSEMBLY DISTANCE BETWEEN FLANGE FACES OF BUSHINGS IN LOWER SIDE STRUT UNIVERSAL ASSEMBLY 737-400 AIRPLANES 737-300/-500 AIRPLANES
Main Landing Gear Side Strut Wear Limits
Figure 601 (Sheet 4)
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