D.
Procedure
S 026-002
(1)
Do this task: " Wing Landing Gear Removal" (Ref 32-11-01/401).
S 216-000
(2)
Do an external inspection of the components on the wing landing gear.
(a)
Examine the shock strut, side strut, drag brace, and wheel truck for corrosion and damage.
(b)
Examine all of the pin connections on the wing landing gear for corrosion and damage.
S 226-003
(3)
Examine the fits of the aft trunnion bearing, the bearing race, the sleeve, and the trunnion journal.
(a)
Measure the parts at the locations shown in figure 601.
(b)
Compare the measured dimensions to the wear limits in figure
601.
(c)
If a part is not in tolerance, replace the part if you cannot repair it.
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S 426-004
(4) Do this task: "Wing Landing Gear Installation" (Ref 32-11-01/401).
TASK 32-11-01-216-006
3. Wing Landing Gear External Inspection (Fig. 601)_____________________________________
NOTE: This is a scheduled maintenance task.
____
A. Access
(1)
Loaction Zone
735 Wing Landing Gear, LH
745 Wing Landing Gear, RH
B.
Procedure
S 206-007
(1)
Do an external inspection of the components on the wing landing gear.
(a)
Examine the shock strut, side strut, drag brace, and wheel truck for corrosion and damage.
(b)
Examine all of the pin connections on the wing landing gear for corrosion and damage.
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MAINTENANCE MANUAL
WALKING BEAM
A A
BEARING AFT TRUNNION
ACTUATOR RETRACT JURY STRUT UPPER SIDE STRUT
BRACE DRAG
FWD
STRUT SHOCK LOWER SIDE STRUT
WHEEL TRUCK
TORSION LINKS
Wear Limits for the Wing Landing Gear Figure 601 (Sheet 1)
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MAINTENANCE MANUAL
AFT TRUNNION BEARING
A-A
Wear Limits For the Wing Landing Gear
Figure 601 (Sheet 2)
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NO. INDEX PART NAME DIM. DESIGN LIMITS WEAR LIMITS WORN PART REPLACE PART WORN REPAIR INSTR REPAIR
DIAMETER PER-MITTED WEAR DIM.5 ANCE CLEAR-MAX DIA
MIN MAX
1 BUSHING 3 ID 0.7580 0.7600 0.7620 0.0132 X
BOLT OD 0.7485 0.7490 0.747 X 1
2 SLEEVE 4 ID 5.507 5.5085 5.5132 0.0092 X 1
CYLINDER 3 OD 5.504 5.506 5.4993 X 1
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