TM 55-1520-240-23-6
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BLEED UTILITY HYDRAULIC SWIVEL LOCK SYSTEM
(Continued)
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8.
Working in cockpit, set SWIVEL switch (9) to
UNLOCK.
9.
Working at aft left landing gear, disconnect hose
(7) from cam (6).
10.
Install plug (5) in port (8) of cam (6).
11.
Repeat steps 4 thru 10 for right aft landing gear.
INSPECT
FOLLOW-ON MAINTENANCE:
Disconnect hydraulic test stand (Task 1-38).
Close aft landing gear access panels (Task 2-2).
END OF TASK
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