TM 55-1520-240-23-3
4-14
PERFORM ENGINE VIBRATION TEST
(Continued)
4-14
60.
Install three bolts (9) and new washers (30).
Torque bolts (9) to 85 inch-pounds.
61.
Remove screw (6) and adapter (4).
62.
Disconnect and remove two cables (1 and 2).
63.
Remove tape from cables and fuselage. Remove
meter (3).
FOLLOW-ON MAINTENANCE:
Close engine access cover (Task 4-50).
Close engine work platform (Task 2-2).
END OF TASK
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