TM 55-1520-240-23-5
6-217
VIBRATION CORRECTION PROCEDURE (AVIATION VIBRATION
ANALYZER) (Continued)
6-217
FOLLOW-ON MAINTENANCE:
Remove vibration analysis equipment for (AVA)
TM 1-6625-724-13&P.
Close engine transmission fairing access cover
(Task 2-2).
Close pylon lower fairing (Task 2-2).
Close pylon hinged fairing (Task 2-2).
Install engine air inlet screen (Task 4-76).
Perform ground run (TM 1-1520-240-10).
Tasks 6-218 through 6-227 have been deleted.
END OF TASK
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Change 1