2-1.6 ROTOR BLADE SHOCK ABSORBER ISOLATION PROCEDURE

VIBRATION FREQUENCY TOO RAPID TO COUNT, VIBRATION FELT IN STRUCTURE (6/REV) (Continued)

2-1.7 LATERAL BALANCE IS 1 IPS OR GREATER DURING GROUND TRACKING

TM-55-1520-240-T-1 CH-47D Heilcopter Manual
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TM 5-1520-240-T 2-1.6 ROTOR BLADE SHOCK ABSORBER ISOLATION PROCEDURE 2-1.6 FAULT ISOLATI0N PROCEDURE INITIAL SETUP Applicable Configurations: All Tools Aircraft Mechanic’s Tool Kit, NSN 5180-00-323-4692 Materials: None Personnel Required: Medium Helicopter Repairer (2) References: TM 55-1520-240-23 TM 55-1520-240-23 Battery Connected Electrical Power On Hydraulic Power On Technical Inspector 2-14 Change 10 END OF TASK

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