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PITCH COCKPIT CONTROL DRIVE ACTUATOR FAILS BRAKE FUNCTION TEST
FAILURE SYMPTOM LIST

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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TM   55-1520-240-T 11-6.8  PITCH  COCKPIT  CONTROL  DRIVE  ACTUATOR FAILS  TRIM  MOTOR  TEST FAULT    ISOLATION    PROCEDURE Personnel  Required: INITIAL   SETUP 35M20   Avionic   Navigation   and   Flight   Control Equipment  Repairer. Applicable   Configurations: All Reference: TM    55-1520-240-23 Tools: Electronic   Repairer’s   Tool   Kit, NSN    5180-00-064-5178 Equipment   Condition: Visual  Check  of  CCDA  Performed   (Task   11-6.2) Multimeter Materials: None 11-6.8 END  OF  TASK 11-237/(11-238 blank)







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