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PITCH COCKPIT CONTROL DRIVE ACTUATOR FAILS CIRCUIT RESISTANCE TEST
PITCH  COCKPIT  CONTROL  DRIVE  ACTUATOR FAILS  TRIM  MOTOR  TEST

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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TM   55-1520-240-T 11-6.7 PITCH COCKPIT CONTROL DRIVE ACTUATOR FAILS BRAKE FUNCTION TEST FAULT   ISOLATION   PROCEDURE Personnel   Required INITIAL  SETUP 35M20   Avionic   Navigation   and   Flight   Control 11-6.7 Applicable    Configurations: Equipment   Repairer. All Reference: TM   55-1520-240-23 Tools: Electronic  Repairer’s  Tool  Kit, NSN    5180-00-064-5178 Multimeter Equipment  Condition: Visual  Check  of  CCDA  Performed  (Task  11-6.2) Materials: None END  OF  TASK 11-236







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