PITCH COCKPIT CONTROL DRIVE ACTUATOR FAILS TRIM MOTOR TEST

PITCH COCKPIT CONTROL DRIVE ACTUATOR FAILS BRAKE FUNCTION TEST

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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