PITCH COCKPIT CONTROL DRIVE ACTUATOR FAILS BRAKE FUNCTION TEST

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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