THRUST COCKPIT CONTROL DRIVE ACTUATOR FAILS BRAKE FUNCTION TEST

THRUST COCKPIT CONTROL DRIVE ACTUATOR FAILS CIRCUIT RESISTANCE TEST

THRUST COCKPIT CONTROL DRIVE ACTUATOR FAILS NULL VOLTAGE AND PHASING TEST

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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11-6.4 THRUST COCKPIT CONTROL DRIVE ACTUATOR FAILS BRAKE FUNCTION TEST FAULT ISOLATION PROCEDURE Personnel Required: INITIAL STEP 35M20 Avionic Navigation and Flight Control Equipment Repairer. Applicable Configurations: All Reference: TM 55-1520-240-23 Tools: Electronic Repairer’s Tool Kit, Equipment Condition: NSN 5180-00-064-5178 Visual Check of CCDA performed (Task 11-6.2) Multimeter Materials: None TM 55-1520-240-T 11-6.4 END OF TASK 11-233

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