AFCS COMPUTER FAILS TEST 10 (YAW RATE TEST)

AFCS COMPUTER FAILS TEST 9 (COLLECTIVE CONTROL DRIVER ACTUATOR (CCDA) TEST) (cont)

AFCS COMPUTER FAILS TEST 11 (NORMAL ACCELERATION TEST)

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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TM 55-1520-240-23. TM 55-1520-240-T 11-5.12 AFCS COMPUTER FAILS TEST 10 (YAW RATE TEST) 11-5.12 FAULT ISOLATION PROCEDURE INITIAL SETUP Applicable Configurations: All Tools: Electronic Repairer’s Tool Kit, NSN 5180-00-064-5178 Multimeter Materials: None Personnel Required: Avionic Navigation and Flight Control Equipment Repairer. References: TM 55-1520-240-23 Equipment Condition: Visual Check of AFCS Computer Performed (Task 11-5.2) TM 55-1520-240-23 D145-12455-SPA END OF TASK 11-222 Change 14

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