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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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