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AFCS COMPUTER FAILS TEST 10 (YAW RATE TEST)
AFCS   COMPUTER   FAILS   TEST   12   (PRESSURE   TRANSDUCERS TEST)

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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TM    55-1520-240-T 11-5.13  AFCS  COMPUTER  FAILS  TEST  11  (NORMAL  ACCELERATION  TEST) FAULT    ISOLATION    PROCEDURE INITIAL   SETUP Applicable   Configurations: All Toots: Electronic   Repairer’s   Tool   Kit, NSN    5180-00-064-5178 Multimeter Materials: None Personnel  Required: 35M20   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) 11-5.13 GO  TO  NEXT  PAGE 11-223







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