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ARTIFICIAL FEEL - MAGNETIC BRAKES (cont) - TM-55-1520-240-T-3_247
AFCS COMPUTER (cont)

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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TM    55-1520-240-T — CHAPTER 11 FLIGHT  CONTROLS  SYSTEMS  TROUBLESHOOTING CHAPTER  OVERVIEW  (Continued) FAILURE SYMPTOM LIST (Continued) AFCS COMPUTER SYMPTON TASK SYMPTOM TASK SYMPTOM TASK AFCS COMPUTER FAILS TEST 1 (CON- TINUITY  TEST) 11-5.2 AFCS  COMPUTER  FAILS  TEST  2  (POWER SUPPLY TEST) 11-5.2 AFCS  COMPUTER  FAILS  TEST  3  (LOGIC TEST) 11-5.2 AFCS  COMPUTER  FAILS  TEST  4  (PITCH AXIS  TEST) 11-5.2 AFCS COMPUTER FAILS TEST 5 (ROLL AXIS  TEST) 11-5.2 AFCS COMPUTER FAILS TEST 6 (YAW AXIS  TEST) 11-5.2 AFCS COMPUTER FAILS TEST 7 (DASH TEST) 11-5.2 AFCS COMPUTER FAILS TEST 8 (LONGI- TUDINAL  CYCLIC  TRIM  (LCT)  TEST) 11-5.2 AFCS COMPUTER FAILS TEST 10 (YAW RATE  TEST) 11-5.2 AFCS  COMPUTER  FAILS  TEST  11 (NORMAL ACCELERATION TEST) 11-5.2 AFCS COMPUTER FAILS TEST 12 (PRESSURE  TRANSDUCERS  TEST) 11-5.2 AFCS COMPUTER FAILS TEST 13 (BITE TEST) 11-5.2 AFCS  COMPUTER  FAILS  TEST  9  (COLLEC- TIVE  CONTROL  DRIVER  ACTUATOR (CCDA) TEST) 11-5.2 11-2.4.2 Change  2







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