AFCS COMPUTER FAILS TEST 11 (NORMAL ACCELERATION TEST)

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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