AFCS VISUAL CHECK (Continued) - TM-55-1520-240-T-3

AFCS VISUAL CHECK (Continued) - TM-55-1520-240-T-3_314

TM-55-1520-240-T-3 CH-47D Heilcopter Manual
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TM 55-1520-240-T 11-3.2 AFCS VISUAL CHECK (Continued) 11-3.2 TASK RESULT 14. Check yaw linear transducer (cpt) (19). 15. Check collective cockpit control driver actua- tor (ccda) (21). 16. Check dash actuator (22). 17. Check pitch and roil Iinear transducer (25). 18. Check longitudinal ccda (27). 18.1 Check all electrical connectors in flight con- trol closet. If transducer (19) is damaged, replace it. If either connector (10) is loose or damaged, tighten or re- place it. If wiring to either connector is damaged, replace transducer. If ccda (21) is loose or damaged, tighten or replace it as required. If connector to ccda is loose or dam- aged, tighten or replace it as required. If wiring to connector is damaged repair or replace it as re- quired. If actuator (22) is damaged, replace it. If connector (23 or 24) is loose or damaged, tighten or replace it as required. If wiring to either connector is dam- aged, repair or replace it as required. If either tranduces (25) is damaged, replace it. If any connector (26) is loose or damaged, tighten or replace it as required. If wiring to any connector is damaged, replace transducer. If ccda (27) is loose or damaged, tighten or replace it as required. If connector to ccda is loose or dam- aged, tighten or replace it as required. If wiring to connector IS damaged, repair or repiace it as re- quired. If any connector contains hydraulic fluid, clean it thoroughly. GO TO NEXT PAGE 11-46 Change 12

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