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.
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Change 12
