TM 55-1520-240-23-9
11-47
RIG ROLL, YAW OR THRUST ILCA INPUT CONNECTING LINKS
(Continued)
11-47
Do not stand, kick, or induce lateral
loads to the thrust idler. A cracked
arm will cause in-flight failure resulting
in disconnecting the thrust cockpit
driver actuator (CCDA) and the
droop eliminator potentiometers
(Without 74 ) or thrust control position
transducer (With 74 ).
NOTE
Procedure is same to rig roll, yaw,
or thrust intermediate bellcrank
connecting links. Roll connecting link
is shown here.
1.
Install first stage rig pin (T46) (1) through hole (2)
in fitting (3), four bellcranks (4, 5, 6, and 7), and
fitting (8). Pin must slide freely.
2.
Remove pin (1) from fitting (3).
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