INSTALL AND RIG THRUST CONTROL POSITION TRANSDUCER
Before the collective position sensor
rigging can be done, the mechanical
flight controls system must be rigged.
Refer to Aircraft Rigging Procedure
Disconnect electrical power (Task 1-37) prior to
connecting LVDT test harness (APP E-319).
Lay out the two test wire harnesses from test box
(18) so that they reach from the cockpit to the
flight controls closet at sta. 95.
At sta. 95, connect test wire harness plug (19)
to either red or blue marked channel (20) of the
collective pitch LVDT assembly (21), adjacent to