TM 55-1520-240-23-3
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INSTALL AND RIG THRUST CONTROL POSITION TRANSDUCER
ASSEMBLY
(Continued)
4-153
28.
Open ENGINE NO. 1 OIL PRESS circuit breaker
(35) on the No. 1 AC PDP.
29.
Remove electrical power from the aircraft (Task
1-37).
30.
Set the BATT switch (27) to OFF.
31.
Remove hydraulic power from the aircraft (Task
1-38).
32.
Disconnect and remove the LVDT test harness.
Close the No. 1 PDP and tighten six fasteners.
33.
Stow the appropriate channel of the collective
pitch LVDT assembly.
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