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INSTALL THERMOCOUPLE HARNESS ASSEMBLIES - TM-55-2840-254-23-3_368
INSTALL THERMOCOUPLE HARNESS ASSEMBLIES - TM-55-2840-254-23-3_370
TM-55-2840-254-23-3 TURBPROP Aircraft Engine Model T74-CP-700 Manual
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TM 55-2840-254-23
4-25 INSTALL THERMOCOUPLE HARNESS ASSEMBLIES (AVIM) (Continued)
4 - 2 5
2. Locate 12 o’clock position on power turbine
assembly (3). Use Indentation (4) in aft face
(5) of aft flange (6) for reference.
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