TM 1-1520-238-23
4-56
4.18.
ENGINE TEARDOWN – NO. 2 ENGINE WIRING REMOVAL – continued
o. Detach connector P34 (70) from anti-ice valve
receptacle L2 (71).
p. Detach connector P953 (72) from temperature
switch receptacle S126 (73).
NOTE
Helicopters with T700-GE-701C engines
installed are equipped with a digital elec-
tronic control (DEC).
q. Detach connector P42 (74) from electrical
control unit receptacle E1 (75).
r. Detach connector P46 (76) from airframe mon-
itoring receptacle E3 (77).
s. Remove wire harness assembly (78) from No.
2 engine.
4.18.4. Inspection
a. Check wire harness for broken, bent, or
burned pins (TM 55-2840-248-23).
b. Check wire harness for worn, chafed, or
burned wiring (TM 55-2840-248-23).
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M04-1336-13
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