TM 1-1520-238-23
4-50
4.17.
ENGINE TEARDOWN – NO. 1 ENGINE WIRING REMOVAL – continued
NOTE
Helicopters with T700-GE-701C engines
installed are equipped with a digital elec-
tronic control (DEC).
j. Detach connector P41 (48) from electrical
control unit receptacle E1 (49).
k. Remove wire harness support clamps (50)
and (51) from bleed duct (52).
(1) Hold screw (53). Remove nut (54) and wash-
er (55).
(2) Remove screw (53) from clamps (51) and
(50).
l. Detach connector P33 (56) from anti-ice valve
receptacle L1 (57).
m. Detach connector P954 (58) from temperature
switch receptacle S127 (59).
n. Detach connector P45 (60) from engine instru-
ments receptacle E3 (61).
o. Remove wire harness (62) from No. 1 engine.
4.17.4. 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).
GO TO NEXT PARAGRAPH
M04-1335-5
49
48
53
51
52
54
55
50
M04-1335-6
61
60
56
57
59
58
M04-1335-7
62
