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Page Title: ENGINE TEARDOWN – NO. 1 ENGINE WIRING REMOVAL – continued
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ENGINE TEARDOWN – NO. 1 ENGINE WIRING REMOVAL – continued
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TM-1-1520-238-23-3 Helicopter Attack AH-64A Apache (NSN 1520-01-106-9519) (EIC: RHA) Manual
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ENGINE TEARDOWN – NO. 2 ENGINE WIRING REMOVA

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

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