ARMY TM 9-6115-673-13&P
AIR FORCE TO 35C2-3-512-1
(4) Visually inspect the wiring harness receptacle for security, cracks, broken wires,
and other damage.
(5) Close and secure instrument panel.
b.
Testing.
(2) Release instrument panel by turning fastener, open instrument panel slowly.
(3) Disconnect alternator wiring harness plug (P1) from receptacle (J1) of control panel
connector 13, J1 pin B and EMI filter load terminal lug N, J1 pin C and TB1
connector 14, J1 pin D and TB1 connector 15, J1 pin E and TB1 connector 8, and
J1 pin F and TB1 connector 9. (MEP-531A).
resistor (R3), J1 pin B and TB1 connector 10, J1 pin D and TB1 connector 11, and
J1 pin C and load terminal lug (-). (MEP-501A).
(6) If necessary, repair wiring harness. Then connect alternator wiring harness plug to
control panel alternator wiring harness receptacle.
(7) Close and secure instrument panel.
c.
Removal.
(2) Release instrument panel by turning fastener, open instrument panel slowly.
(3) Disconnect alternator wiring harness plug from receptacle of control panel
(4) Cut cable ties as necessary.
(5) Tag and disconnect electrical leads for control panel alternator wiring harness from
terminals 8, 9, 13, 14, and 15 of TB1, and EMI filter load terminal lug N. (MEP-
531A)
(6) Tag and disconnect electrical leads for control panel alternator wiring harness from
terminals 10 and 11 of TB1, shunt resistor (R3), and load terminal lug (-). (MEP-
501A)
(7) Remove screws, lockwashers, washers, control panel alternator wiring harness,
and gasket from control panel.
(8) If necessary, remove threaded inserts from control panel.
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