ARMY TM 9-6115-673-13&P
AIR FORCE TO 35C2-3-512-1
TERMINATION
WIRE
NUMBER
FROM
TO
S-1
G2-1
P1-A
S-2
G2-2
P1-B
S-3
G2-3
P1-C
S-4
G2-4
P1-D
S-5
G2(+)
P1-E
S-6
G2(-)
P1-F
g. Installation.
(1)
Position adapter plate (27, Figure 5-39) with notch on LOP switch side. Then apply locking compound
(Item 6, Appendix E) to threads of bolts (24) and install adapter plate (27) on engine with washers
(26), lockwashers (25), and bolts (24).
(2)
Install rotor (21) as follows:
CAUTION
Ensure inner taper of rotor and outer taper of engine shaft are clean of
rust and oil.
(a)
Apply locking compound (Item 6, Appendix E) to threads of capscrew (19) and screw capscrew
(19) into end of engine shaft until there is approximately 3/8 in. (9.5 mm) between head of
bolt and engine shaft.
CAUTION
Do not allow capscrew (19) to contact rotor windings. If necessary, screw
the capscrew further into engine shaft.
(b) Carefully align rotor (21) and engine shaft and push rotor toward engine until shaft taper seats
inside rotor yoke casting.
CAUTION
Do not allow C-washer (20) to shift while tightening capscrew (19). This
could adversely affect the integrity of the attachment joint.
(c)
Place a new C-washer (20) between the rotor yoke casting and head of capscrew (19).
Tighten capscrew (19) until C-washer (20) starts to deform (properly deformed when .020 in.
(0.51mm) feeler gauge will slip between C-washer and yoke of rotor).
