ARMY TM 9-6115-464-34
AIR FORCE 35C2-3-445-2
NAVY NAVFAC P-8-624-34
NOTES:
1.
2.
3.
4.
5.
6.
LOCATE HEAD STUD AS SHOWN, 45° ± 5°
FROM ROTOR RETWIST.
SOLDERING SHALL BE IN ACCORDANCE
WITH MIL-STD-454, REQUIREMENT 5.
BAND COIL EXTENSIONS AT EACH BEND
WITH TAPE, FIND NO. 4.
BAND OUTSIDE CIRCUMFERENCE OF
WINDING WITH 9 LAYERS OF TAPE, FIND
NO. 16, AS SHOWN, UNDER 33 LBS ± 10°.
VACUUM-PRESSURE IMPREGNATE IN
ACCORDANCE WITH 72-2487.
INTERPRET DRAWING PER MlL-STD-100.
Figure 3-145. 400 Hz Generator Rotor Winding Procedures
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