Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf stu-20/a34; j79-ge-15 aircraft eng
General Description
O/a h 0.400 to 0.420 in.; flange diameter 1.020 to 1.040 in.; o/a body diameter 0.760 to 0.780 in.; flange h 0.160 to 0.180 in.; flange grooved 0.060 to 0.080 in. W, 0.060 to 0.080 in. Dp; matl cobalt base ems 576, wi 52
