Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34; u/o j79-ge-15 aircraft eng
General Description
Flange diameter 1.360 to 1.370 in.; flange w 0.060 to 0.064 in.; body diameter 1.150 to 1.170 in.; taper diameter 0.420 to 0.440 in.; body id 0.341 to 0.347 in.; o/a h 0.470 to 0.490 in.; body wall thk 0.060 to 0.080 in.; matl cobalt base, ems 575, haynes 25
