Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34; j79-ge-15 aircraft eng
General Description
O/a lg 0.950 to 0.970 in.; od 0.406 to 0.407 in.; flange diameter 0.580 to 0.590; flange h 0.040 to 0.060 in.; sleeve id 0.313 to 0.314 in.; ball od 0.3115 to 0.3135 in.; matl cobalt base
