Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34; j79-15 aircraft engine
General Description
Flange diameter 0.898 to 0.902 in.; flange h 0.380 to 0.420 in.; o/a lg 0.770 to 0.790 in.; bore diameter 0.289 to 0.291 in.; matl cres, qq-s-763, type 347
