Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34; u/o j79-15 aircraft engine
General Description
O/a diameter 0.610 to 0.630 in.; o/a lg 1.2816 in.; body diameter 0.399 to 0.404 in.; body lg 0.541 to 0.551 in.; beginning taper diameter 0.610 to 0.630 in.; ending taper diameter 0.438 to 0.448 in.; taper lg 0.7206 to 0.7306 in.; matl cobalt base alloy, ems-575