Starter, engine, gas, turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34; j79-ge-15 aircraft eng
General Description
Po/a lg 2.435 to 2.490 in.; o/a w 0.790 to 0.820 in.; pivot hole diameter 0.2008 to 0.2013 in.; pivot end od 0.910 to 0.940 in.; pivot end o/a w 0.420 to 0.440 in.; matl cres ams 5355 or 5643; heat treat rockwell c 35.0 to 42.0
