Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34
General Description
O/a lg 0.605 to 0.615 in.; od 0.793 to 0.797 in.; taper diameter 0.450 to 0.470 in.; id 0.520 to 0.540 in. Tapered to 0.340 to 0.347 in.; matl carbon grade g-84