Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34; u/o j79-15 aircraft eng
General Description
O/a diameter 7.225 to 7.229 in.; id 6.530 to 6.540 in.; wall thk 0.090 to 0.135 in.; o/a chamber lg 7.583 to 7.613 in.; boss lg 0.575 to 0.585 in.; boss stock diameter 0.875 in.; matl cres
