Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34
General Description
O/a lg 0.975 to 0.995 in.; od 0.359 to 0.361 in.; 2 inserts ms21209f1-20 in each end; thru hole perpendicular tothru bore 0.150 to 0.180 in. Dia; 0.470 to 0.530 in. Hole c to end; matl cres, mil-s-7720, type 303
