Starter, engine, gas turbine p/n 383242-1-7; usaf type stu-20/a34; j79-15 aircraft engine
General Description
Boss matl cres, type 410, ams 5613; chamber matl cres, type 410, ams 5504; o/a lg 7.008 to 7.028 in.; o/a diameter 7.225 to 7.229 in.; boss projection from chamber 0.573 to 0.585 in.; boss diameter 0.875 in.; chamber id 6.530 to 6.540 in.
