Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34
General Description
Od 1.350 to 1.370 in.; wall thk 0.020 in.; o/a w 0.170 to 0.210 in.; id 0.380 to 0.440 in.; surface r 0.490 to 0.510 in.; matl cobalt base ams 5537 haynes 25
