Starter, engine, gas turbine p/n 383934-1-2, usaf type stu-20/a34
General Description
Matl cres 17-4ph, ams 5355; rockwell hardness rc 35.0 to 42.0; splined shank 2.510 to 2.530 in. Lg, splinequantity type 36, major diameter 0.3110 in., minor diameter 0.2910 in.; lever end thk 0.590 to 0.610 in.; distance between shank and lever end hole 1.584 in.; incl insert ms21209f1-15
