Starter, engine, gas turbine p/n 383242-1-8, 383934-1-2; usaf type stu-20/a34; j79-ge-15 aircraft eng
General Description
Ko/a lg 1.421 to 1.445 in.; flanged w 0.180 to 0.200 in.; flange diameter 2.340 to 2.370 in.; body o/a diameter 1.130 to 1.150 in.; flange 6 mtg holes 0.215 to 0.225 in. On 1.920 in. Bolt circle; matl cres ams 5355 or ams 5643
