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J79-GE-17 acft engine
anodized finish, o/a dim. approx 12.510 in. min to 12.685 in. max lg by 7.419 in. min to 7.593 in. max h, torque motor, includes feedback shaft size 0.437 in. dia by 3.289 in. min to 3.305 in. max lg, round earred flange w/3 inserts size 0.250-28 UNF-3B by 0.474 in. deep, optional 4th hole, throttle shaft size 0.656 in. dia by 1.165 in. min to 1.189 in. max lg, round earred flange w/3 inserts size 0.190-32 UNF-3B, optional 4th hole, rotates clockwise, 24 clutch teeth, servo inlet w/triangular flange
as differentiated by source control no. 635E344P03
1EA
FSC 2915 ⁓ Engine fuel system components, aircraft and missile prime movers
Note-fuel components specially designed for propulsion fuel systems, aircraft and missiles are to be placed in this fsc.
Excluding aircraft fuel tanks (fsc 1560); in-flight refueling system fuel components (fsc 1680). fuel system components not specifically designed for use with aircraft engines or missile prime-movers.
Used on j79-ge-17 acft engine.
1. | 231E230G3 | Cage 89954 |