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J79-17/17A17C aircfaft engine
distance between support arms 5.824 in.max, distance center bore of side arm to center of throttle shaft 8.776 in.max; throttle shaft thd 0.375-24UNF-2A, 0.53 min thd lg, keyway 0.095 in max wide; feedback shaft 3.305 in.max lg, thd 0.4375-20UNF-3A, 0.48 min thd lg, distance shaft center to elec receptacle center 4.60 in.nom.
as differentiated by source control dwg. no. 635E344
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 j79-17/17a17c aircfaft engine.
1. | 274E594G3 | Cage 89954 |
2. | 274E594G3 | Cage 89954 |
3. | 274E594G3 | Cage 89954 |
4. | 274E594G3 | Cage 89954 |