Serving our customers with quality and safety first.
F100-PW-100/-200 aircraft engine
length top to nozzle center 4.908 in. nom; top to flange center 2.046 in. max; 6 flange mtg holes thru 0.276 in. min, 0.286 in. max; nozzle tip dia 0.998 in. min, 1.001 in. max o/a
as differentiated by source control dwg no. 4056040
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 f100-pw-100/-200 aircraft engine.
1. | 502P931 | Cage 65065 |
2. | 502P931-03 | Cage 65065 |
3. | 502P931 | Cage 21178 |
4. | 502P931-03 | Cage 21178 |