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plumbing installation fuel, lockheed dwg no. 770846-1, aircraft, F104
0.900 in. o/a lg, 2.250 in. od, 1.309 in. min, 1.315 in. max body id, 0.272 in. dia 4 holes 2.375 in. center to center distance between holes along w and h, operating pressure 50 psi, proof pressure 120 psi, bursi pressure 180, temperature range M65 deg f to P250 deg f
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 plumbing installation fuel,lockheed dwg no. 770846-1,aircraft,f104.
1. | 315100 | Cage 96124 |
2. | 634127-1 | Cage 98897 |