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T-38A aircraft engine
manifold, engine fuel, rh eng
no flammable materials shall be used. dissimilar metals shall not be used. metallic surfaces shall be treated i/a/w MIL-F-7179
used to direct fuel to the main and afterburner fuel pumps of a turbo jet engine
fuel pressure will be 50 psig, fluid temperature will range from -65F to 110f, ambient temperature will range from -65F to 200f
1EA
Schedule B number: 8803909060
nmfc 133300
Other parts, for use in other military aircraft, spacecraft and spacecraft launch vehicles (excluding parts of communicat
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 t-38a aircraft engine. no flammable materials shall be used. dissimilar metals shall not be used. metallic surfaces shall be treated i/a/w mil-f-7179 manifold, engine fuel, rh eng
1. | R11525 | Cage 50599 |
2. | R11223 | Cage 50599 |