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F100-PW-229 turbo fan engine
manifold assembly
new configuration precludes hot streaks at two locations which result in excessive augmentor aft end distress/warpage and finger seal erosion
t.o.2J-F100-54, f.53 pending; outermanifold, augmentor, assembly of
aircraft F-15 or F-16; p/n 4083223-01 is production configuration may beused indiscriminately with p/n 4082793-01 which is modified from p/n 4075541-01
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 f100-pw-229 turbo fan engine. new configuration precludes hot streaks at two locations which result in excessive augmentor aft end distress/warpage manifold assembly
1. | 4082793-01 | Cage 77445 |
2. | 4082793-01 | Cage 65065 |
3. | 4082793-01 | Cage 52661 |