F100 Pw220 (f-15c/d/e) Aircraft Engine Parts

(Page 11) End item NSN parts page 11 of 13
Part Number
NSN
NIIN
26-4100-24P Electrical Receptacle Connector
006237199
26093 O-ring
010069034
2632855-4 Bearing Ball
000442269
2640-627X2 PIECE 34 Bearing Ball
009650329
2642752 Shim
000111989
2650-3375GP1 ITEM 13,17 Screw Thread Insert
002904515
2651407 Plate Spacer
003652483
26519-1 Turbine Spark Plug
008766692
2652367 Table Lever Assembly
002795775
2661058Y242 O-ring
002799353
2664701 Sleeve Spacer
012203152
2666407 Pressure Bellows
012628027
2666429 Pin And Plate Unit
012235810
012214218
012226935
012206538
2670406 Self-aligning Plain Bearing
010069515
2671716 Annular Ball Bearing
012315952
269SPA163 Transistor
001500822
270-C-69 O-ring
002913272
Page: 11

Engine, Aircraft, F100 Pw220 (f-15c/d/e)

Picture of F100 Pw220 (f-15c/d/e)  Aircraft Engine

The Pratt & Whitney F100 (company designation JTF22) is an afterburning turbofan engine manufactured by Pratt & Whitney which powers the F-15 Eagle and F-16 Fighting Falcon.

In 1967, the United States Navy and United States Air Force issued a joint engine Request for Proposals (RFP) for the F-14 Tomcat and F-15 Eagle fighters. The combined program was called Advanced Turbine Engine Gas Generator (ATEGG) with goals to improve thrust and reduce weight to achieve a thrust-to-weight ratio of 9. The program requested proposals and would award Pratt & Whitney a contract in 1970 to produce F100-PW-100 (USAF) and F401-PW-400 (USN) engines. The Navy would cut back and later cancel its order, choosing to continue to use the Pratt & Whitney TF30 engine from the F-111 in its F-14.

The F100-100 first flew in an F-15 Eagle in 1972 with a thrust of 23,930 lbf (106.4 kN). Due to the advanced nature of engine and aircraft, numerous problems were encountered in its early days of service including high wear, stalling and "hard" afterburner starts. These "hard" starts could be caused by failure of the afterburner to start or by extinguishing after start, in either case the large jets of jet fuel were lit by the engine exhaust resulting in high pressure waves causing the engine to stall. Early problems were solved in the F100-PW-220, and the engine is still in the USAF fleet to this day.

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