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

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Filter By: Electrolytic Fixed Capacitors
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Part Number
NSN
NIIN
10394288-011 Electrolytic Fixed Capacitor
010743037
111D505X8200M1 Electrolytic Fixed Capacitor
010743037
29F2210G2 Electrolytic Fixed Capacitor
010743037
5E1570/02-1022 Electrolytic Fixed Capacitor
011950668
M39003/01-2158 Electrolytic Fixed Capacitor
013052915
M39003/01-2397 Electrolytic Fixed Capacitor
013052915
M39003/01-2637 Electrolytic Fixed Capacitor
013052915
M39003/01-3117 Electrolytic Fixed Capacitor
013052915
M39003/01-3118 Electrolytic Fixed Capacitor
013052915
M39003/01-8262 Electrolytic Fixed Capacitor
013052915
M39003/09-0354 Electrolytic Fixed Capacitor
011950668
M39006-04-1276 Electrolytic Fixed Capacitor
010743037
M39006/04-1321 Electrolytic Fixed Capacitor
010743037
M39006/04-1366 Electrolytic Fixed Capacitor
010743037
MIL-C-39003/1 Electrolytic Fixed Capacitor
013052915
MIL-C-39003/9 Electrolytic Fixed Capacitor
011950668
MIL-C-39006/4 Electrolytic Fixed Capacitor
010743037
Page:

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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