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

(Page 7) End item NSN parts page 7 of 13
Part Number
NSN
NIIN
142C688H05 Fluid Pressure Dampener
008516818
146424-1 Cotter Pin
000673871
146424PC1 Cotter Pin
000673871
148-284 Electrical Special Purpose Cable
010113231
158198 Electrical Solenoid
012741017
158621 Electrical Solenoid
012741017
16100-050 Diode Semiconductor Device
006323511
1617180 Electrical Engine Starter
012925704
1643143 Transistor
004600982
166993 Bearing Ball
009650329
16776751-007 Electrical Special Purpose Cable
010113231
16P1106-1 Rigid Connecting Link
010549979
16P1554-30 Exhaust Pipe Flange
011189897
16VE002005-51 Liquid Quantity Transmitter
010513812
16VH302-2 Solenoid Valve
010503369
16VH302-4 Solenoid Valve
010503369
16VP126-1 Ice Detector
013593208
16VP126-4 Ice Detector
013593208
17-1INBLACK Electrical Insulation Tape
004193164
171 1-2INBLACK Electrical Insulation Tape
001502009
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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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