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

(Page 4) End item NSN parts page 4 of 13
Part Number
NSN
NIIN
10122758 Headless Straight Pin
008343468
101235 Vacuum Regulating Valve
001066647
10123730 Pin-rivet
004004056
10123934 Blind Rivet
010148972
10128265 Ceramic Dielectr Fixed Capacitor
012422662
10133106 Unitized Semiconductor Devices
005011730
10133332 Diode Semiconductor Device
011619490
10139356 Knitted Wire Mesh
000053272
10159604 Filler Opening Cap
010416607
10159963 O-ring
013970829
10163208 O-ring
001661101
10163350 O-ring
010069034
10163352 O-ring
010069048
10163876 O-ring
004985733
10173119 Screw Thread Insert
008644958
1026-08010-34 Knitted Wire Mesh
000053272
10316C Bearing Ball
009650329
10353714 Cotter Pin
001850037
10360536 Machine Bolt
000541438
10394288-011 Electrolytic Fixed Capacitor
010743037
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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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