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

(Page 10) End item NSN parts page 10 of 13
Part Number
NSN
NIIN
2156866 Gasket
003678756
2156866E Gasket
003678756
217741-1 Fluid Filter Body
013302708
221456 Incandescent Lamp
001557916
224132-019 Cartridge Fuse
009267445
23-411-12 Tube To Hose Straight Adapter
000755684
23-50225 Knitted Wire Mesh
000053272
2320-0063 Packing Retainer
000575709
2320-275 Grooved Clamp Coupling
003957392
2320-275BP Grooved Clamp Coupling
003957392
234-564-9201 Grooved Clamp Coupling
005655335
23711 Nonmetallic Bushing
006709708
240762 Knitted Wire Mesh
000053272
25-1009A-02B Dial Indicating Pressure Gage
008145704
25-1009A-02BXFWPD60 Dial Indicating Pressure Gage
008145704
2501459-498 Film Fixed Resistor
003329893
253587 O-ring
005506748
256197 Dial Indicating Pressure Gage
008145704
25SE Fluid Pressure Dampener
008516818
26-0402-67 O-ring
014150820
Page: 10 ...

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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