Pw-100 (c-17a) Aircraft F-117 Engine Parts

End item NSN parts page 1 of 5
Part Number
NSN
NIIN
003-007868-069 Socket Head Cap Screw
009887843
003-007868-080 Socket Head Cap Screw
009887844
0127-2 Key Washer
001860960
03A088-3-5 Solid Rivet
012343152
09NM-82MONEL Hexagon Self-locking Nut
002453502
09NM82 Hexagon Self-locking Nut
002453502
1-905707-2 Saddled Wire Rope Clamp
002339567
1005074PC3 Screw Thread Insert
008121894
10086613 O-ring
011060943
10109329 Hexagon Plain Nut
011195915
10112246 Solid Rivet
012343152
10116698 Packing Retainer
011312980
10117041 O-ring
001031506
10117042 O-ring
001031512
10117048 O-ring
001031987
10117462 Dust And Moistur Protective Plug
008170912
10117489 Nut And Bolt Retainer
008821428
10119147 Nonmetallic Grommet
006412651
10125755 O-ring
003520321
10163352 O-ring
010069048
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Engine, Aircraft F-117, Pw-100 (c-17a)

Picture of Pw-100 (c-17a)  Aircraft F-117 Engine

The Pratt & Whitney PW2000, also known by the military designation F117, is a series of high-bypass turbofan aero engines with a thrust range from 37,000 to 43,000 lbf (165 to 190 kN). Built by Pratt & Whitney, they were designed for the Boeing 757. As a 757 powerplant, these engines compete with the Rolls-Royce RB211.

Pratt & Whitney began working on the JT10D in October 1971 intended for the McDonnell Douglas YC-15 into the Advanced Medium STOL Transport project and the Boeing 767 then code named 7X7, which first ran in August 1974 and grew into the PW2000.

The PW2000 is a dual-spool, axial air flow, annular combustion, high by-pass turbofan with a dual-channel Full authority digital engine control (FADEC) system. It was certified in 1984 as the first civilian FADEC-controlled aviation engine.

MTU Aero Engines holds a 21.2% stake in the engine, having developed the low-pressure turbine and turbine exit casing as well as producing critical parts of the low-pressure turbine, the turbine exhaust casing, high-pressure compressor and high-pressure turbine components.

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