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

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Part Number
NSN
NIIN
10109329 Hexagon Plain Nut
011195915
10823-00195 Hexagon Plain Nut
007638927
15066 Hexagon Plain Nut
007638927
1A232 Hexagon Plain Nut
007638927
2HE994 Hexagon Plain Nut
007638927
3378579 Hexagon Plain Nut
007638927
5310009651800 Hexagon Plain Nut
009651800
7-660-260008 Hexagon Plain Nut
007638927
D322724 ITEM 100 Hexagon Plain Nut
007638927
E104555 FIND 95 Hexagon Plain Nut
007638927
E108165 FIND NO 128 Hexagon Plain Nut
007638927
E108165 PART NO 128 Hexagon Plain Nut
007638927
FFN836 Hexagon Plain Nut
009651800
MS35690-710 Hexagon Plain Nut
009651800
MS51971-10 Hexagon Plain Nut
007638927
MS51971-4 Hexagon Plain Nut
009651800
N0227P00039 Hexagon Plain Nut
007638927
NAS1423-12C Hexagon Plain Nut
011195915
NAS1423C12 Hexagon Plain Nut
011195915
WG105264 Hexagon Plain Nut
007638927
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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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