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

(Page 4) End item NSN parts page 4 of 5
Part Number
NSN
NIIN
18000 Industrial Spectacles
011400282
190631 Socket Head Cap Screw
006853492
1A232 Hexagon Plain Nut
007638927
1A7736 Nut And Bolt Retainer
008821428
1A7738 Nut And Bolt Retainer
008821428
1A7740 Nut And Bolt Retainer
008821428
1B1415 Tube Coupling Nut
013882773
1B3108 Paint Spray Gun
002618415
1B46158 Paint Spray Gun
002618415
2 0028-176 O-ring
003520321
2-020 L677-70 O-ring
003520321
2-020L677-70 O-ring
003520321
2-020L998-70 O-ring
003520321
2-115 L806-80 O-ring
011948661
2-115L1007-80 O-ring
011948661
2-115L1218-80 O-ring
011948661
2-128L677-70 O-ring
010071595
2-134L677-70 O-ring
010071600
2-145V0747-75 O-ring
001031506
2-145V1164-75 O-ring
001031506
Page: 4

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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