Tf33-100 (e3a/b/c) Aircraft Engine Parts

(Page 12) End item NSN parts page 12 of 13
Part Number
NSN
NIIN
144-5 O-ring
002483836
145545 O-ring
002917295
14604 Gasket
011759232
14A Nonrechargeable Battery
009857846
150-6408432 FIN Wire Rope Swaging Sleeve
001329163
1503-12 Nonmetallic Hose
005951089
1513-12-20 Nonmetallic Hose
005951089
153-0013-003 Flat Washer
005843782
154433 Bearing Ball
001839164
1547 Electrical Plug Connector
010123066
155-1228 O-ring
002651078
155-122B O-ring
002651078
155-S5-12D Quick Disconnect Coupling Half
005401268
15525-12D Quick Disconnect Coupling Half
005401268
155643 Packing Retainer
001715889
1557052-24 O-ring
005312070
1557052-27 O-ring
005312068
155S5-12D Quick Disconnect Coupling Half
005401268
Page: 12

Engine, Aircraft, Tf33-100 (e3a/b/c)

Picture of Tf33-100 (e3a/b/c)  Aircraft Engine

The Pratt & Whitney JT3D is an early turbofan aircraft engine derived from the Pratt & Whitney JT3C turbojet. It was first run in 1958 and was first flown in 1959 under a B-45 Tornado test aircraft. Over 8,000 JT3Ds were produced between 1959 and 1985. Most JT3D engines still in service today are used on military aircraft, where the engine is referred to by its USAF designation of TF33.

Aware of the competition from the Rolls-Royce Conway turbofan, Pratt&Whitney decided to develop the JT3D turbofan from the JT3C turbojet for later deliveries of the Boeing 707 and the Douglas DC-8, then nearing entry into service. A 2-stage fan replaced the first 3 stages of the 9-stage JT3C LP compressor. On the LP turbine, the second stage was enlarged and a third stage added.

Unlike GE with the CJ805-23, Pratt & Whitney had not undertaken any transonic fan research prior to designing the JT3D, so they were unable to incorporate a single stage unit into the specification. Instead P&W designed a 2-stage unit based on some research they had done to support the J91 nuclear turbojet.

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