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

(Page 7) End item NSN parts page 7 of 13
Part Number
NSN
NIIN
10370042 O-ring
001651949
10374799 O-ring
001733025
10388353 Machine Screw
009844977
10405343 Quick Disconnect Coupling Half
005401268
105-01484 Tube Coupling Nut
002221912
10510579 O-ring
010050509
10510778 O-ring
001675121
1053-01-11 Packing Retainer
001715889
10543685-2 Annular Ball Bearing
002938120
10717605 Nonrechargeable Battery
009857846
1090351-12 O-ring
002483836
10937 Cable Assembly
009672413
109A032606 O-ring
006182517
10B131-59 Toggle Switch
009619920
10V60-141-010 O-ring
002483835
10V60-141-012 O-ring
002483836
10V60-141-111 O-ring
002483839
10V60-141-112 O-ring
007332208
10V60-141-123 O-ring
005791021
10V60-141-127 O-ring
002651078
Page: 7 ...

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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