Tf-33-p-7 (c-141a/b) Aircraft Engine Parts

(Page 50) End item NSN parts page 50 of 51
Part Number
NSN
NIIN
2-078C5 Spring Pin
005505011
2-0N506-7 O-ring
005518250
2-1-2 40H Needle Roller Bearing
009021641
2-111 47-071 O-ring
006847784
2-111 N602-70 O-ring
002483839
2-111 S355-75 O-ring
001326974
2-112 S355-75 O-ring
001326976
2-112 S604-70 O-ring
009153630
004801853
2-114 L677-70 O-ring
004801853
2-114L677-7 O-ring
004801853
2-115 N506-65 O-ring
005506744
2-116 N602-70 O-ring
002483850
2-117 N602-70 O-ring
002500222
002500222
2-121 N506-65 O-ring
005764974
2-121 N602-70 O-ring
003378593
2-121N602-70 O-ring
003378593
2-123 N602-70 O-ring
005791021
2-124 N602-70 O-ring
002651074
Page: 50

Engine, Aircraft, Tf-33-p-7 (c-141a/b)

Picture of Tf-33-p-7 (c-141a/b)  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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