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

(Page 13) End item NSN parts page 13 of 51
Part Number
NSN
NIIN
10117075 O-ring
002500235
10117080 O-ring
002638033
10117083 O-ring
002917295
10117099 O-ring
005493628
10117135 O-ring
010050509
10117252 Loop Clamp
001032945
10117271 Dust And Moi Protective Cap-plug
001712436
10117521 Sealing Plug Assembly
009869445
10117546 Dust And Moisture Protective Cap
010168180
10118574 Shim
005960277
10119437 Packing Retainer
000888719
10119444 Packing Retainer
001715074
10119492 Packing Retainer
005506742
10119493 Packing Retainer
005506743
10119542 Packing Retainer
008346676
10121225 Hexagon Castellated Plain Nut
002687292
10121232 Flat Washer
002748768
10121621 Plate Self-locking Nut
007287703
10121692 Plate Self-locking Nut
007796689
10122230 Flat Washer
013529564
Page: 13 ...

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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