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

(Page 46) End item NSN parts page 46 of 51
Part Number
NSN
NIIN
1A7896 Magnetic Machine Thread Plug
014805412
1AJC44040ADA Dial Indicating Pressure Gage
008129169
1HA11 Sensitive Switch
000340571
1HA9 Sensitive Switch
000340572
1JA2714-2 Retaining Ring
009037567
1KK529 O-ring
011543998
1KK531 O-ring
004486753
1PS12 O-ring
002259054
1PS4 O-ring
006182517
1S14597F Motor Stator
008152901
2 0028-176 O-ring
003520321
2 1/2 4-OH Needle Roller Bearing
009021641
2-007L1120-70 O-ring
005719549
2-007L677-70 O-ring
005719549
2-01238 Boss Nipple
006843578
2-01238J6 Boss Nipple
006843578
2-012N179-70 O-ring
002426628
2-013L1120-70 O-ring
007592022
2-014 L308-8 O-ring
007592113
2-014L1120-70 O-ring
007592113
Page: 46

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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