Tf 30 Pratt & Whitney Engines And Components Parts

(Page 9) End item NSN parts page 9 of 13
Part Number
NSN
NIIN
749902 Fuel Nozzle Tip
010035572
80314 Fluid Filter Element
009425260
86026 Fuel Pump Housing
004003933
922151 Tee Head Bolt
000756136
93324-141 O-ring
004311853
C18 Profile Gage
000565918
CR2653-4-2 Blind Rivet
001658499
DC2-1235F Film Fixed Resistor
003501236
HD11829 Harness Branch Separator
005057941
HS90-4 Pin-rivet Collar
007754309
J11 Profile Gage
004500961
J58 Profile Gage
000565918
MLS100-EU04-02 Blind Rivet
001658499
MLS100EU4-2 Blind Rivet
001658499
P10491 Dust And Moisture Protective Cap
010284409
P8907 Dust And Moisture Protective Cap
010284409
PWA10766 Vented Oil Tank Cap
008004211
PWA21052 Driver
009076767
PWA21053 Wrench Assembly
009076844
PWA21054 Bearing And Bushing Inserter
009025709
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Pratt & Whitney Engines And Components, Tf 30

Picture of Tf 30 Pratt & Whitney Engines And Components

The Pratt & Whitney TF30 (company designation JTF10A) is a military low-bypass turbofan engine originally designed by Pratt & Whitney for the subsonic F6D Missileer fleet defense fighter, but this project was cancelled. It was later adapted with an afterburner for supersonic designs, and in this form it was the world's first production afterburning turbofan, going on to power the F-111 and the F-14A Tomcat, as well seeing use in early versions of the A-7 Corsair II without an afterburner. First flight of the TF30 was in 1964 and production continued until 1986.

In 1958, the Douglas Aircraft Company proposed a short-range, four-engined jet airliner to fill the gap below its new DC-8 intercontinental, known internally as the Model 2067. Intended to be marketed the DC-9, it was not directly related to the later twin-engined Douglas DC-9.

In 1960, the United States Navy selected the JT10A, designated TF30-P-1, to power the proposed Douglas F6D Missileer, but the project was canceled in April 1961. The version of the TF30 for the F-111 included an afterburner.

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