T-38 Aircraft Parts

(Page 23) End item NSN parts page 23 of 26
Part Number
NSN
NIIN
4003T77P01 Aircraft Gas Lubricating Nozzle
009051139
4014T60P01 Aircraft Gas Turbi Metallic Seal
007634161
40194 Structural Beam
005287282
40234-H-712 Dust And Moisture Protective Cap
008373711
40234H Dust And Moisture Protective Cap
008373711
4023T44P02 Nonmetallic Hose Assembly
000035533
4036T45P04 Headed Grooved Pin
010061070
405-20290-1 Quick Disconnect Coupling Half
008025123
405944-1 Electr Receptacle Connector Body
009467636
41.5524-00 Electr Receptacle Connector Body
009467636
411960-1 Annular Ball Bearing
007221185
4129015-1 Sway Brace Pylon Fitting
000433362
413510 Nonmetallic Tubing
000186602
414-00-0074-5 Thermocouple Harness
013034169
414-0074-5 Thermocouple Harness
013034169
414-290F Electrical Temperature Indicator
009565040
414-290F-143C Electrical Temperature Indicator
009565040
4141772P059 Dial Window
008660579
4141772P59 Dial Window
008660579
416H Thermal Resistor
008217832
Page: 23

Aircraft, T-38

Picture of T-38 Aircraft

The Northrop T-38 Talon is a two-seat, twin-engined supersonic jet trainer. It was the world's first supersonic trainer and is also the most produced. The T-38 remains in service as of 2017 in several air forces.

The United States Air Force (USAF) operates the most T-38s. In addition to training USAF pilots, the T-38 is used by NASA. The U.S. Naval Test Pilot School is the principal US Navy operator (other T-38s were previously used as USN aggressor aircraft until replaced by the similar Northrop F-5 Tiger II). Pilots of other NATO nations fly the T-38 in joint training programs with USAF pilots.

As of 2015, the T-38 has been in service for over 50 years with its original operator, the United States Air Force.

In 1952 Northrop began work on a fighter project, the Fang, with shoulder-mounted delta wing and a single engine. Then in 1953, representatives from General Electric Aviation's newly created Small Aircraft Engine Department showed Northrop a relatively tiny engine (around 400 lb installed wt) capable of 2,500 lb of thrust, and Northrop VP-Engineering Edgar Schmued saw the possibility of reversing the trend toward the large fighters. Schmued and chief engineer Welko Gasich decided on a small twin-engine "hot-rod" fighter, the N-156. Northrop began its N-156 project in 1954, aiming for a small supersonic fighter jet capable of operating from the US Navy's escort carriers. However, when the Navy chose not to pursue equipping its fleets in that fashion, Northrop continued the N-156 design using in-house funding, recasting it as a lightweight fighter (dubbed N-156F) and aimed at the export market.

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