T-38 Aircraft Parts

(Page 21) End item NSN parts page 21 of 26
Part Number
NSN
NIIN
37B201660P101 Double Angle Bracket
008312042
37B201798P101 Check Valve Sleeve
007844753
37B201897P101 Temper Bellows Assembly
007984095
37C301713P102 Speed Adjustment Guide Block
007972759
37C301828P101 Fuel Control Sensor Bellows
007954054
37C301863P101 Acceleration Lever
007865737
37C311067P101 Drain Valve Piston
003511275
37C311068P101 Drain Valve Sleeve
003511276
37C3L11068P101 Drain Valve Sleeve
003511276
37D401204P101 Accessory Gearshaft
008958463
37D401204P103 Accessory Gearshaft
008958463
37D401477P107 Temperature Linkage Support
000737246
37D401495P101 Speed Feedback Lever
000737247
37D401634P101 Stopcock Piston
007404131
37D401690P101 Flange To Tube Elbow
000204499
37D401728P102 Nonmetallic Hose Assembly
009790849
37E501237P101 Nonmetallic Hose Assembly
009790849
37E501260P105 Thermocouple Harness
013034169
37E501462G001 Drain Valve Housing
003511277
37R601161P145 Actuator Mount Cap
009663366
Page: 21

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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