Samiksha Jaiswal

Temco TT Pinto

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Top speed  555 km/h
Length  9.32 m
First flight  March 26, 1956
Wingspan  9.09 m
Engine type  Teledyne CAE J69
Manufacturer  Temco Aircraft
Temco TT Pinto Temco TT Pinto RC Groups

The Temco TT Pinto was a jet-powered, tandem two-place primary trainer aircraft built for the United States Navy by Temco Aircraft of Dallas, Texas.


Temco TT Pinto TEMCO TT1 PInto

Design and development

Temco TT Pinto Warbird Alley Temco TT1 Pinto

The Temco Model 51 had been initially proposed to the US Air Force in response to an Air Force competition for a jet-powered primary trainer, which was won by the Cessna T-37 Tweet. The concept behind the Model 51 was an attempt to provide primary training in a jet-powered aircraft. The official name for the Model 51 was the Pinto.

Temco TT Pinto Temco TT1 Super Pinto Untitled Aviation Photo 1341498

The Pinto was a mid-wing, tricycle landing gear trainer with an enclosed cockpit powered by a single Continental Motors J69-T-9 (license-built Turbomeca Marboré) jet engine. The aircraft carried no armament.

Temco TT Pinto TEMCO TT1 Pinto Untitled Aviation Photo 0349358 Airlinersnet

The TT-1s were equipped with many of the same features found in operational jets, including ejection seats, liquid oxygen equipment, speed brakes, along with typical flight controls and instrument panels. Although the flight characteristics were considered good, the "wave off" capability was rated marginal due to being slightly underpowered.

Temco TT Pinto httpsuploadwikimediaorgwikipediacommonsthu

After its first flight in 1956, the prototype was sent to the Naval Air Test Center (NATC) Patuxent River to be evaluated alongside the Beech Model 73 Jet Mentor. Fourteen of the aircraft, designated TT-1, were produced between 1955 and 1957.

AJI T-610 Super Pinto

Temco TT Pinto TheBlueprintscom Blueprints gt Modern airplanes gt Modern T

In 1968, American Jet Industries (AJI) (later to become Gulfstream Aerospace) re-engined a TT-1 Pinto, replacing the J69 with a 2,850 lbf (12.7 kN) General Electric CJ610 (the civil version of the J85), with the modified aircraft, the T-610 Super Pinto, flying on 28 June 1968. The new engine significantly increased performance, with maximum speed reaching 450 kn (518 mph; 833 km/h), and AJI marketed the aircraft as a light attack aircraft.

The prototype Super Pinto, together with drawings and production rights, were purchased by the Philippine Air Force, which planned to build the aircraft as the T-610 Cali.

Operational history

In 1959, these aircraft served in the Air Training Command at Pensacola, Florida and used in a training program demonstration testing the feasibility of using a jet-powered trainer for primary flight training.

In March 1959, Aviation Cadet E. R. Clark soloed in a TT-1, the first student in naval aviation history to solo a jet without previous experience in propeller aircraft.

By the end of 1960, the TT-1s were phased out of operations in the Naval Air Training Command and sold as surplus.


In December 2016, five of the TT-1 Pinto series still appeared on the U.S. civil roster (one with an expired certificate), down from seven, four of them Super Pintos, in 2011.

As of late 2015, one T-610 prototype was still preserved at the Philippine Air Force Museum.


TT-1 Pinto
Two-seat primary jet trainer aircraft.
American Jet Industries T-610 Super Pinto
Re-engined with 2,850 lbf (12.7 kN) General Electric CJ610-6 turbojet.


 United States
  • United States Navy
  •  Philippines
  • Philippine Air Force
  • Specifications (TT-1)

    Data from Jane's All The World's Aircraft 1956–57

    General characteristics

  • Crew: two
  • Length: 30 ft 7 in (9.33 m)
  • Wingspan: 29 ft 10 in (9.09 m)
  • Height: 10 ft 10 in (3.30 m)
  • Wing area: 150 sq ft (13.9 m2)
  • Loaded weight: 4,440 lb (2,018 kg)
  • Powerplant: 1 × Teledyne CAE YJ69-T-9 turbojet, 920 lbf (4.01 kN)
  • Performance

  • Never exceed speed: 518 mph (450 knots, 834 km/h)
  • Maximum speed: 345 mph (300 knots, 556 km/h) at 15,000 ft (4,600 m)
  • Cruise speed: 247 mph (215 knots, 398 km/h) at 25,000 ft (7,600 m)
  • Stall speed: 69 mph (60 knots, 111 km/hr)
  • Endurance: 1.5 hr
  • Service ceiling: 30,000 ft (9,145 m)
  • Rate of climb: 1,900 ft/min (9.7 m/s)
  • References

    Temco TT Pinto Wikipedia

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