T-39 Sabreliner Trainer/Transport

T-39 Sabreliner Trainer/Transport

Historical Snapshot

T-39 Sabreliner Trainer/Transport

A twin-jet, multipurpose aircraft, the military version of the North American Aviation Sabreliner was designated the T-39 by the U.S. Air Force and Navy.

It was designed to cruise at speeds of 500 mph (804 kph) at 40,000 feet (12,192 meters), above most weather. Its leading edge slats, swept-back wing and tail gave it a strong resemblance to the F-86 Sabre Jet and the F-100 Super Sabre. It is between the two in size, with a wingspan and length of approximately 44 feet (13 meters).

Basic configuration of the military versions provided for a crew of two and four passengers. The interior could be modified from a radar or navigational trainer configuration to that of a cargo or passenger carrier in a matter of minutes. As a cargo carrier, the aircraft could transport items weighing up to 2,300 pounds (589 kilograms) with a length of 16 feet (5 meters). Seat tie-down fittings were suitable for use as cargo rings in lashing down equipment.

The civilian version of the T-39 Sabreliner, developed in 1962, was North American’s only successful commercial aircraft, and the Sabreliner Division was established to build the new jet. The civilian version of the Sabreliner was essentially the same as the military version, but provided for installation of deicing boots, autopilot and other communications and navigation equipment not required by the armed services. It could accommodate a crew of two and up to seven passengers.

North American built a total of 599 Sabreliners, 204 of which were for the military. The company changed its name to Rockwell International in 1973 and sold its Sabreliner Division to private investors in 1983. In January 2014, Innovative Capital Holdings acquired the assets of the resulting Sabreliner Corp. and reorganized as Sabreliner Aviation.

    Technical Specifications

    First flight Sept. 16, 1958
    Wingspan 44.5 feet
    Tailspan 17.55 feet
    Wing area 342.1 square feet
    Length 44 feet
    Height 16 feet
    Empty weight 9,257 pounds; military: 9,265 pounds
    Max. gross takeoff weight 18,340 pounds; military: 17,760 pounds
    Engines Two P&W J60-P-3A; 3000 pounds of thrust
    Cruise speed 500 mph
    Cruise range (with reserve) 1,950 statute miles
    Cruise altitude Above 40,000 feet
    Single-engine cruise altitude 20,000 feet
    Fuel capacity 7,284 pounds (1,087 gallons); military: 6,864 pounds (1,056 gallons)
    Takeoff ground roll, sea level 2,500 feet
    Landing ground roll, sea level 1,850 feet
    Landing approach speed 113 mph; military: 123 mph
    Touchdown speed 107 mph; military: 113 mph