Tri-Pacer Specifications

Piper Tri-Pacer airplanes were first introduced in 1952 and remained in production until 1960. When buying a Tri-Pacer you could choose from four different engines. The plane was regarded as easy to fly and designed to take off and land almost anywhere. The only drawback was the lack of glide on low airspeeds, which was caused by the model's short wings.
  1. Engine and Performance

    • Tri-Pacers were powered by Lycoming engines. The engine line included the 125-HP O-290-D engine, then the 135-HP O-290-D2 engine, the 150-HP O-320-A engine, and finally the 160-HP O-320-B engine.

    Dimensions

    • The Tri-Pacer measures 20.4 feet long and 8.33 feet high. It has a wingspan measuring 29.3 feet, and the wing area measures 147.5 square feet. It uses a 74-inch two-blade propeller. The plane has a gross weight of 1,800 pounds, with an empty weight of 1,000 pounds and a a useful load of 890 pounds. The baggage allowance for the plane is 100 pounds.

    Takeoff and Landing

    • The plane has an average takeoff roll of 1,220 feet. The aircraft has a rate of climb of 725 feet per minute, and its best stalling speed is 49 miles per hour (mph).

    In Flight

    • The Tri-Pacer has a top speed of 141 mph. Its cruising speed, at 75 percent of power and 7,000 feet altitude, is 134 mph. Service ceiling, or maximum altitude, is 19,000 feet.The plane has a usable fuel capacity of 44 gallons. At 75 percent power and 7,000 feet altitude, the cruising range of the plane would be 655 miles.

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