Piper PA-12 Super Cruiser

Single Engine Piston

ICAO aircraft code PA12

Manufacturer Piper Aircraft

Country United States

New price USD .003 million (1946)

The Piper PA-12 Super Cruiser is an American three-seat, high wing, single-engine conventional landing gear-equipped light aircraft that was produced by Piper Aircraft between 1946-48.

Specifications

Full description

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Piper PA-12 Super Cruiser specifications

General

ICAO aircraft code

PA12

Manufacturer

Piper Aircraft

Manufactured

1946 - 1948

Country

United States

New purchase price

USD .003 million (1946)

Aircraft performance

Engine:

1x Lycoming O-235-C
Piston

Power:

108 HP

Max Cruise Speed:

91 Kts
169 Km/h

Approach Speed (Vref):

42 Kts

Travel range:

521 Nm
965 Kilometers

Service Ceiling:

12,600 feet

Rate of Climb:

600 feet / minute
3.05meter / second

Take Off Distance:

220 meter - 721.78 feet

Landing Distance:

143 meter - 469.15 feet

Weight & dimensions

Max Take Off Weight:

795 Kg
1,753 lbs

Max Landing Weight:

795 Kg
1,753 lbs

Max Payload:

259 Kg
571 lbs

Fuel Tank Capacity:

38 gallon
144 liter

Disclaimer: The information on this page may not be accurate or current. Never use it for flight planning or any other aircraft operation purposes. No warranty of fitness for any purpose is made or implied. Flight planning or any other aircraft operations should only be done using official technical information provided by the manufacture or official aviation authorities.

About the Piper PA-12 Super Cruiser

The Piper PA-12 Super Cruiser is an American three-seat, high wing, single-engine conventional landing gear-equipped light aircraft that was produced by Piper Aircraft between 1946-48. The PA-12 was an upgraded and redesignated Piper J-5.