The Piper PA-28 Cherokee is designed and produced by Piper Aircraft as a two to four-seat civil utility aircraft introduced in 1960. It was an unpressurized light aircraft with an all-metal structure, single-piston engine, low wings, and tricycle undercarriage. Produced from 1961 up to the present, the PA-28 is used as a personal aircraft, as well as for flight training and air taxi.

Piper Aircraft
United States
1961 to: Present
US$.5 million (2019)
1x Lycoming O-320-E2A
150 horsepower
Max Cruise Speed:
108 knots
200 Km/h
Approach Speed (Vref):
47 knots
Travel range:
465 Nautical Miles
861 Kilometers
Fuel Economy:
Service Ceiling:
14,300 feet
Rate of Climb:
660 feet / minute
3.35metre / second
Take Off Distance:
502 metre - 1,646.96 feet
Landing Distance:
564 metre - 1,850.37 feet
Max Take Off Weight:
975 Kg
2,149 lbs
Max Landing Weight:
975 Kg
2,149 lbs
Max Payload:
421 Kg
928 lbs
Fuel Tank Capacity:
50 gallon
189 litre
Baggage Volume:
.6 m3 / 21 ft3
Seats - Economy / General:
4 seats
Seats - Business Class:
Seats - First Class:
Cabin Height:
1.09 metre - 3.58 feet
Cabin Width:
1.01 metre - 3.31 feet
Cabin Length:
2.5 metre - 8.20 feet
Exterior Length:
7.1 metre - 23.29 feet
Tail height:
2.22 metre - 7.28 feet
Fuselage Diameter:
1.15 metre - 3.77 feet
Wing Span / Rotor Diameter:
9.14 metre - 29.99 feet
Wing Tips:
No Winglets

Blog Mentions

Blog posts that mention the Piper PA-28 Cherokee:

In 1960, the first PA-28 was awarded the Federal Aviation Administration type certification. Aircraft production started from 1961 up to this day. Designed as a more economical substitute to the PA-24 Comanche, the PA-28 Cherokee has lesser manufacturing costs and cheaper parts that enable it to contest against the high-wing Cessna 172.

In 1961, the production of the original Cherokees designated as PA-28-150 and PA-28-160 began. In 1962, the manufacturing company built the PA-28-180 fitted with a Lycoming O-360 engine rated at 180 horsepower. The additional power enabled it to efficiently fly with four persons on board. In 1968, modifications were added such as a third window on each side and the cockpit of the aircraft was improved from push-pull engine throttle controls to quadrant levers.

In 1964, the Pa-28-140 Cherokee was introduced. It was powered by a Lycoming O-320-E2A four-cylinder, air-cooled, horizontally-opposed piston engine rated at 150 horsepower and driven by Sensenich M74DM propellers. The aircraft has a maximum speed of 123 knots, a cruise speed of 108 knots, and a stall speed of 47 knots.

The travel range is 465 nautical miles. It can fly up to 14,300 feet and can climb at a rate of 660 feet per minute. It has a takeoff distance of 502 meters and a landing distance of 564 meters. The maximum takeoff and landing weight are both 975 kg. It has a maximum payload of 421 kg and a fuel capacity of 50 gallons.

The Cherokee 140 has an external length of 7.1 meters, an external height of 1.5 meters, a tail height of 2.22 meters, and a fuselage diameter of 1.15 meters. It has a wheelbase of 1.9 meters, a wingspan of 9.14 meters, and a wing area of 15 square meters.

In 1967, the PA-28R-180 Cherokee Arrow was built. It was equipped with a constant-speed propeller and retractable undercarriage. The version was fitted with a Lycoming IO-360-B1E engine rated at 180 horsepower. Several other versions were produced afterward.

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