Piper 28 Aircraft - 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.
Piper continued to expand the 28 line rapidly. In 1963, the company introduced the more powerful Cherokee 235 (PA-28-235). The Cherokee 235 featured a Lycoming O-540 engine derated to 235 horsepower (175 kW) and a longer wing. It included tip tanks. The aircraft had its fuselage stretched in 1973 giving more room in the rear. In 1973 the marketing name was changed from 235 to the Charger, In 1974 to Pathfinder. Production of the Pathfinder continued until 1977. In 1979 the aircraft was given the Piper tapered wing and was again renamed the Dakota.
Piper 28 Aircraft
Light aircraft. In service since 1961 (PA-28-140 since 1964). Replacement for PA-22 Tri-Pacer and Colt. Developed in many versions with fixed gear. Licence production by AICSA, Columbia, and CHINCUL, Argentinia. Also in licence production by EMBRAER and NEIVA, Brazil, as EMB-712 Carioquinha, Tupi. PA-28-140 two seat trainer version.
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.
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.
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.
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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.
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.
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.
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