Quote for Piper Arrow Parts

Model No: Piper Arrow

Category: Rotary Wing Aircraft

Aircraft Type: Private Single Engine

Manufacturer: Piper Aircraft

Country: United States

Manufactured: 1960 to: Present

Avionics: Garmin GNS 430

Engine: 1 X Lycoming IO 360 C1C6

Power: 200 horse[Power]

Max Cruise Speed: 137 knots - 254 Km/h

Fuel Economy: 28.74 nautical mile / gallon - 14.061 kilometres / litre

Take Off Distance: 488 metre - 1,601.03 feet

Landing Distance: 463 metre - 1,519.01 feet

Max Tak eOff Weight: 6,063 Kg - 13,366 lbs

Max Payload: 435 Kg - 959 lbs

Seats Economy/General Class: 3 seats

Seats Business Class: 0

Seats First Class: 0

Thank you for your interest in the Piper Arrow aircraft and its related parts and components. The Arrow is a four-place, retractable landing gear airplane, and it serves as a variant within the Piper PA-28 Cherokee family of aircraft. The Cherokee series of aircraft first began production in 1961, and over 32,700 units have been produced to date. Like the other members of the series, the Piper Arrow is all-metal, unpressurized, and single-engined. The Arrow utilizes tricycle landing gear for ground operations, and a door installed on the right side of the fuselage allows for entrance and exiting by stepping on the wing.

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The Piper Arrow is powered by a single Lycoming IO 360 C1C6 aircraft engine producing 200 horsepower, allowing the aircraft to reach a maximum cruise speed of 137 knots. The first Arrow variant, the PA-28R-180 Arrow, was first certified on June 8, 1967, and multiple subsequent Arrow variants released over the following years leading into the 1980’s. As a light civil aircraft, the Piper Arrow features 3 seats for the pilot and passengers. Altogether, the Arrow may accommodate up to 959 pounds for its maximum payload capacity.

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