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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.

Aircraft Model Piper Arrow Details

Model No : Piper Arrow
Aircraft Type : Private Single Engine
Manufacturer : Piper Aircraft
Country : United States
Manufactured : 1960 to: Present
ICAO : NA
Avionics : Garmin GNS 430
Engine : 1 X Lycoming IO 360 C1C6
Power : 200 horse[Power]
Max Cruise Speed : 137 knots - 254 Km/h
Approach Speed : NA
Travel Range : NA
Fuel Economy : 28.74 nautical mile / gallon - 14.061 kilometres / litre
Service Ceiling : NA
Rate of Climb : NA
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
Fuel Tank Capacity : NA
Baggage Volume : NA
Seats Economy/General Class : 3 seats
Seats Business Class : 0
Seats First Class : 0
Cabin Height : NA
Cabin Width : NA
Cabin Length : NA
Exterior Length : NA
Tail Height : NA
Fuselage Diameter : NA
Wing Span Rotor Diameter : NA
Wing Tips : NA
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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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