Piper PA-31T Cheyenne Civil Aircraft Model Details

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General Information of Piper PA-31T Cheyenne

Developed From : Piper PA-31 Navajo

First Flight : 25444

Manufacturer : Piper Aircraft

Number Built : 823

Primary Users : Corporate

Produced : 1974-1985

Role : Turboprop

Variants : Piper PA-42 Cheyenne

General characteristics of Piper PA-31T Cheyenne

Capacity : 4–6 passengers

Crew : 2

Empty Weight : 4,870 lb (2,209 kg)

Height : 12 ft 9 in (3.89 m)

Length : 34 ft 8 in (10.57 m)

Max Takeoff Weight : 9,000 lb (4,082 kg)

Powerplant : 2 × Pratt & Whitney PT-6-28 turboprop, 620 shp (462 kW) each

Wing Area : 229 sq ft (21.3 m²)

Wingspan : 42 ft 8¼ in (13.01 m)

Performance of Piper PA-31T Cheyenne

Cruise Speed : 244 mph (393 km/h, 212 knots) at 25,000 ft (7,600 m)

Maximum Speed : 326 mph (525 km/h, 283 knots) at 11,000 ft (3,360 m)

Range : 1,702 mi (2,739 km, 1,478 nmi) (econ cruise, 45 min reserves)

Rate Of Climb : 2,800 ft/min (14.2 m/s)

Service Ceiling : 29,000 ft (8,840 m)

Stall Speed : 88 mph (142 km/h, 77 knots) (flaps down)

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