Piper PA-31 Navajo Civil Aircraft Model Details

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General Information of Piper PA-31 Navajo

First Flight : 30 September 1964[1]

Introduction : 24561

Manufacturer : Piper Aircraft

Number Built : 3942[3]

Produced : 1967–1984[2]

Role : Civil utility aircraft

Status : Active service

Variants : Piper PA-31T Cheyenne

General characteristics of Piper PA-31 Navajo

Capacity : five to seven passengers

Crew : one or two

Empty Weight : 3,930 lb (1,782 kg)

Height : 13 ft 0 in (3.96 m)

Length : 32 ft 7½ in (9.94 m)

Max Takeoff Weight : 6,500 lb (2,948 kg)

Powerplant : 2 × Lycoming TIO-540-A air-cooled six-cylinder horizontally opposed piston engine, 310 hp (231 kW) each

Propellers : Two or three blade, metal, fully feathering, Hartzell propeller

Wing Area : 229 sq. ft (21.3 m²)

Wingspan : 40 ft 8 in (12.40 m)

Performance of Piper PA-31 Navajo

Cruise Speed : 207 knots (383km/h (238mph)) econ cruise at 20,000ft (6,100m)

Maximum Speed : 227 knots (420km/h (260mph)) at 15,000ft (4,600m)

Never Exceed Speed : 236 knots[34] (438km/h (272mph))

Range : 1,011 nmi (1,875km (1,165mi))

Rate Of Climb : 1,445 ft/min (7.3 m/s)

Service Ceiling : 26,300 ft (8,015 m)

Stall Speed : 63.5 knots (118km/h (73mph)) flaps down

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