PA-31-325

The Piper PA-31-325 Navajo C/R is a twin-engine aircraft with two Lycoming TIO-540-A2C engines producing 325 hp each. Key specifications include a maximum takeoff weight of 6,500 lbs, a typical capacity of 1-2 crew and 5-7 passengers, a maximum speed of 226 kts, and a service ceiling of up to 26,300 ft. Its wingspan is 40 ft 8 in, and it has a length of 32 ft 7.5 in.

General characteristics

• Crew: 1 or 2
• Capacity: 5-7 passengers
• Length: 32 ft 7.5 in (9.94 m)
• Wingspan: 40 ft 8 in (12.40 m)
• Height: 13 ft 0 in (3.96 m)
• Maximum takeoff weight: 6,500 lb (2,948 kg)
• Empty weight: 3,930 lb (1,783 kg)
• Fuel capacity: 183 US gal (710 L)

Performance

• Maximum speed: 226 kts
• Normal cruise speed: 207 kts
• Rate of climb: 1,445 fpm
• Maximum range: 1,011 nm
• Service ceiling: 26,300 ft
• Balanced field length: 1,750 ft

Powerplant

• Engines: 2 x Lycoming TIO-540-A2C
• Horsepower: 325 hp each
• Propellers: 3-bladed, fully feathering