Piper PA-31 Navajo

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Piper PA-31 Navajo
Piper PA-31 Navajo (C-GXCY)
Type Piston
Manufacturer Piper Aircraft
Designed by Project Engineer, Paul E. Everly
Maiden flight September 30, 1964
Primary user Corporate
Number built 2044
Piper PA-31 Navajo (C-GXCY)
Piper PA-31 Navajo (C-GXCY)

The PA-31 Navajo is a family of cabin-class, twin-engine aircraft designed and built by Piper Aircraft using Lycoming engines for the general aviation market.

In the mid-1960s, an aircraft of this size was sorely needed and founder William T. Piper requested the type be developed. Targeted at small-scale cargo and feeder liner operations and the corporate market, the aircraft was a success. It continues to prove a popular choice, but due to greatly decreased demand across the general aviation sector in the 1980s, production of the PA-31 ceased.

Contents

The PA-31 series was produced in a variety of versions.

  • PA-31-310 Navajo, sometimes referred to as a "straight Navajo". Also called the "Mini - Liner"
  • PA-31-325 Navajo, referred to as the "CR" or Counter Rotating.
  • PA-31-350 Navajo Chieftain (originally called the "Navajo II") featured a stretched cabin and more powerful engines (Lycoming TIO-540-J2BD)
  • T-1020 was a Chieftain modified to be marketed to the commuter airline market.
  • PA-31P Pressurized Navajo (commonly referred to as "P-Navajo") was equipped with a pressurized cabin
  • Piper Mojave was an upgraded, reengined version of the PA-31P
  • PA-31T Cheyenne, pressurized, turboprop
  • T-1040, PA-31T3, was an airline version of the PA-31T Cheyenne.

General characteristics

  • Crew: 1, possibly 2 depending on regulations operated under
  • Capacity: 6 passengers
  • Length: 32 ft 7.5 in (9.95 m)
  • Wingspan: 40 ft 8 in (12.40 m)
  • Height: 13 ft 0 in (3.96 m)
  • Wing area: 229 sq. ft (21.. m²)
  • Empty weight: 3759 lb (1709 kg)
  • Useful load: 2741 lb (1246 kg)
  • Max takeoff weight: 6,500 lb (2,900 kg)
  • Maximum ramp weight: 6,880 lb (3,130 kg) with BLRI VG System
  • Maximum (STC) takeoff weight: 6,840 lb (3,110 kg) with BLIRI VG System
  • Powerplant:Lycoming TIO-540-A2B or -A2C , 310 hp (230 kW) each
  • Propellers: constant speed, controllable pitch, fully feathering, Hartzell propeller

Performance

General characteristics

  • Crew: 1, possibly 2 depending on regulations operated under
  • Capacity: 8 passengers
  • Length: ft in (m)
  • Wingspan: 40 ft 8 in (12.40 m)
  • Height: 13 ft (3.96 m)
  • Wing area: 229 ft² (21.28 m²)
  • Empty weight: 4,003 lb (1,817 kg)
  • Useful load: 2,533 lb (1,150 kg)
  • Max takeoff weight: 7,000 lb (3,175 kg)
  • Maximum Ramp Weight: 7,045 lb (3,195kg)
  • Powerplant: 2× Lycoming TIO-540-J2BD , 350 hp (260 kW) each
  • Propellers: with a constant speed, controllable pitch, fully feathering, Hartzell propeller

Performance


Related development

Comparable aircraft

Designation sequence

See also

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