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PA-31 Navajo

American light, twin-engined aircraft, used extensively for air taxi, flight training, and personal use during the late 20th century.

Origin country
🇺🇸 United States
First flight
1964Sep 30
Introduced
1967
Produced
3,942units
Active worldwide
8
Piper PA-31 Navajo military transport aircraft side profile drawing
Side profile · Piper PA-31 Navajo · length 9.9 m
Technical SpecificationsVersion: PA-31
Length9.9 m (32.6 ft)
Wingspan12.4 m (40.8 ft)
Height4.0 m (13.0 ft)
Wing area21 m² (226.0 sqft)
Empty weight1,783 kg (3,931 lbs)
Max. takeoff weight2,948 kg (6,499 lbs)
Powerplant2 × pistons engine Lycoming TIO-540-A 231 kW each
PerformanceVersion: PA-31
Maximum speed420 km/h (261 mph)
Operational range1,875 km (1,165 mi)
Service ceiling8,016 m (26,299 ft)
Climb rate7.3 m/s (24.0 ft/s)
Operators — 2026
ActiveOn order
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🇦🇬 Antigua and Barbuda· 🇧🇸 Bahamas· 🇨🇴 Colombia· 🇩🇴 Dominican Republic· 🇫🇮 Finland· 🇫🇷 France· 🇬🇹 Guatemala· 🇭🇳 Honduras· 🇭🇷 Croatia· 🇰🇪 Kenya· 🇲🇽 Mexico· 🇲🇷 Mauritania· 🇳🇬 Nigeria· 🇵🇦 Panama· 🇵🇪 Peru· 🇸🇪 Sweden· 🇹🇹 Trinidad and Tobago· 🇺🇸 United States

Description

At the behest of William T. Piper, Piper Aircraft began developing a six- to eight-seat twin-engined corporate and commuter transport aircraft in 1962, under the project name Inca. The PA-31 conducted its first flight on September 30, 1964, and was announced later that year. It was initially powered by two 310 hp (231 kW) Lycoming TIO-540-A turbocharged engines. As testing progressed, cabin windows were added to each side of the fuselage, and the engines were repositioned forward. The PA-31, named "Navajo", received FAA certification on February 24, 1966, with a maximum takeoff weight (MTOW) of 6,500 lb (2,948 kg). Deliveries commenced in 1967. The PA-31 series was also manufactured under license in Argentina, Colombia, and Brazil, from kits supplied by Piper. Production ran from 1967 to 1984.

Design

The PA-31 Navajo is a low-wing monoplane with a conventional tail configuration. It was constructed for utility, small cargo, feeder airlines, and corporate transport. The initial design was influenced by the PA-30 Twin Comanche, featuring a similar engine cowling. Early models were equipped with two 310 hp Lycoming TIO-540-A turbocharged engines. Variants such as the PA-31P Pressurized Navajo featured 425 hp Lycoming TIGO-541-E engines and a pressurized cabin. The PA-31-350 Navajo Chieftain introduced a stretched fuselage for increased seating, along with counter-rotating propellers. The 1971 Navajo B variant included air conditioning, increased baggage space, and optional pilot access doors.

The Piper PA-31 Navajo is a civil utility aircraft. Its payload capacity is for passenger and cargo transport. The original PA-31 Navajo has a maximum takeoff weight of 6,500 lb (2,948 kg). Variants like the PA-31-350T1020 were configured for commuter airline use, allowing for increased seating capacity. The PA-31T3 variant could be fitted with an optional underbelly cargo pod.

Operational History

The Navajo family has seen widespread operational use since its introduction among air charter companies, feeder airlines, and commuter air carriers. Air West, a predecessor to Hughes Airwest, operated the PA-31 in scheduled passenger airline service in the U.S. starting in 1968. West Coast Airlines initiated passenger service in 1967, designating the aircraft the "MiniLiner". Military forces have also employed the Navajo in various roles, including the Chilean Navy, Colombian Air Force and Navy, Dominican Republic Air Force, Finnish Air Force, French Navy, Honduran Air Force, Kenya Air Force, Spanish Air Force, and the Aeroplane and Armament Experimental Establishment in the United Kingdom. The Finnish Air Force utilized the PA-31-350 Chieftain for liaison and light transport, while the Kenya Air Force operated a Navajo Chieftain for VIP transport.

Variants

Main Variants:

  • PA-31 Navajo: The initial production version, unofficially known as the PA-31-310.

  • PA-31-300 Navajo: This variant used normally aspirated engines, with 14 units built.

  • PA-31 Navajo B: Introduced in 1971, this variant featured 310 hp (231 kW) Lycoming TIO-540-E turbo-charged piston engines, along with air conditioning and an optional pilot access door.

  • PA-31P Pressurized Navajo: Piper's first pressurized aircraft, this version was powered by two 425-hp (317-kW) Lycoming TIGO-541-E1A piston engines.

  • PA-31-350 Chieftain: This stretched version featured 350-hp (261-kW) counter-rotating engines and increased seating capacity.

Frequently Asked Questions

What type of aircraft is the PA-31 Navajo?
The Piper PA-31 Navajo is a military transport aircraft aircraft developed by Piper and entered service in 1967.
What is the maximum speed of the PA-31 Navajo?
The Piper PA-31 Navajo has a maximum speed of 420 km/h (260 mph).
What is the range of the PA-31 Navajo?
The Piper PA-31 Navajo has an operational range of 1,875 km (1,165 miles). This range can vary based on payload, altitude, and mission profile.
When did the PA-31 Navajo first fly?
The Piper PA-31 Navajo made its first flight on September 30, 1964. It entered operational service in 1967.
How many PA-31 Navajo have been built?
Approximately 3,942 units of the Piper PA-31 Navajo have been produced since it entered service in 1967.
Which countries operate the PA-31 Navajo?
The Piper PA-31 Navajo is operated by 7 countries with approximately 8 aircraft in active service. The largest operators include Colombia, Antigua and Barbuda, and Dominican Republic.
What is the service ceiling of the PA-31 Navajo?
The Piper PA-31 Navajo has a service ceiling of 8,016 meters (26,299 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
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