Twin Engine • Piper • PA-31T (Standard), PA-31T-500 (Turbocharged), PA-31T-620 (Enhanced), Cheyenne II, Cheyenne IIIA
| Manufacturer | Piper |
| Model | PA-31T Cheyenne |
| Category | Twin Engine |
| Variants | PA-31T (Standard), PA-31T-500 (Turbocharged), PA-31T-620 (Enhanced), Cheyenne II, Cheyenne IIIA |
| Production Years | 1974 – 1985 |
| Seating | 6, 7, 8 seats |
| Typical TTAF | 4,200 hours |
| Markets | United States, Canada, Australia, South Africa, Brazil |
| Price Range | $180K – $650K |
The Piper PA-31T Cheyenne is a pressurized, twin-engine executive transport aircraft designed for business travel and charter operations. First introduced in the 1970s, the Cheyenne combines the reliability of proven Lycoming engines with sophisticated avionics and cabin pressurization, allowing operations at high altitudes with passenger comfort. The aircraft is distinguished by its swept-wing design, retractable landing gear, and ability to carry 6-8 passengers with useful loads suitable for transoceanic missions. The Cheyenne earned respect in corporate aviation circles and remains a capable platform for charter operators, particularly in regions where unprepared airfields are common. Its robust construction and twin-engine redundancy made it popular with humanitarian operators and remote-area services. The aircraft represents mid-range business aviation of its era, positioning itself between light twins and larger turboprop transports. Today, well-maintained examples serve in niche markets including special missions, cargo operations, and private ownership among experienced pilot-owners seeking economical twin-engine performance.
Maximum Speed: 260 knots
Cruise Speed: 235 knots
Range: 1,500 nautical miles
Service Ceiling: 25,000 feet
Engines: Twin Lycoming TIO-540-J2B or TIO-541 turbocharged pistons
Maximum Takeoff Weight: 7,000 lbs
Empty Weight: 4,400 lbs
Fuel Capacity: 162 gallons
Pressurization: 6,000 feet cabin altitude at 25,000 feet