Piper Cheyenne II

Turboprop • twin engine • Low Wing • Retractable gear

Range Visualization

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Payload vs. Range

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Default: 190 lbs (FAA standard)

Default: 30 lbs

Passengers
lbs @ lbs / pax
0 lbs
Fuel on board
gal
+ Weight
Range
Available Range / nm
Mission capable — Aircraft can handle the current load with full fuel tanks.
Fuel tradeoff required — You'll need to leave gallons of fuel behind ( gal usable for nm range).
Over max gross weight — Reduce payload by lbs to safely operate this aircraft.

Mission Profile

283
KTAS
Cruise Speed
7
Occupants
1350
nm
Max Range
1041
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper Cheyenne II

The Piper PA-31T Cheyenne II is the original high-performance model that launched Piper’s turboprop success. Powered by 620 shp Pratt & Whitney PT6A-28 engines, it offers significantly more power than the Cheyenne I/IA. It is a “hot rod” in its class, known for impressive climb rates and speed, but it demands respect due to its stability characteristics.

Key Features for GA Buyers

  • Power to Weight: With 620 shp per side and a 9,000 lb MTOW, the Cheyenne II boasts an exceptional power-to-weight ratio. This translates to a sea-level climb rate of 2,800+ fpm, allowing it to rocket up to the flight levels faster than most King Airs of the era.
  • Range & Fuel: Standard tip tanks bring the total fuel capacity to 382 gallons, offering a range of over 1,300 nm at economy cruise, making it a true cross-continent traveler.
  • Value: Because of the market stigma surrounding its stability history (see below), the Cheyenne II typically commands a lower purchase price than the Cheyenne I or IIXL, offering arguably the best “knots per dollar” value in the twin turboprop market.

Trade-offs

  • Stability Augmentation System (SAS): The high power combined with the short fuselage created longitudinal stability issues at high angles of attack. As a result, the Cheyenne II is certified with a mandatory Stability Augmentation System (SAS). If this system fails, the aircraft may be grounded or restricted to a lower flight envelope.
  • Handling: It is less docile than the Cheyenne I or the stretched Cheyenne IIXL. The short-coupled fuselage can make pitch control sensitive, particularly during takeoff and landing phases.
  • Cabin Noise: The high-power engines mounted close to the fuselage create a louder cabin environment compared to the stretched IIXL or the King Air series.

Technical Specifications

Dimensions

Wingspan
42.67 ft
Length
34.67 ft
Height
12.75 ft

Weights

Max Takeoff Weight
9,000 lbs
Max Landing Weight
9,000 lbs
Useful Load
3,600 lbs
Fuel Capacity
382 gal

Performance

Cruise Speed
283 KTAS
Range
1350 NM
Service Ceiling
31,000 ft
Rate of Climb
2800 fpm

Engines

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