Piper Cheyenne 400

Turboprop • twin engine • Low Wing • Retractable gear

Range Visualization

Origin: · click map to move · nm at current load

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

351
KTAS
Cruise Speed
9
Occupants
2240
nm
Max Range
751
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper Cheyenne 400

The Piper Cheyenne 400LS (PA-42-1000) is the ultimate development of the Cheyenne family and is widely regarded as the “hot rod” of corporate turboprops. Designed to compete directly with light jets like the Cessna Citation I, it features massive Honeywell (Garrett) TPE331-14 engines flat-rated to 1,000 shp each, driving distinctively large four-blade Dowty Rotol propellers.

Key Features for GA Buyers

  • Jet-Like Speed: With a cruise speed of over 350 knots (400 mph), it is one of the fastest production turboprops ever built, outpacing many light jets of its era while offering better runway performance.
  • Climb Performance: A sea-level initial climb rate of over 3,200 fpm allows it to reach FL410 quickly, getting above weather and traffic.
  • Range & Payload: Capable of transcontinental range (up to ~2,200 nm max) with a useful load exceeding 4,500 lbs.
  • Cabin Comfort: Pressurized to 7.6 psi, maintaining a 10,000 ft cabin altitude at FL410.

Trade-offs

  • Engine Management: The TPE331 engines are highly efficient but require precise management and are known for being louder on the ground compared to PT6A variants.
  • Maintenance Costs: Higher operating costs than smaller Cheyennes due to the high-performance engines and unique composite propellers.
  • Cockpit: While capable, the avionics in un-upgraded models may feel dated compared to modern glass cockpits found in newer turboprops.

Technical Specifications

Dimensions

Wingspan
47.7 ft
Length
43.4 ft
Height
17.0 ft

Weights

Max Takeoff Weight
12,050 lbs
Max Landing Weight
11,100 lbs
Useful Load
4,570 lbs
Fuel Capacity
570 gal

Performance

Cruise Speed
351 KTAS
Range
2240 NM
Service Ceiling
41,000 ft
Rate of Climb
3242 fpm

Engines

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