Piper Cheyenne 400

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

Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Pressurization
  • Multi-Engine
  • Instrument
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

Overview

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 Honeywell (Garrett) TPE331-14 engines flat-rated to 1,000 shp each from a 1,650 shp gas-generator capability, driving distinctive four-blade Dowty Rotol composite propellers.

Certified in 1984 and built through 1991, only 43 aircraft were produced, making the 400LS one of the rarest production turboprops in the secondary market. The combination of TPE331 power, transcontinental range, and 41,000 ft service ceiling positioned it as a turboprop alternative to entry-level jets that could still operate from short runways and remote airfields.

Key Features for GA Buyers

  • Jet-Like Speed: Cruise of 351 KTAS (over 400 mph) puts the 400LS among the fastest production turboprops ever built, matching or beating many light jets of its era.
  • Climb Performance: Sea-level initial climb above 3,200 fpm allows direct departure to FL410, getting above weather and traffic in minutes.
  • Range and Payload: Up to 2,240 nm range with a useful load exceeding 4,500 lbs and pressurization to 7.6 psi for a 10,000 ft cabin at FL410.
  • Single-Pilot Capable: Certified for single-pilot operations with autopilot, broadening the operator profile beyond corporate flight departments.

Trade-offs

  • Engine Management: TPE331 engines are highly efficient but operationally distinct from PT6A variants. The direct-drive single-shaft design demands precise temperature management and produces a louder ground signature.
  • Operating Costs: Variable cost runs $1,500 to $2,000 per hour depending on operator and engine reserve assumptions, well above the smaller PT6A-powered Cheyennes.
  • Cockpit: Avionics in un-upgraded airframes feel dated against modern glass cockpits, though Garmin and Avidyne retrofits are available.
  • Rarity: With only 43 built, parts and type-experienced maintenance are harder to source than for the broader Cheyenne family.

See Also

Technical Specifications

Dimensions

Wingspan
47.7 ft
Length
43.4 ft
Height
17.0 ft
Parking area (ft2)
2792.68 ft2

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
Max Structural Cruise (Vno)
351 KIAS
Approach Speed
105 KIAS
Stall, Clean (Vs1)
93 KIAS
Range
2240 NM
Service Ceiling
41,000 ft
Rate of Climb
997 - 3242 fpm
Takeoff over 50 ft obstacle
2,325 ft
Landing ground roll
2,317 ft

Engines

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