Range Map
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Payload vs. Range
Fuel on board
Cargo
nm
Range
Trip Preview
Name a destination in the map header above and this becomes your trip: time en route, what you burn, what it costs, and whether you get there without stopping — at the load you have set.
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We do not have a cruise speed on file for this aircraft, so there is no honest time or cost to give you for this leg.
En route
Fuel burned
Direct cost
Fuel cost
Tanks run dry about past before at this burn.
Mission Profile
- High-Performance
- Complex
- High-Altitude
- Pressurization
- Multi-Engine
- Instrument
Estimated Ownership Costs
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About the Piper Cheyenne 400
Type certificated 1984
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. The honest case against the 400LS is scarcity: only 43 were built, so type-experienced maintenance and TPE331 parts are harder to find than for any PT6A-powered Cheyenne, and operating cost runs $1,500 to $2,000 an hour. For the owner who can place a shop fluent in the single-shaft Garrett engine and wants near-jet speed without a jet’s acquisition and fuel bill, that scarcity is a price worth paying.
Key Features for GA Buyers
- Jet-Like Speed: Cruise of 351 KTAS (over 400 mph) gives the 400LS speed in the realm of the light jets it was built to challenge.
- 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 roughly 2,180 nm range with a useful load exceeding 4,500 lbs and pressurisation 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
- Piper PA-42 Cheyenne III – the 720 shp PT6A-41 sibling at the next tier down. Compare
- Beechcraft King Air 350 – top-of-line PT6 turboprop with larger cabin and broader parts support. Compare
- Cessna Conquest II – the direct period rival, also TPE331-powered, slightly smaller and slower. Compare
- Mitsubishi Marquise/Solitaire – the other “fast turboprop” of the era, with comparable speed but tighter cabin. Compare
- Cessna Citation II/SP – the single-pilot light jet alternative the 400LS was built to challenge. Compare
Technical Specifications
Dimensions & Weights
- Height
- 17 ft
- Length
- 43 ft
- Parking area (ft²2)
- 2,793 ft²
- 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
- Never-Exceed (VNE)
- Source: FAA Type Certificate Data Sheet 244 KIAS
- Max Structural Cruise (VNO)
- Source: FAA Type Certificate Data Sheet 244 KIAS
- Approach Speed
- 105 KIAS
- Stall, Clean (VS1)
- Source: third-party reference 93 KIAS
- Range
- 2176 NM
- Service Ceiling
- 41,000 ft
- Rate of Climb
- 997 - 3242 fpm
- Takeoff over 50 ft obstacle
- 2,325 ft
- Landing over 50 ft obstacle
- 2,317 ft
Engines
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Sources
Where the figures on this page come from. Piper Cheyenne 400 specifications are traced to published references; estimated values are flagged inline next to the figure.
Similar to the Piper Cheyenne 400
Similar TurbopropsPiaggio Avanti EVO
Piaggio P-180 Avanti
Beechcraft King Air 250
Cessna 441 Conquest II
Piper PA-42 Cheyenne III
Fairchild Swearingen Merlin IIIB
Compare the Piper Cheyenne 400 to other aircraft