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
Mission Profile
- High-Performance
- Complex
- High-Altitude
- Pressurization
- Multi-Engine
- Instrument
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
- Piper PA-42-720 Cheyenne III – the 720 shp PT6A-41 sibling at the next tier down. Compare
- Beech Super 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
- 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
Similar to the Piper Cheyenne 400
Raytheon 300 Super King Air
King Air 250
Cessna Conquest II
See how the Piper Cheyenne 400 stacks up against similar aircraft