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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Over max payload by . At this load it cannot lift a single occupant. Please adjust your payload inputs.
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
- Pressurization
- Multi-Engine
Estimated Ownership Costs
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About the Piper Aero Star
Type certificated 1984 Source: third-party reference
Overview
The Piper Aerostar 700P is the fastest and most powerful version of the Aerostar, a pressurised piston twin designed by Ted Smith and built from the late 1960s before Piper acquired the line in 1978. The 700P, introduced in 1984, pairs the Aerostar’s distinctive mid-wing, high-wing-loading airframe with two 350-horsepower counter-rotating, turbocharged Lycoming TIO-540 engines. It is often cited as the fastest production piston twin, cruising around 261 knots true at altitude.
The Aerostar is a speed-first airplane: a pressurised, high-altitude cross-country machine for owners who value pace over cabin volume or low operating cost. Its mid-wing layout and slippery design deliver the speed, but the type demands proficiency and rewards disciplined fuel and engine management, and its maintenance and parts costs run high. The honest case against the Aerostar is plain: about 40 gallons an hour at high cruise, a cabin tighter than other cabin-class twins, demanding high-wing-loading handling, and parts and maintenance bills that run above simpler twins. None of that deters the owner who buys the Aerostar for what it does best: cover ground fast, pressurised, at altitude. The proficient, disciplined pilot who prizes pace over economy and cabin room is exactly who it rewards.
Key Features for GA Buyers
- Speed-first piston twin. Around 261 knots true at altitude on twin 350-horsepower turbocharged engines, the type’s defining trait.
- Pressurised cabin. Cabin pressurisation supports high-altitude cruise above weather.
- Counter-rotating turbocharged TIO-540s. 350 hp per side with counter-rotation removing the critical engine.
- Mid-wing aerodynamic design. Ted Smith’s high-wing-loading layout delivers the speed and reduces gust response at cruise.
- Six seats. Seating for six in a pressurised cabin.
Trade-offs
- High operating and maintenance cost. Turbocharged TIO-540s and pressurisation carry high parts and maintenance costs over simpler twins, and the type has demanding parts availability.
- Demanding to fly. High wing loading and a history of accidents from engine failures on takeoff and fuel mismanagement make proficiency and discipline essential.
- Tight cabin for its class. Cabin volume is modest relative to cabin-class twins, trading room for speed.
- Fuel system complexity. Electrically operated remote fuel valves and a particular fuel-management routine require careful attention.
- High fuel burn. Around 40 GPH combined at high-speed cruise.
See Also
- Piper PA-23-250 Aztec – Piper’s slower, simpler naturally aspirated six-place twin. Compare
- Piper PA-34 Seneca – Piper’s turbocharged six-place trainer and touring twin. Compare
- Piper Navajo – Piper’s larger cabin-class piston twin. Compare
- Cessna 340 – a pressurised cabin-class piston twin. Compare
Technical Specifications
Dimensions & Weights
- Height
- 13 ft
- Length
- 35 ft
- Parking area (ft²2)
- 1,859 ft²
- Max Takeoff Weight
- 6,315 lbs
- Max Landing Weight
- 6,000 lbs
- Useful Load
- 1,744 lbs
- Fuel Capacity
- 166 gal
Performance
- Cruise Speed
- Source: third-party reference 261 KTAS
- Never-Exceed (VNE)
- Source: manufacturer figure 241 KIAS
- Max Structural Cruise (VNO)
- Source: manufacturer figure 215 KIAS
- Approach Speed
- 96 KIAS
- Stall, Clean (VS1)
- 74 KIAS
- Range
- 1200 NM
- Service Ceiling
- 25,000 ft
- Rate of Climb
- 320 - 1840 fpm
- Takeoff over 50 ft obstacle
- 3,080 ft
- Landing over 50 ft obstacle
- 2,100 ft
Engines
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Sources
Where the figures on this page come from. Piper Aero Star specifications are traced to published references; estimated values are flagged inline next to the figure.
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AeroResources Aerostar 601P pilot report (FAA AFM airspeed limits) aeroresourcesinc.com
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Wikipedia - Piper Aerostar (operational history) en.wikipedia.org
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PlanePhD (Aerostar PA-60-700P, wizard 7), distance block planephd.com
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PlanePhD (Aerostar PA-601P, wizard 13) -- sibling differentiation check planephd.com
Similar to the Piper Aero Star
Similar PistonsCessna 340
Piper PA-34 Seneca
Cessna P337 Pressurized Skymaster
Cessna 310
Piper PA-31P Pressurized Navajo
Cessna 320 Skyknight
Compare the Piper Aero Star to other aircraft
External Media
Articles and other links
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Aviation Consumer: Aerostar 600 / 700 Series Used Aircraft Guide www.aviationconsumer.com
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Flying Magazine: Used Aircraft Guide -- Piper Aerostar Offers Turbine-Like Performance www.flyingmag.com
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Plane & Pilot: Piper Aerostar 600 / 601 / 700P planeandpilotmag.com
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Wikipedia: Piper Aerostar en.wikipedia.org