Range Map

Origin: · two fingers to move map

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1

Tank-dry, where fuel runs out at catalogue's stored cruise burn.

Excludes reserves: range beyond the dashed circle requires a leaner cruise than what we store. Great-circle, still air, book cruise. Estimates only: always verify against the POH.

Payload vs. Range

Occupants:

Fuel on board

Cargo

nm

Range

Cargo is additional payload after occupants and baggage.
full tanks
Available Range / nm
Mission capable. This load flies with full fuel.
Fuel reduced by . left aboard for nm range.
Over max payload by . At this load it cannot lift a single occupant.

Trip Preview

Mission Profile

In production Aircraft available new or used
213
KTAS
Cruise Speed
1,338
nm
Max Range
25,000
ft
Service Ceiling
6
Occupants
588
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • Pressurization
Piper PA-46-350P M350 (N151TM) at Daytona Beach International Airport, March 2023. Photo: ZLEA, CC BY-SA 4.0.
Piper PA-46-350P M350 (N151TM) at Daytona Beach International Airport, March 2023. Photo: ZLEA, CC BY-SA 4.0.

Estimated Ownership Costs

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About the Piper M350

Type certificated 1988

Overview

The Piper M350 is the direct descendant of the PA-46 Malibu Mirage and occupies a unique position in general aviation: it is the only pressurised single-engine piston aircraft currently in production. That distinction matters. Pressurisation at the piston level has historically been a difficult engineering problem, and the PA-46 airframe, refined across four decades, remains the only current answer to it.

Powered by a turbocharged Lycoming TIO-540-AE2A producing 350 HP, the M350 cruises at 213 knots at altitudes up to FL250 while holding an 8,000-ft cabin equivalent throughout, and the current production variant pairs the Garmin G1000 NXi suite with active safety systems unavailable on earlier Mirage models. It sits at the entry of Piper’s M-class line, below the turboprop M500, for the buyer who wants cabin-class comfort and genuine weather capability on a piston fuel bill. That positioning points the M350 at the buyer flying two adults and bags on trips under 800 NM who wants those qualities without a turbine’s fuel bill. Anyone who needs turbine speed, flight-level climb, or PT6A dispatch simplicity should start one rung up, at the M500.

Key Features for GA Buyers

  • Pressurisation at the Piston Level. The 5.5 psi differential pressurisation system maintains an 8,000-ft cabin at FL250. This is the M350’s defining characteristic: the ability to operate above most convective weather and turbulence without supplemental oxygen, in an aircraft with piston operating economics.

  • Advanced Safety Suite. The G1000 NXi integration includes Pulse Oximetry monitoring, Hypoxia Recognition with Automatic Descent Mode, and Electronic Stability Protection. These are substantive pilot-incapacitation mitigations that meaningfully change the risk profile of single-pilot IFR operations.

  • Cabin-Class Utility. The PA-46 cabin offers airstair door entry, club seating for four passengers, and stand-up headroom adequate for most occupants. For a single-engine piston, the interior environment is genuinely competitive with light twins.

  • Piston Operating Economics. At 21 GPH, the M350 burns roughly 40% less fuel per hour than the turboprop M500. For owners flying 150 to 200 hours per year on missions under 800 NM, the fuel cost differential is substantial over an ownership period.

Trade-offs

  • Systems Complexity. Pressurisation, turbocharging, FIKI, and retractable gear in combination require disciplined maintenance. Annual inspection costs reflect this: budget $5,000 to $8,000 as a base, with unscheduled items on top.
  • Useful Load vs. Full Fuel. 120 gallons (720 lb) of fuel against a 1,308-lb useful load leaves 588 lb for passengers and bags. Two adults with luggage and full fuel is comfortable; four adults with bags and full fuel is not. Mission planning around fuel load is a routine part of M350 ownership.
  • Piston Ceiling Limitations. While the M350 can reach FL250, climb performance degrades meaningfully above FL180 compared to the turboprop M500. Pilots regularly operating in the flight levels will notice the difference.
  • Single-Engine Risk Profile. Despite the safety systems, a pressurised single-engine piston operating at altitude carries an irreducible risk profile that some buyers, insurers, and passengers will not accept.

See Also

  • Piper M500 – the turboprop step-up on the same PA-46 airframe: more speed, higher ceiling, and a fundamentally different engine risk profile. Compare
  • Piper M600 – the turboprop tier with more fuel, more range, and the Garmin G3000 with Autoland. Compare
  • Piper M700 – the top of the M-class line: 301-knot cruise and the full HALO safety suite. Compare
  • Pilatus PC-12 – the cross-manufacturer single-engine turboprop benchmark: larger cabin, more utility, significantly higher acquisition cost. Compare

Technical Specifications

Dimensions & Weights

Wingspan 43 ft
Height
11 ft
Length
29 ft
Parking area (ft²2)
1,797 ft²
Max Takeoff Weight
4,340 lbs
Max Landing Weight
4,123 lbs
Useful Load
1,308 lbs
Fuel Capacity
120 gal

Performance

Cruise Speed
213 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 198 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 168 KIAS
Approach Speed
75 KIAS
Stall, Clean (VS1)
69 KIAS
Range
1338 NM
Service Ceiling
25,000 ft
Rate of Climb
1275 fpm
Takeoff over 50 ft obstacle
2,090 ft
Landing over 50 ft obstacle
1,968 ft

Engine

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Sources

Where the figures on this page come from. Piper M350 specifications are traced to published references; estimated values are flagged inline next to the figure.

Similar to the Piper M350

Similar Pistons

Riley Super P210

Cruise
200 kts (lower than this aircraft)
Range
925 nm (lower than this aircraft)
Seats
6
Compare

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