Piper M350

Piston • single 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

213
KTAS
Cruise Speed
6
Occupants
1343
nm
Max Range
588
lbs
Wet Payload

Estimated Ownership Costs

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About the Piper M350

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 pressurized single-engine piston aircraft currently in production. That distinction matters. Pressurization at the piston level has historically been a difficult engineering problem, and the PA-46 airframe — now refined across four decades — represents the only current answer to it.

Powered by a turbocharged Lycoming TIO-540-AE2A producing 350 HP, the M350 can cruise at 213 knots at altitudes up to FL250, maintaining an 8,000-ft cabin equivalent throughout. The current production variant features the Garmin G1000 NXi avionics suite with active safety technologies that were unavailable on earlier Mirage models. For a buyer who wants cabin-class comfort, genuine weather avoidance capability, and a piston fuel bill, the M350 is the only aircraft in the world that delivers all three simultaneously.

Key Features for GA Buyers

Pressurization at the Piston Level. The 5.5 psi differential pressurization 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, not marketing features, and they 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 half what the turboprop M500 burns for comparable legs. For owners flying 150–200 hours per year on missions under 800 NM, the fuel cost differential is substantial over an ownership period.

Trade-offs

  • Systems Complexity. Pressurization, turbocharging, FIKI, and retractable gear in combination require disciplined maintenance. Annual inspection costs reflect this: budget $5,000–$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 pressurized 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 next turboprop tier: 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

Wingspan
43.0 ft
Length
28.9 ft
Height
11.3 ft

Weights

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
Range
1343 NM
Service Ceiling
25,000 ft
Rate of Climb
1275 fpm

Engines

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