Range Map

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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
260
KTAS
Cruise Speed
1,000
nm
Max Range
30,000
ft
Service Ceiling
6
Occupants
559
lbs
Wet Payload
Endorsements & ratings:
  • High-Performance
  • Complex
  • High-Altitude
  • Pressurization
  • Instrument
Piper PA-46-500TP Meridian (N71562) at Bowman Field, Louisville, Kentucky, May 2013. Photo: Aeroprints.com, CC BY-SA 3.0.
Piper PA-46-500TP Meridian (N71562) at Bowman Field, Louisville, Kentucky, May 2013. Photo: Aeroprints.com, CC BY-SA 3.0.

Estimated Ownership Costs

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About the Piper M500

Type certificated 2000

Overview

The Piper M500 is the entry point to PA-46 turboprop ownership and the aircraft that defined the owner-flown single-engine turboprop category. Its origins trace to the PA-46-500TP Meridian, introduced in 2000 as a turboprop conversion of the same PA-46 airframe used by the piston Malibu Mirage. The M500 designation arrived in 2015 alongside the G1000 NXi avionics upgrade that substantially expanded the aircraft’s safety technology baseline.

Powered by a Pratt and Whitney PT6A-42A flat-rated to 500 SHP, the M500 cruises at 260 knots at FL280 and carries six occupants in a pressurised cabin. The PT6 engine is the foundation of the type’s appeal: it is among the most proven turbine powerplants in general aviation, with a deep maintenance network, a 3,600-hour TBO, and an operational simplicity that represents a genuine step change from the high-performance piston aircraft it typically replaces. Mixture management, cowl flaps, and magneto checks are gone, and the power management philosophy is more forgiving than a turbocharged piston at altitude. The mission that fits the M500 is the roughly 1,000 NM regional trip flown behind a turbine: a buyer who wants PT6A simplicity and a pressurised cabin at the lowest entry cost in the M-class, and whose legs rarely exceed what 170 gallons will carry, is matched to this airplane rather than the longer-legged M600 or M700.

Key Features for GA Buyers

  • PT6A Reliability and Simplicity. The PT6A-42A’s reverse-flow design, single-lever power management, and established overhaul network make it one of the more approachable turbine transitions for owner-pilots moving up from complex pistons. The 3,600-hour TBO is meaningful: at 200 hours per year, that is 18 years of flying between overhauls under ideal conditions.

  • Active Safety Systems. The G1000 NXi suite includes Electronic Stability Protection, Automatic Level Mode, and Underspeed Protection. Automatic Level Mode in particular has real operational significance: it can recover the aircraft from an unusual attitude with a single button press, a capability that addresses the leading cause of fatal GA accidents.

  • FL280 Operations. The M500 can cruise at FL280, well above the M350’s FL250 ceiling and comfortably above most convective activity in the continental United States. The pressurisation system maintains a comfortable cabin altitude throughout.

  • Useful Load Advantage over the M350. At 1,698 lb, the M500’s useful load is 390 lb more than the M350’s. With 170 gallons (about 1,190 lb) of fuel, that leaves approximately 508 lb for payload: similar fuel-payload dynamics, but with significantly more range on full tanks.

Trade-offs

  • Fuel Burn. At 35 GPH of Jet-A, the M500 burns roughly 67% more fuel per hour than the M350. The operating cost step from piston to turboprop is real and should be modelled over the anticipated mission profile before committing.
  • Payload with Full Fuel. 170 gallons leaves limited cabin payload. Like all PA-46 variants, the M500 rewards owners who plan fuel loads deliberately rather than departing full tanks on every leg.
  • Runway Requirements. The M500’s takeoff and landing distances are longer than many buyers expect from a single of this size, requiring at least 3,000 ft of runway for comfortable margins. Access to shorter strips is restricted compared to the M600 or M700.
  • Transition Training. The turbine type rating and recurrent training requirements add a fixed cost overhead that piston owners do not carry. Factor this into total annual cost of ownership.

See Also

  • Piper M350 – the pressurised piston predecessor on the same airframe: lower fuel burn, lower acquisition cost, lower ceiling. Compare
  • Piper M600 – the longer-range turboprop tier that followed, since succeeded by the M700: more fuel, more range, and the Garmin G3000 with Autoland. Compare
  • Piper M700 – the performance flagship of the M-class line: 301 knots and the full HALO emergency autoland system. Compare
  • Pilatus PC-12 – the principal cross-manufacturer alternative: larger cabin, greater payload, more utility-oriented mission profile. Compare
  • Daher TBM 850 – the higher-performance single-engine turboprop alternative: faster cruise, higher ceiling, different ownership community. Compare

Technical Specifications

Dimensions & Weights

Wingspan 43 ft
Height
11 ft
Length
30 ft
Parking area (ft²2)
1,834 ft²
Max Takeoff Weight
5,092 lbs
Max Landing Weight
4,850 lbs
Useful Load
1,698 lbs
Fuel Capacity
170 gal

Performance

Cruise Speed
260 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 188 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 188 KIAS
Approach Speed
85 KIAS
Stall, Clean (VS1)
69 KIAS
Range
1000 NM
Service Ceiling
30,000 ft
Rate of Climb
1556 fpm
Takeoff over 50 ft obstacle
2,438 ft
Landing over 50 ft obstacle
2,110 ft

Engine

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