HangarMart
Piston SinglesP2010 SeriesIntroduced 2013

Tecnam

P2010

The Tecnam P2010 is a four-seat, high-wing, fixed-gear composite single-engine aircraft powered by a Lycoming IO-360-M1A producing 180 hp, designed as a modern and cost-effective personal and training aircraft. It features a wide cabin, a Garmin G1000 NXi glass cockpit, and a high-wing configuration offering excellent visibility and stability. The P2010 TDI variant uses the Austro Engine AE300 diesel engine for operators seeking Jet-A fuel compatibility.

  • High-wing design with outstanding cabin visibility
  • Wide composite cabin seating four adults
  • Garmin G1000 NXi avionics suite
  • TDI diesel variant available for Jet-A operations
  • Modern Italian design with efficient aerodynamics
  • Fixed gear for low maintenance
Tecnam P2010

P2010 key specifications

Range
890 nm
Cruise speed
138 kts
Passengers
up to 4
Max take-off weight
2,756 lb
Engines
1 × Piston
Overview

About the P2010

The Tecnam P2010 — part of the P2010 Series family — is a single-engine piston aircraft aimed at affordable personal flying and owner-operation. It entered service in 2013 and is now a current-generation design, developed in Italy.

On performance, it offers a maximum range of about 890 nautical miles and a cruise of roughly 138 knots. It seats up to 4 passengers and is powered by 1 Lycoming IO-360-M1A engine.

Its 890 nm range makes it well matched to short-haul hops and local operations. It is certified for single-pilot operation and is approved for IFR flight. For buyers weighing the P2010, compare its specifications and operating profile against the closest alternatives below before requesting a quote.

Gallery

At a glance

Performance

Max Range
890 nm
Cruise Speed
138 kt
Max Seats
4
MTOW
2,756 lbs

Full specifications

Operator and certification details for the P2010, plus the complete performance, dimensions, weights and powerplant sheet — free with an account.

Country of Origin
Italy
Engines
1 × Piston
Engine Model
Lycoming IO-360-M1A
IFR Certified
Yes
Single-Pilot
Yes

20 more specifications — performance, dimensions, weights and powerplant — are free with an account.

View plans

Value & depreciation

How a piston single like the P2010 typically holds value — indicative, class-typical retention of a new example against age. Run your own year and hours in the valuation calculator for a specific estimate.

At 5 years
~82%
of typical new value retained
At 10 years
~66%
of typical new value retained
At 15 years
~54%
of typical new value retained

Indicative only — actual value depends on hours, maintenance-program status, avionics, condition and the current market.

Pricing & seller quotes

Aggregated market pricing and multi-seller quotes — shared with verified partners.

Pricing is shared with verified partners

We aggregate live market pricing and seller quotes for the P2010. Request a quote and our team will send tailored pricing and availability — or sign in if you’re an approved partner.

Prefer a quick public estimate? Estimate the P2010 cost of ownership with our free calculator.

Ownership & ROI calculator

Model the true economics of owning or chartering the P2010. Pre-filled with realistic defaults for this type — adjust any assumption and the results update instantly.

Model the economics of the P2010

Create a free account to see the true cost per flight hour and annual ownership cost. Upgrade for the full five-year ROI projection, charter profitability and a client-ready report.

True cost per flight hour
Fully-burdened ownership cost from fuel to financing — free.
Five-year ROI projection
Revenue, EBITDA, equity, ROI, NPV & IRR modelled out five years.
Charter profitability
Private, hybrid and full-charter scenarios side by side.
Compare aircraft
Acquisition, cost/hour and ROI across multiple types.

How the P2010 compares

Side by side with the most similar piston singles.

Performance
Range
890 nm
915 nm
1,000 nm
900 nm
Cruise speed
138 kt
145 kt
155 kt
170 kt
Max speed
Locked — sign in to view
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Service ceiling
Locked — sign in to view
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Rate of climb
Locked — sign in to view
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Capacity & dimensions
Max seats
4
4
4
6
Crew
Locked — sign in to view
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Max takeoff weight
2,756 lbs
3,100 lbs
3,150 lbs
3,800 lbs
Length
Locked — sign in to view
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Cabin height
Locked — sign in to view
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Powerplant
Engines
1 × Piston
1 × Piston
1 × Piston
1 × Piston
Engine model
Lycoming IO-360-M1A
Lycoming IO-540-AB1A5
Continental IO-360-ES
Continental IO-520 / TSIO-520

6 more specs per aircraft — ceiling, climb, cabin, dimensions and more — are free with an account.

Beyond the spec sheet

Buying or operating the P2010? Get an independent acquisition recommendation, or see how fleet management keeps operations, maintenance, crew and compliance in one place.

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