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.

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Mission Profile

In production Aircraft available new or used
134
KTAS
Cruise Speed
715
nm
Max Range
12,000
ft
Service Ceiling
4
Occupants
527
lbs
Wet Payload
Tecnam P2010 (G-GAEE) in flight near Kempen Airport. Photo: Poppo154, CC BY-SA 4.0.
Tecnam P2010 (G-GAEE) in flight near Kempen Airport. Photo: Poppo154, CC BY-SA 4.0.

Estimated Ownership Costs

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About the Tecnam P2010

Type certificated 2014

Overview

The Tecnam P2010 is a modern four-seat high-wing single that pairs a carbon-fiber fuselage with metal wings, powered by the 180-horsepower Lycoming IO-360-M1A burning avgas through a fixed-pitch propeller. Type-certificated in 2014 (EASA.A.576; FAA A00066CE, 2015), it offers three-door cabin access, a Garmin G1000 NXi suite, and an IFR-capable cross-country platform aimed at personal owners and flight schools alike.

A current-production, glass-panel four-seater on simple avgas, it undercuts the diesel and 215-hp variants on purchase price. It cross-shops directly against the Cessna 172 Skyhawk and Piper Archer, trading their aluminum legacy for a composite fuselage and a more modern cabin. Step up to the Tecnam P2010 TDI for Jet-A economy and an 18,000-foot ceiling, or to the 215-hp MkII (Lycoming IO-390) for more climb and useful load.

Key Features for GA Buyers

  • Modern composite-and-metal airframe. A carbon-fiber fuselage with metal wings gives a roomy, corrosion-resistant cabin newer than the legacy aluminum trainers it competes with.
  • Three-door access. Two forward doors plus a rear door ease cabin loading for passengers and baggage.
  • Garmin glass, IFR-capable. Typically delivered with a Garmin G1000 NXi suite, making it a credible IFR trainer and personal cross-country aircraft.
  • Simple avgas operation. The fixed-pitch Lycoming IO-360 keeps operation and maintenance familiar and inexpensive relative to the FADEC diesel.

Trade-offs

  • Modest cruise on 180 hp. A fixed-pitch 180-hp P2010 cruises around 134 KTAS, competitive with a Skyhawk but slower than the 215-hp MkII or a retractable.
  • Borderline MOSAIC. The clean stall sits at 59 KCAS, right at the sport-pilot gate; a KCAS verification can flip the verdict, so sport-pilot eligibility is not confirmed.
  • 12,000-foot ceiling. Normally aspirated, it lacks the turbocharged TDI’s high-altitude reach.
  • Premium over legacy trainers. A current-production composite single costs more to buy than a used Skyhawk or Archer.

See Also

Technical Specifications

Dimensions & Weights

Wingspan 34 ft
Height
9 ft
Length
26 ft
Parking area (ft²2)
1,357 ft²
Max Takeoff Weight
Source: FAA Type Certificate Data Sheet 2,557 lbs
Max Landing Weight
2,557 lbs
Useful Load
Source: manufacturer figure 893 lbs
Fuel Capacity
61 gal

Performance

Cruise Speed
Source: manufacturer figure 134 KTAS
Never-Exceed (VNE)
Source: FAA Type Certificate Data Sheet 164 KIAS
Max Structural Cruise (VNO)
Source: FAA Type Certificate Data Sheet 130 KIAS
Approach Speed
77 KIAS
Stall, Clean (VS1)
Source: Pilot's Operating Handbook / Aircraft Flight Manual 59 KIAS
Range
Source: third-party reference 715 NM
Service Ceiling
12,000 ft
Rate of Climb
784 fpm
Takeoff over 50 ft obstacle
2,054 ft
Landing over 50 ft obstacle
1,709 ft

Engine

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