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Piston TwinsP2006T SeriesIntroduced 2009

Tecnam

P2006T

The Tecnam P2006T is a four-seat twin-engine composite light aircraft powered by two Rotax 912S3 engines of 100 hp each, making it the lightest and most fuel-efficient twin-engine trainer certified under CS-23/FAR Part 23. It is widely used by flight academies worldwide for multi-engine training thanks to its low operating costs, modern Garmin G1000 avionics, and docile handling. The P2006T's lightweight design and Rotax engines result in significantly lower fuel burn than traditional piston twins.

  • Lightest FAR Part 23 certified twin-engine aircraft
  • Twin 100 hp Rotax 912S engines — very low fuel burn
  • Cost-effective multi-engine training platform
  • Garmin G1000 glass cockpit
  • All-composite airframe with modern design
  • Widely operated by European and global flight academies
Tecnam P2006T

P2006T key specifications

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

About the P2006T

Introduced in 2009 in Italy, the Tecnam P2006T is a twin-engine piston aircraft from the P2006T Series family built for the redundancy of two engines at modest running cost. It is a current-generation design.

On performance, it offers a maximum range of about 800 nautical miles and a cruise of roughly 148 knots. It seats up to 4 passengers and is powered by 2 Rotax 912S3 (x2) engines.

Its 800 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. Use the comparisons below to see how the P2006T stacks up against similar aircraft, then request a tailored assessment.

Gallery

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At a glance

Performance

Max Range
800 nm
Cruise Speed
148 kt
Max Seats
4
MTOW
2,756 lbs

Full specifications

Operator and certification details for the P2006T, plus the complete performance, dimensions, weights and powerplant sheet — free with an account.

Country of Origin
Italy
Engines
2 × Piston
Engine Model
Rotax 912S3 (x2)
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 twin like the P2006T 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
~77%
of typical new value retained
At 10 years
~60%
of typical new value retained
At 15 years
~46%
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 P2006T. 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 P2006T cost of ownership with our free calculator.

Ownership & ROI calculator

Model the true economics of owning or chartering the P2006T. Pre-filled with realistic defaults for this type — adjust any assumption and the results update instantly.

Model the economics of the P2006T

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 P2006T compares

Side by side with the most similar piston twins.

Performance
Range
800 nm
1,140 nm
1,000 nm
1,020 nm
Cruise speed
148 kt
155 kt
175 kt
185 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
6
6
4
Crew
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Max takeoff weight
2,756 lbs
4,594 lbs
5,200 lbs
4,078 lbs
Length
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Cabin height
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Locked — sign in to view
Powerplant
Engines
2 × Piston
2 × Piston
2 × Piston
2 × Piston
Engine model
Rotax 912S3 (x2)
Lycoming IO-360-A1B6
Lycoming IO-540-C4B5
Austro Engine AE330 (x2)

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

Beyond the spec sheet

Buying or operating the P2006T? Get an independent acquisition recommendation, or see how fleet management keeps operations, maintenance, crew and compliance in one place.

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