The Tecnam P2006T
A modern 4-seat aircraft built for efficiency, safety, and travel
The Tecnam P2006T
A modern 4-seat aircraft built for efficiency, safety, and travel
Why Pilots Love the P2006T
The Tecnam P2006T has earned a reputation as one of the most versatile light twins in the world, combining jet-like handling with the efficiency of twin Rotax 912 engines. With a modern Garmin G1000 NXi cockpit, impressively low operating costs, and the ability to run on mogas or avgas, the P2006T delivers twin-engine safety without the usual complexity or expense.
Add in Tecnam’s renowned Italian design and a proven global training record, and it’s clear why the P2006T has become the preferred twin for flight schools and private owners alike.
Tecnam P2006T Specs
Performance numbers and key features that set the P2006T apart from other four-seat aircraft.
9 gal/hr fuel burn
2 × Rotax 912S3, 4-cylinder, 100 HP each, with electronic fuel injection and reduction gear
145 kts max speed
(10,000 ft, MCP)
140 kts cruise speed at 75% (10,000ft)
14,000 ft service ceiling
Max. operating altitude (4,267 m)
14,000 ft single engine service ceiling
1,036 ft/min max. rate of climb (MSL)
1,100 nm max range
Includes auxiliary tanks which are standard in the USA
9 US gal/hr fuel consumption at 60 %
4 seat capacity
Comfortable access for all on board is assured through the two forward gull wing doors and the huge rear door that provides access to all rear seats
816 lbs useful load
Baggage is stowed in the generous nose compartments and cabin, offering maximum loading flexibility for any mission.
Tecnam P2006T Specs
Performance numbers and key features that set the P2006T apart from other four-seat aircraft.
9 gal/hr fuel burn
Fuel consumption (34 I/h)
2 × Rotax 912S3, 4-cylinder, 100 HP each, with electronic fuel injection and reduction gear
145 kts max speed
(10,000 ft, MCP)
140 kts cruise speed at 75 % (10,000 ft)
14,000 ft service ceiling
Max operating altitude
1,036 ft/min max rate of climb (MSL)
1,100 nm max range
Includes auxiliary tanks which are standard in the USA
9 US gal/hr fuel consumption at 60 %
4 seat capacity
Comfortable access for all on board is assured through the two forward gull wing doors and the huge rear door that provides access to all rear seats
816 lbs useful load
Baggage is stowed in the generous nose compartments and cabin, offering maximum loading flexibility for any mission
Twin-Engine Performance That Leads Its Class
The Tecnam P2006T delivers twin-engine safety, advanced Garmin avionics, and efficient Rotax power—making it the smart, cost-effective choice for training and personal flying alike.
P2006T Market: Curious about pricing?
See our live P2006T for sale listings for real-time market prices.
Design and Comfort
The wing construction incorporates advanced materials and aerodynamics to improve fuel efficiency and reduce environmental impact. Furthermore, the fuselage is made from durable, lightweight composite materials, which contribute to the aircraft's overall fuel efficiency and help reduce the environmental footprint. Its design prioritizes both aerodynamics and pilot comfort, ensuring a smooth and efficient flying experience.
The P2006T is engineered for low fuel consumption and reduced emissions, aligning with modern aviation's shift toward greener practices. Its efficient twin-engine configuration ensures optimal performance while maintaining a lower environmental impact compared to larger, less efficient aircraft.
Safety Record and Features
Safety is provided by the twin-engine configuration, which burns less fuel than comparable single-engine competitors; safety of flight is enhanced by the TAS 800 Garmin.
Retractable landing gear and variable pitch MEP for all types of pilot training using a single platform.
The superior high-wing configuration offers stability, superior cabin visibility and easy access for passengers and luggage. TECNAM has used its extensive experience with aluminium airframes to create a robust yet very light airframe in the TECNAM P2006T, resulting in an outstanding payload-to-total-weight ratio, with total average consumption of 34 L/H, and as low as 25 L/H in holding/loiter.
Propulsion and Avionics
The Tecnam P2006T is powered by twin 100-HP Rotax 912S3 engines with efficient three-blade constant-speed propellers for smooth, economical performance. Its Garmin G1000 NXi cockpit and GFC 700 autopilot deliver advanced navigation, communication, and safety features. Together, they make the P2006T a modern, reliable platform for training and touring alike.
Training Excellence
The Tecnam P2006T redefines flight training by offering a superior platform for aspiring pilots to reach their full potential. As a light twin-engine aircraft, the P2006T provides an excellent training environment for both general aviation and commercial purposes. Its combination of reliable performance, advanced avionics, and versatile design makes it the first choice for flight schools offering Private Pilot License (PPL), Instrument Rating (IR), and Multi-Engine Rating (ME) training. Its stable flight characteristics, fuel efficiency, and user-friendly systems ensure a positive and valuable learning experience.
Explore the Entire Tecnam Family
Learn about the history of Tecnam Aircraft, the unique qualities of each model, and what makes Tecnam among the most advanced and trusted general aviation manufacturers in the world today.
Frequently Asked Questions
The P2006T is powered by two 100-horsepower Rotax 912 S3 engines, known for reliability and low fuel consumption.
It can operate on either avgas or unleaded mogas, giving owners flexibility and lower fuel costs.
Typical cruise speed is around 145 knots, depending on weight and conditions.
It can fly up to about 650 nautical miles on standard tanks.
The P2006T features the Garmin G1000 NXi glass cockpit with a GFC 700 autopilot.
Yes, it’s certified for single-pilot IFR operations under CS-23/FAR-23 standards.
It typically burns about 9–10 gallons per hour total, making it one of the most efficient twins in its class.
The aircraft offers a useful load of roughly 900 pounds, depending on configuration.
It requires about 1,300 feet to clear a 50-foot obstacle under standard conditions.
It combines twin-engine safety with remarkably low operating costs and simple systems.
It’s popular with flight schools, private owners, and government operators needing a dependable light twin.
Powerplant
|
|
||
|---|---|---|
|
Engine |
2 × Rotax 912S3, four-stroke, fuel-injected, 100 HP each | |
|
Propeller |
2 × MTV-9-B/190-56, 3-blade constant speed propeller | |
|
Fuel grades |
Mogas and Avgas |
Performance (max. mass)
|
Max. cruise speed |
269 km/h | 145 kts | ||
|---|---|---|---|---|
|
Stall speed, landing configuration |
102 km/h | 55 kts | ||
|
Rate of climb (MSL) |
5.3 m/s | 1,036 ft/min | ||
|
Take off run |
301 m | 988 ft | ||
|
Take off distance |
394 m | 1,293 ft | ||
|
Landing run |
231 m |
758 ft | ||
|
Landing distance |
349 m | 1,145 ft | ||
|
Max. operating altitude |
4,267 m | 14,000 ft | ||
|
Fuel consumption |
34 l/h |
9 US gal/h |
Dimensions
Mass and Loading
|
Seats |
4 | |||
|---|---|---|---|---|
|
Empty weight |
860 kg | 1,896 lbs | ||
|
Useful load |
370 kg | 816 lbs | ||
|
Max. take off mass |
1,230 kg | 2,712 lbs | ||
|
Main tank capacity |
200 L | 53 US gal |
Interested in the P2006T?
Reach out to us to see if this plane is a good fit for your mission.
Interested in the P2006T?
Reach out to us to see if this plane is a good fit for your mission.
