GlobalMilitary.net Open-source military intelligence Updated daily

Tecnam P2006T

Italian light twin-engine aircraft, notably used for training and light transport since the late 2000s. Key figures: top speed 287 km/h, range 1,722 km, service ceiling 4,267 m, max takeoff weight 1,180 kg, built 578. In service with 1 air force as of 2026 — Dominican Republic (1).

Max speed
287km/h
Range
1,722km
Produced
578units
Active worldwide
1
Tecnam P2006T military special mission aircraft side profile drawing
Side profile · Tecnam P2006T · length 8.7 m
Technical SpecificationsVersion: P2006T
Crew1
Length8.7 m (28.5 ft)
Wingspan11.4 m (37.4 ft)
Height2.8 m (9.3 ft)
Wing area14.8 m² (158.8 sqft)
Empty weight760 kg (1,676 lbs)
Max. takeoff weight1,180 kg (2,601 lbs)
Powerplant2 × pistons engine Rotax 912S3 75 kW each
PerformanceVersion: P2006T
Maximum speed287 km/h (178 mph)
Operational range1,722 km (1,070 mi)
Endurance5 hours
Service ceiling4,267 m (13,999 ft)
Climb rate6.4 m/s (21.0 ft/s)
Takeoff distance448 m (1,470 ft)
Operators — 2026
ActiveOn order
Compare This Aircraft
Tecnam P2006T vs
All Operators
🇩🇴 Dominican Republic· 🇮🇹 Italy

Description

The Tecnam P2006T is an Italian twin-engined light aircraft developed by Costruzioni Aeronautiche Tecnam. It was designed as a high-winged, all-metal aircraft and received airworthiness certification in the European Union by EASA under CS23 in 2003, type certification in 2009, and Federal Aviation Administration FAR Part 23 certification in 2010. The P2006T made its first flight on 13 September 2007 and was certified by EASA on 5 June 2009. A significant application of the P2006T's design is NASA's use of its basic structure for the all-electric X-57 Maxwell prototype aircraft.

Design

The P2006T is a twin-engined four-seat cantilever high-wing monoplane, equipped with retractable tricycle landing gear. Its stabilator, a single unit with a cutout in its leading edge, is attached to the fuselage aft of the vertical fin. The nosewheel retracts into the nose cone, while the main units retract into stubs extending from the lower fuselage. Access to the seating area is provided by a door on each side of the fuselage, with an additional escape hatch above the forward seats for emergency egress. The aircraft's Rotax engines feature liquid-cooled cylinder heads and cooling vanes on the cylinder barrels, necessitating both cooling airflow through the nacelle and a cooling radiator in each cowl. The electric starters are required for both ground starts and inflight restarts, prompting the addition of a backup battery for FAA certification. The pilot's power quadrant includes controls for throttle, propeller RPM, and carburetor heat for each engine; automatic mixture adjustment eliminates the need for a manual mixture control. Pushrods are used for linkage between the flight controls and the flight surfaces.

Operational History

The specifications mention a payload of 618 pounds (280 kg) with full fuel. The P2006T has seen service in a variety of roles and locations. The Italian Air Force utilizes three leased aircraft for multi-engine pilot training, designated as T-2006A. Several air forces such as the Dominican Air Force also employ the P2006T. Civilian operators include Harv's Air Service in Canada, Air Taxi in India, and the Romanian Aviation Academy. Law enforcement agencies such as the Guardia Civil in Spain and the Michigan Department of Natural Resources in the United States also operate the aircraft.

Variants

Main Variants:

  • P2006T: The standard civilian version of the aircraft, designed for general aviation use.

  • P2006T MRI: A maritime patrol variant, equipped for coastal surveillance and monitoring operations.

  • P2006T MMA: A multi-mission variant, modified by Airborne Technologies to incorporate specialized mission equipment.

  • T-2006A: The Italian military designation for P2006T aircraft used by the Italian Air Force's 70° Stormo in a training role, specifically for multi-engine pilot training.

Frequently Asked Questions

What type of aircraft is the Tecnam P2006T?
The Tecnam P2006T is a military special mission aircraft aircraft developed by Tecnam and entered service in 2010.
What is the maximum speed of the Tecnam P2006T?
The Tecnam P2006T has a maximum speed of 287 km/h (178 mph).
What is the range of the Tecnam P2006T?
The Tecnam P2006T has an operational range of 1,722 km (1,070 miles). This range can vary based on payload, altitude, and mission profile.
When did the Tecnam P2006T first fly?
The Tecnam P2006T made its first flight on September 13, 2007. It entered operational service in 2010.
How many Tecnam P2006T have been built?
Approximately 578 units of the Tecnam P2006T have been produced since it entered service in 2010.
Which countries operate the Tecnam P2006T?
The Tecnam P2006T is operated by 1 countries with approximately 1 aircraft in active service. The largest operators include Dominican Republic.
What is the service ceiling of the Tecnam P2006T?
The Tecnam P2006T has a service ceiling of 4,267 meters (13,999 feet). This is the maximum altitude at which the aircraft can maintain controlled flight.
Wikipedia (CC BY-SA) and other open sources. Illustrations generated by AI. Last updated on 27 July 2026. Suggest a change
Latest Data Updates
  1. JUL 272026 Updated Name updated
  2. APR 72026 Updated Picture credits updated in a site-wide editorial pass
  3. FEB 72026 Updated Endurance added
  4. JAN 122026 Updated Range updated in a site-wide editorial pass