Tecnam P2006T SMP

The Tecnam P2006T SMP (Special Mission Platform) is a versatile twin-engine light aircraft developed by Tecnam, an Italian aerospace manufacturer. Specifically designed for special missions, this aircraft is a modified variant of the Tecnam P2006T.

The Tecnam P2006T SMP offers a durable yet lightweight airframe constructed with advanced materials, providing stability and efficiency during flight. Its twin-engine configuration, powered by modern Rotax engines, ensures reliability and fuel efficiency, making it suitable for various specialized operations.

What distinguishes the P2006T SMP is its adaptability for different mission requirements. It can be equipped with specialized sensors, surveillance equipment, and additional systems tailored to specific tasks such as aerial photography, environmental monitoring, reconnaissance, and law enforcement missions.

The interior of the aircraft is versatile, allowing for the integration of mission-specific equipment while accommodating a pilot and a co-pilot comfortably. The cabin’s flexibility makes it suitable for various mission profiles, providing ample space for essential technology and personnel.

The P2006T SMP is equipped with modern avionics and navigation systems, ensuring enhanced operational capabilities and safety features for pilots during specialized missions.

Overall, the Tecnam P2006T SMP stands out as a reliable and adaptable platform, well-suited for diverse special missions due to its sturdy design, efficient performance, and capacity for customization to meet the specific operational needs of various specialized tasks.

P2006T SMP

The TECNAM P2006T SMP is built on the innovative TECNAM P2006T aircraft, uniquely capable of fulfilling various special missions. It’s fully certified for IFR under CS/FAR 23 standards, available with analog or digital cockpit options, and recognized in multiple countries besides EASA/FAA regulations.

Offering cost-effectiveness, it boasts a low initial purchase price and minimal operation and maintenance expenses. It allows for single-pilot IFR operations, ensuring flexibility and reduced operational costs.

Moreover, the P2006T SMP offers versatility by accepting both Aviation and Automotive fuel (even with up to 10% ethanol content), allowing mixing in any ratio. It’s designed with a weight-saving program, providing a high payload capacity for mission-specific requirements.

The aircraft also demonstrates a wide speed range, cruising comfortably between 55 to 145 knots, catering to various mission demands efficiently.

Specifications

ItemDescription
Length28.5 ft (8,7 m)
Height8.46 ft (2,58 m)
Wingspan37.4 ft (11,4 m)
Area159 ft2 (14,8 m2)
Main Door Width25 in (634 mm)
Main Door Height38 in (970 mm)
Max Seating capacity4
Max cruise speed150 kts (278 km/h)
Stall Speed (Flaps Down Power Off)55 kts 102 km/h
Maximum Take Off Weight2712 lb (1230 kg)
Empty Weight, Standard1933 lb (877 kg)
Useful Load779 lb (353 kg)
Baggage allowance176 lb (80 kg)
Engine ManufacturerROTAX 912 S3