Tecnam
P2006T Twin

The Tecnam P2006T is an Italian high-winged twin-engined all-metal light aircraft,[1] built by Costruzioni Aeronautiche Tecnam.

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Tecnam P2006T Twin engine

The Tecnam P2006T is an Italian high-winged twin-engined all-metal light aircraft,[1] built by Costruzioni Aeronautiche Tecnam based in Capua, Italy, near Naples. The P2006T received airworthiness certification in the European Union by EASA under CS23 in 2003,[2] type certification in 2009,[2] and Federal Aviation Administration FAR Part 23 certification in 2010

Development
The P2006T is a twin-engined four-seat cantilever high-wing monoplane with a retractable tricycle landing gear. Its stabilator is attached to the fuselage, mostly aft of the vertical fin (the stabilator is a single unit with a cutout in its leading edge where it mounts to the tailcone). The nosewheel of the tricycle landing gear retracts into the nose cone; the trailing-link main units retract into stubs which extend from the lower fuselage. The fuselage section is a slightly rounded rectangle, higher than it is wide. A door on each side of the fuselage provides access to the seating area; in addition an escape hatch is provided above the two forward seats, to be used if fuselage deformation in a crash prevents those doors from being operable

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Honda Aircraft Company

Tecnam P2006T

"Your exciting Journey into the world of aviation starts here".

Tecnam  Aircraft 

General Info

      • Crew: 1
      • Capacity: 3 passengers or 618 pounds (280 kg) payload with full fuel
      • Length: 8.7 m (28 ft 7 in)
      • Wingspan: 11.4 m (37 ft 5 in)
      • Height: 2.90 m (9 ft 6 in)
      • Wing area: 14.8 m2 (159 sq ft)
      • Aspect ratio: 8.80
      • Empty weight: 819 kg (1,806 lb)
      • Max takeoff weight: 1,230 kg (2,712 lb)
      • Fuel capacity: 200 litres (44 imp gal; 53 US gal)
      • Powerplant: 2 × Rotax 912S3 horizontally opposed four-cylinder

 P2006T

Performance

    • Maximum speed: 287 km/h (178 mph, 155 kn)
    • Cruise speed: 269 km/h (167 mph, 145 kn)
    • Stall speed: 102 km/h (63 mph, 55 kn)
    • Never exceed speed: 309 km/h (192 mph, 167 kn)
    • Minimum control speed: 115 km/h (71 mph, 62 kn)
    • Range: 1,204 km (748 mi, 650 nmi)
    • Endurance: 4.25 hours
    • Service ceiling: 4,300 m (14,000 ft)
    • Rate of climb: 5.3 m/s (1,040 ft/min) 250 ft/min (single engine)
    • Wing loading: 78 kg/m2 (16 lb/sq ft) at MTOW
    • Power/mass: 0.162 
Data from Wikipedia

Drawing

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