Costruzioni Aeronautiche Tecnam
Tecnam P2006 Twin"2007"

RoleFour-seat light twin
National originItaly
ManufacturerTecnam
DesignerLuigi Pascale
First flight13 September 2007
Introduction2010
StatusIn production, active
Produced2007-present
Number built578 (24/8/2017)
VariantsTecnam MMA
Developed intoNASA X-57 Maxwell

 

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Costruzioni Aeronautiche Tecnam
Tecnam P2006 Twin"2007"

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Tecnam P2006 Twin"2007"

The Tecnam P2006T is an Italian high-winged, twin-engined all-meta light aircraft built by Costruzioni Aeronautiche Tecnam, which is based in Capua, Italy (near Naples). Certified in the European Union by EASA under CS23, the P2006T received Federal Aviation Administration FAR Part 23 certification in 2010.

The P2006T is the lightest twin-engined certified aircraft available, and is a four-seat aircraft with fully retractable landing gear and liquid-cooled Rotax engines that can run on 92 octane unleaded automotive gasoline as well as 100LL

Design

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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Tecnam P2006 Twin"2007"

P2006T
Standard civilian version.
P2006T MRI
Maritime patrol variant.
P2006T MMA
Multi-Mission variant modified with mission equipment by Airborne Technologies.
T2006A

Italian military designation for aircraft delivered in the Training role to 70° Stormo of the Italian Air Force on 5 July 2016 for multi-engine pilot training.

Specifications

  • Crew: 1 (pilot)
  • Capacity: 3 passengers or 618 pounds (280 kg) payload 
  • Length: 8.69 m (28 ft 6 in)
  • Wingspan: 11.40 m (37 ft 5 in)
  • Height: 2.84 m (9 ft 4 in)
  • Empty weight: 760 kg (1,675 lb)
  • Max takeoff weight: 1,230 kg (2,712 lb)
  • Powerplant: 2 × Rotax 912S3 horizontally opposed four-cylinder geared piston engines, 75 kW (100 hp) each
  • Maximum speed: 287 km/h (178 mph, 155 kn)
  • Cruise speed: 250 km/h (155 mph, 135 kn)
  • Stall speed: 87 km/h (54 mph, 47 kn)
  • Never exceed speed: 309 km/h (192 mph, 167 kn)
  • Minimum control speed: 115 km/h (71 mph, 62 kn)
  • Range: 1,374 km (853 mi, 742 nmi)
  • Endurance: 4.25 hours
  • Service ceiling: 4,300 m (14,000 ft)

Aircrafttoaal encyclopedia

The Tecnam P2002 Sierra is a two-seat, low-wing, light aircraft designed and constructed by the Italian aircraft manufacturer Tecnam. Introduced during the early 2000s, the aircraft quickly became a staple of the company's product lineup, comprising 70 percent of its available production capacity during some years.