Aircraft History, Specification and Information
Tecnam P2002
Tecnam P2002-JF - HB-KOS
2007 Tecnam P2002-JF - HB-KOS (sn 053)
Photo taken Sep. 11, 2011
Grenchen Flugplatz - Switzerland (ZHI / LSZG)
Photo © Marcel Siegenthaler

The Tecnam P2002 is a two seat, low-wing, light aircraft built by Tecnam, constructed from aluminium and powered by a single Rotax 912 engine. The aircraft features a sliding canopy which can be opened in flight.

Variants

  • P2002-JF - Certified single engine
  • P2002-JR - Certified single engine with retractable landing gear
  • P2002 Sierra - Light Sport Aircraft (LSA)
  • P2002 Sierra RG - Advanced ultralight with retractable landing gear

Specifications (P2002-JF)

General characteristics
Capacity: 1 crew & 1 passenger
Length: 21 ft 7 in (6.63 m)
Wingspan: 28 ft 2 in (8.6 m)
Height: 7 ft 9 in (2.4 m)
Wing area: 124 ft² (11.5 m²)
Empty weight: 790 lb (360 kg)
Max takeoff weight: 1,320 lb (600 kg)
Powerplant: 1 × Rotax 912 S2, 100 hp (75 kW) at 5,800 rpm
Propeller diameter: 5 ft 3 in (1.6 m)

Performance
Never exceed speed: 138 knots (256 km/h)
Cruise speed (75% power): 113 knots (210 km/h)
Fuel consumption: 5 US gal/h (19 Lt./h) of mogas

Last updated November 20, 2011
This article is licensed under the GNU Free Documentation License. It uses material from the Wikipedia article "Tecnam P2002".
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