P2008 | |
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Role | Light aircraft |
National origin | Italy |
Manufacturer | Costruzione Aeronautiche Tecnam |
First flight | 30 September 2009 |
Introduction | 2009 |
Unit cost |
US$154,999 (basic instrumentation, 2011)
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The Tecnam P2008 is a single-engine, high-wing two-seat aircraft built in Italy but aimed at the US market. It is the first Tecnam aircraft to incorporate major composite components. It was introduced at the AERO Friedrichshafen 2009 show, with first deliveries in December 2009.
The P2008 is a conventionally laid out strut braced high-wing monoplane aimed specifically at the US market. Resembling the earlier Tecnam P92 and P2004 in general appearance, the P2008 differs by introducing a carbon fibre fuselage and integrated fin. The wings and tailplane are all-metal. It can be adapted to LSA, ultralight or ELA1 categories.
The wing leading edge is straight except for some pinching at the root and the wing has constant chord over about the inner 60% of span. Outboard, the trailing edge is tapered; the straight wing tips are slightly upturned. Frise ailerons on piano hinges span the outboard sections and the inner sections are spanned by slotted flaps. There is a single lift strut on each side, attached to the lower fuselage. The P2008 has a low set all-moving constant chord tailplane with an anti-balance tab. The fin is swept and the rudder moves above the tailplane.