P2002 Sierra click photos for larger versions   Download your Sierra PDF file       See bottom of page for SLIDE SHOW of the P2002 Sierra retractable (1:17 min) This slideshow is courtesy of Sato International AG, Mellingham, Switzerland www.tecnamswiss.ch   P2002 Sierra The tapered wing improves the aerodynamic characteristcs of the aeroplane which join with elimination of any sharp corner on the fuselage section and the cabin profile enhances its performance. The landing gear, tested on over one thousand units, is the same of the previous Tecnam models. The wing-integrated tanks provide 50 litres each. The fuselage structure is a steel Cr-Mo tubing framework for the cabin area to guarantee a high capacity to absorb energy in case of crash landing, and light alloy tail cone to support the empennage. The entirely moving tail plane permits superior control and a high degree of stick-free stability. Flight controls are traditional type with dual Stick, dual pedals and dual throttles knobs on control panel. Longitudinal trim and flaps are electric with position indicators on the instrument panel.   Specifications for P2002 Sierra   DIMENSIONS     Wingspan 28.2 ft 8.6 m Height overall 7.8 ft 2.43 m Length overall 21.7 ft 6.61 m Width cabin 43.33" 1.1 m Wing area 123.8 sq ft   Wing dihedral 5º 5º Wheel track 6.1 ft 1.85 m Wheel tyres 5.00-5 5.00-5   ENGINE & PROPELLER   Engine Rotax 912ULS Power max. 100 Hp (73.5 KW) 5800 rpm Reduction 2.42861 : 1 Propeller GT Tonini Fuel Euro Super, Unleaded or AvGas Tanks 100 lt (2 x 50) 24.4.US Gal   PERFORMANCE     Max speed s/l   135 kts Cruising Speed (75%) 5250 rpm   119 kts Rate of Climb   1200 ft/min Stalling Speed (with flap)   35 kts Service Ceiling   14,500 ft Take off run   180m Landing Run   125 m VNE   138 kts   WEIGHT     Designed MTOW   600 kg Average Empty weight LSA Specification   340 kg Load ultimate factor   +6 -3     Click PLAY button to start