A continuous improvement effort with advanced computer design, structural and fluid dynamics modelling led TECNAM to the P2002. Tapered wing, laminar airfoils, slotted flaps, up turned wing tips and a streamlined fuselage led the P2002 to outstanding performances. The P2002-JF (JAR-VLA certified) and P2002 Sierra (Ultralight versions) match any possible customer desire. The Tecnam P2002, a symphony of aerodynamic and structure effectiveness.

TECHNICAL FEATURES
Wing span 8,60 m 28.2 ft
Length over-all 6,61 m 21.7 ft
Height over-all 2.43 m 7.8 ft
Width cabin 1.10 m 43.3”
Wing area 11.5 m2 123.8 sq.ft.
Wing Dihedral 5° 5°
Tailplane span 2,9 m 9.5 ft
Wheel track 1,85 m 6.1 ft
Wheel tyres 5,00-5 5,00-5
ENGINE & PROPELLER
Engine Rotax 912 S (FAR 33)
Power max. 100 Hp @ 5800 rpm
Reduction 2.4286 : 1
Propeller Hoffmann H017GHM
Fuel Leaded, Unleaded or AvGas
Tanks 100 Lt. (2x50)26.4 US gal
WEIGHT
MTOW 580 Kg 1279 lbs.
Std empty weight 320 kg 705 lbs.
Load ultimate factor +6 -3 +6 -3
PERFORMANCES (MTOW - ISA cond.)
Max speed s/l 241 km/h 130 KTS
Cruising speed 75% 215 km/h 116 KTS
Rate of climb @ s/l 5.3 m/sec 1050 ft/min
Stalling speed (flap) 72 Km/h 39 KTS
Service ceiling 4267 m 14000 ft
Take off run 180 m 591 ft
Landing run 125 m 410 ft
VNE 290 km/h 156 KTS