P2012 Traveller

 

visit: http://p2012.tecnam.org for more info.

 

Specification

Aircraft Dimensions

Fuselage Height 4.4 mt – 14.4 ft
Fuselage Length 11.8 mt – 38.7 ft
Wingspan 14 mt – 46 ft
Cabin Height (seat to cover) 1.35 mt – 4.4 ft
Cabin Width 1.47 mt – 4.8 ft
Max Seating capacity 2+9
Fuel tank capacity 750 lt – 198 US Gal

Powerplant

Engine Manufacturer Lycoming TEO-540-C1A
Engine Power 2 x 375 HP
Time Before Overhaul 2000 hrs
Propeller 2 x 4 blades constant speed
Fuel Consumption
Fuel Type 100/130, 100LL and UL100

Design Weight & Loading

Maximum Take Off Weight 3600 kg – 7936.64 lb
Empty Weight, Standard 2286 kg – 5040 lb
Useful Load 1332 kg – 2937 lb

Performance

Max Cruise Speed (KTAS) 190 kts @ 10.000 ft
Stall Speed (Flaps Down Power Off) KCAS 126 km/h – 68 kt
Practical ceiling
Take off run 380 m – 1246 ft
Take off distance 654 m – 2146 ft
Landing Run 295 m – 968 ft
Landing Distance 546 m – 1791 ft
Rate of climb 6 m/sec – 1,200 ft/min
Range + 950 nm + 6.3 hrs
Flight Rule VFR Day/Night, Fully IFR

Specifications subject to change without notice. Always consult the Aircraft Flight Manual.

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