P2006T SMP

SPECIAL MISSION  PLATFORM The TECNAM SMP is based on the revolutionary aircraft TECNAM P2006T, the only twin engine aircraft that can fully match all the today special missions purposes due to its characteristics.
Categories: Special Mission
Specification

Aircraft Dimensions

Fuselage Height 2,58 mt – 8.46 ft
Fuselage Length 8.7 mt – 28.5 ft
Wingspan 11.4 mt – 37.4 ft
Cabin Height (seat to cover) 0.91 mt – 3 ft
Cabin Width 1.22 mt – 4 ft
Max Seating capacity 4
Fuel tank capacity 2×100 lt – 2×26.4 US Gal

Powerplant

Engine Manufacturer ROTAX 912 S3
Engine Power 100 + 100 HP
Time Before Overhaul 2000 hrs
Propeller Two-Bladed Constant Speed Full Feathering
Fuel Consumption 17 + 17 lt/h – 4.50 + 4.50 US Gal/h
Fuel Type Mogas and Avgas
 

Design Weight & Loading

Maximum Take Off Weight 1230 kg – 2712 lb
Empty Weight, Standard 819 kg – 1806 lb VFR Standard
Useful Load 411 kg – 906 lb
Baggage allowance 80 kg – 176 lb

Performance

 

Max Cruise Speed (KTAS) 278 km/h – 150 kts
Stall Speed (Flaps Down Power Off) KCAS 102 km/h – 55 kts
Practical ceiling 4267 mt – 14,000 ft
Take off run 301 mt – 988 ft
Take off distance 394 mt – 1293 ft
Landing Run 231 mt – 758 ft
Landing Distance 349 mt – 1145 ft
Rate of climb 5.3 m/sec – 1036 ft/min
Range 669 NM – 1239 km
Flight Rule VFR Day, VFR Night, IFR