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.
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 |