P2008 MKII
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Aircraft Dimensions
| Fuselage Height | 4.4 mt – 14.4 ft |
| Fuselage Length | 11.8 mt – 39.7 ft |
| Wingspan | 14 mt – 46 ft |
| Cabin Height (seat to cover) | 1.36 mt – 4.46 ft |
| Cabin Width | 1.48 mt – 4.85 ft |
| Max Seating capacity | 2+9 |
| Fuel tank capacity | 800 lt – 212 US Gal |
Performance
| Max Cruise Speed (KTAS) | 190 kts @ 10.000 ft |
| Stall Speed (Flaps Down Power Off) KCAS | 60 kts – 111 km/h |
| Practical ceiling | |
| Take off run | 350 mt – 1148 ft |
| Take off distance | 600 mt – 1968.5 ft |
| Landing Run | 250 mt – 820 ft |
| Landing Distance | 500 mt – 1640 ft |
| Rate of climb | 7,62 m/s – 1500 ft/min |
| Range | 1.137 nm 6.3 hrs |
| Flight Rule | VFR Day/Night, Fully IFR |
Design Weight & Loading
| Maximum Take Off Weight | 3600 kg – 7936.64 lb |
| Empty Weight, Standard | 2250 kg – 4960 lb |
| Useful Load | 1350 kg – 2976 lb |
Powerplant
| Engine Manufacturer | Lycoming TEO-540-C1A |
| Engine Power | 2 x 375 HP |
| Time Before Overhaul | 2000 hrs |
| Propeller | 2 x 3 blades constant speed |
| Fuel Consumption | 30 US Gal/h |
| Fuel Type | 100/130, 100LL and UL100 |