PERFORMANCE
Performance Figures Below are for aircraft at MAUW
Rotax 582 'C' Box engine fitted with two blade DUC Prop
Jabiru fitted with Newton 2 blade wood 60" x 40".
Verner 133M 2:1 box fitted with 2 blade DUC prop.
All aircraft fitted with doors.
| 582DCDI | Jabiru | Verner 133M | |||||||||||||
| Stall Speed | 28 mph | Stall speed | 32 mph | Stall speed | 32 mph | ||||||||||
| V.N.E. | 98 mph | V.N.E. | 98 mph | V.N.E. | 98 mph | ||||||||||
| Cruise Speed | 70 mph | Cruise Speed | 75 mph | Cruise Speed | 80 mph | ||||||||||
| Climb Speed | 40 mph | Climb Speed | 40 mph | Climb Speed | 40 mph | ||||||||||
| Rate of Climb | 700 ft/min | Rate of Climb | 700 ft/min | Rate of Climb | 800 ft/min | ||||||||||
| Glide Ratio | 7@40 mph | Glide Ratio | 7@40 mph | Glide Ratio | 7@40 mph | ||||||||||
| Fuel Consumption | 16 Ltr/hr | Fuel Consumption | 11 ltr/hr | Fuel Consumption | 11 ltr/hr |
Structurally the Falcon has been tested, at it's all up weight of 450kg,
to 6 Gs positive and 3 Gs negative. This is far beyond the limits, to which the aircraft
will be exposed to, even in the worst turbulent conditions.