P2004 Bravo
The P2004 Bravo is a cantilevered high wing, twin side by side seat airplane. The P2004 Bravo features a refined aerodynamic with a tapered cantilevered wing. Laminar airfoils, large slotted flaps with up-turned wing tips lead, together with a streamlined fuselage, to a high performance airplane with increased cruise speed and range. The planes outstanding performance and flying qualities together with low operating costs, easy piloting and maintenance, make of this aircraft an excellent solution for the flying-schools and training activity, and also for many other missions as touring, territory surveillance, patrol, etc.
| DIMENSIONS | ft | m | ENGINE | |
|---|---|---|---|---|
| Wing Span: | 27.5 ft | 8.40 m | Engine: | Rotax 912ULS |
| Length over-all: | 21.7 ft | 6.61m | Power max: | 100 Hp @ 5800 rpm |
| Height over-all: | 8.5 ft | 2.60 m | Reduction: | 2.4286 : 1 |
| Width cabin: | 45" | 1.15 m | Propeller: | GT Tonini |
| Wing area: | 118.4 sq ft | 11.0 m² | Fuel: | Leaded, Unleaded or AvGas |
| Wing Dihedral: | 1.5° | 1.5º | Tanks: | 100 Lt (2 x 50) 26.4 US Gal |
| Tailplane span: | 9.5 ft | 2.9 m | ||
| Wheeltrack: | 6.1 ft | 1.85 m | ||
| Wheel tyres: | 5.00-5 | 5.00-5 |
| PERFORMANCES | WEIGHT | kg | |
|---|---|---|---|
| Max Speed s/l: | 130 kts | MTO design weight: | 600 kg |
| Cruising Speed 75% (19 litres/hour): | 115 kts | MTOW: | 600 kg (LSA) |
| Rate of Climb @ s/l: | 1200 ft/min | Average empty weight: | 340 kg |
| Stalling speed (flap): | 34.5 kts | Load ultimate factor: | (+6 / -3) |
| Service Ceiling: | 14000 ft | ||
| Take off run: | 140m | ||
| Landing run: | 121m | ||
| VNE: | 138 kts |
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