Tecnam P-2004 Bravo
The Tecnam P2004 Bravo is an Italian light aircraft that combines a metal fuselage with composite wings. Its low wing, side-by-side seats, and Rotax engine make it a practical trainer and touring machine. It is part of Tecnam’s broad family of modern European light aircraft.
Did you know?
The Tecnam P2004 Bravo mixes a metal fuselage with composite wings, an unusual hybrid construction for a light trainer.
Specifications
| Length | 6.7 m (22 ft) |
|---|---|
| Wingspan | 8.7 m (28 ft) |
| Height | 2.3 m (8 ft) |
| Maximum passengers | 1 |
| Persons on board | 2 |
| Crew | 1 |
| Maximum take-off weight | 0.6 t |
| Range | 700 NM (1,296 km) |
| Maximum speed | 125 kt (232 km/h) |
| Stall speed | 45 kt (83 km/h) |
| Service ceiling | 15,000 ft (4,572 m) |
| Optimum ceiling | 10,000 ft (3,048 m) |
| Rate of climb | 1,100 ft/min (5.6 m/s) |
| Take-off distance | 140 m (459 ft) |
| Landing distance | 120 m (394 ft) |
| Fuel capacity | 100 l |
| Engines | 1x Rotax 912 |
Curated by CatchFlights from manufacturer documents, ICAO Doc 8643 and reference works; values are left out where no source could confirm them. Sources are listed on our credits page.
In CatchFlights
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