Tecnam P2004 Bravo
From Wikipedia, the free encyclopedia
The Tecnam P2004 Bravo is a high-wing, light aircraft built by the Tecnam aircraft company. It is similar to the Tecnam P92 Echo Super, but has a cantilevered wing rather than the P92's strut-braced wing.[1]
Specifications (P2004 Bravo)
Data from http://www.tecnam.com/ing/p_2004Bravo.cfm
General characteristics
- Crew: one, pilot
- Capacity: one passenger
- Length: 6.61 m (21 ft 8 in)
- Wingspan: 8.40 m (27 ft 6 in)
- Height: 2.60 m (8 ft 6 in)
- Wing area: 11 m2 (118.4 ft2)
- Empty weight: 331 kg (730 lb)
- Useful load: 269 kg (590 lb)
- Max. takeoff weight: 600 kg (1,320 lb)
- Powerplant: 1 × Rotax 912ULS GT, 100 hp (73.5 kW)
Performance
- Never exceed speed: 290 km/h (156 kt)
- Maximum speed: 222 km/h at sea-level (120 kt)
- Cruise speed: 215 km/h (116 kt)
- Stall speed: 64 km/h (34.5 kt)
- Service ceiling: 4000 m (13110 ft)
- Rate of climb: 366 m/min (1,200 ft/min)
- Wing loading: 54 kg/m2 (11.15 lb/ft2)
- Take off run: 140 m (460 ft)
- Landing distance: 120 m (394 ft)
See also
- Aircraft of comparable role, configuration and era
References
- ↑ Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 80. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
External links
 |
Wikimedia Commons has media related to Tecnam. |
| |||||
| ||||||||||||||
This article is issued from Wikipedia. The text is available under the Creative Commons Attribution/Share Alike; additional terms may apply for the media files.