Tecnam P2004
From Wikipedia, the free encyclopedia
The Tecnam P2004 is a high-wing, light aircraft built by the Tecnam aircraft company. It is similar to the Tecnam P92 Echo Super, but with a cantilevered wing in place of the P92's strut-braced wing.
[edit] External links
[edit] Specifications (P2004 Bravo)
This aircraft article is missing some (or all) of its specifications. If you have a source, you can help Wikipedia by adding them.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 lbs)
- Useful load: 269 kg (590 lbs)
- Max takeoff weight: 600 kg (1,320 lbs)
- Powerplant: 1× Rotax 912ULS, 100 hp (73.5 kW)
Performance
- Never exceed speed: 290 km/h (156 kts)
- Maximum speed: 222 km/h at sea-level (120 kts)
- Cruise speed: 215 km/h (116 kts)
- Stall speed: 64 km/h (34.5 kts)
- Service ceiling 4000 m (13110 ft)
- Rate of climb: 366 m/min (1,200 ft/min)
- Wing loading: 54 kg/m2 (11.15 lbs/ft2)
- Take off run: 140 m (460 ft)
- Landing distance: 120 m (394 ft)
[edit] See also
Comparable aircraft Tecnam P92
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