Tecnam P2004 Bravo
| P2004 | |
|---|---|
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| |
| Role | Two-seat ultralight monoplane |
| National origin | Italy |
| Manufacturer | Tecnam |
| First flight | 2002 |
| Status | Active |
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)
[edit]Data from Jane's All the World's Aircraft 2010-11[2]
General characteristics
- Crew: 1
- Capacity: 3 pax
- Length: 6.61 m (21 ft 8 in)
- Wingspan: 8.6 m (28 ft 3 in)
- Height: 2.6 m (8 ft 6 in)
- Wing area: 11 m2 (120 sq ft)
- Empty weight: 336 kg (741 lb)
- Max takeoff weight: 600 kg (1,323 lb)
- Max useful weight: 269 kg (593 lb)
- Powerplant: 1 × Rotax 912 ULS 4-cylinder air-cooled horizontally-opposed piston engine, 73.5 kW (98.6 hp)
- Propellers: 2-bladed Tonini fixed-pitch propeller
Performance
- Maximum speed: 238 km/h (148 mph, 129 kn) at sea level
- Cruise speed: 215 km/h (134 mph, 116 kn) (75% power)
- Stall speed: 84 km/h (52 mph, 45 kn) flaps up
- 64 km/h (40 mph; 35 kn)
- Never exceed speed: 290 km/h (180 mph, 160 kn)
- Range: 1,092 km (679 mi, 590 nmi)
- Service ceiling: 4,420 m (14,500 ft)
- g limits: +6 -3
- Rate of climb: 5.6 m/s (1,100 ft/min)
- Wing loading: 54 kg/m2 (11 lb/sq ft) [citation needed]
- Take-off run: 140 m (459 ft)
- Landing run: 120 m (394 ft)
Avionics
- Icom IC-A-200 radio
- AvMap EKP-IV colour GPS
- optional Garmin suite
See also
[edit]Aircraft of comparable role, configuration, and era
References
[edit]
Wikimedia Commons has media related to Tecnam P2004 Bravo.
- ^ Bayerl, Robby; Berkemeier, Martin; et al. (2011). "World Directory of Leisure Aviation 2011-12". World Directory of Light Aviation. Lancaster: WDLA UK: 80. ISSN 1368-485X.
- ^ Jackson, Paul, ed. (2010). Jane's All the World's Aircraft 2010-11 (101st ed.). London: Jane's Information Group. p. 407. ISBN 978-0710629166.
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