Tecnam P2004 Bravo

P2004
Role	Two-seat ultralight monoplane
National origin	Italy
Manufacturer	Tecnam
First flight	2002
Unit cost	$145,000 in 2010

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

• Tecnam P92

References

External links

Wikimedia Commons has media related to Tecnam.

• Company web site