Tecnam P2004 Bravo

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]

P2004
Role Two-seat ultralight monoplane
National origin Italy
Manufacturer Tecnam
First flight 2002
Status Active

Specifications (P2004 Bravo)

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)
  • 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)
  • 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

Aircraft of comparable role, configuration, and era

References
  1. Bayerl, Robby; Berkemeier, Martin; et al. (2011). World Directory of Leisure Aviation 2011-12. Lancaster: WDLA UK. p. 80. ISSN 1368-485X.
  2. 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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