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.

Specifications (P2004 Bravo)

Data from Jane's All the World's Aircraft 2010-11

General characteristics

  • Crew: 1
  • Capacity: 1 passenger
  • Length: 6.61m (21ft 8in)
  • Wingspan: 8.6m (28ft 3in)
  • Height: 2.6m (8ft 6in)
  • Wing area: 11m2 (120sqft)
  • Empty weight: 336kg (741lb)
  • Max takeoff weight: 600kg (1,323lb)
  • Max useful weight: 269kg (593lb)
  • Powerplant: 1 × Rotax 912 ULS 4-cylinder air-cooled horizontally-opposed piston engine, 73.5kW (98.6hp)
  • Propellers: 2-bladed Tonini fixed-pitch propeller

Performance

  • Maximum speed: 238km/h (148mph, 129kn) at sea level
  • Cruise speed: 215km/h (134mph, 116kn) (75% power)
  • Stall speed: 84km/h (52mph, 45kn) flaps up

64km/h (40mph; 35kn)

  • Never exceed speed: 290km/h (180mph, 160kn)
  • Range: 1,092km (679mi, 590nmi)
  • Service ceiling: 4,420m (14,500ft)
  • g limits: +6 -3
  • Rate of climb: 5.6m/s (1,100ft/min)
  • Wing loading: 54kg/m2 (11lb/sqft) [citation needed]
  • Take-off run: 140m (459ft)
  • Landing run: 120m (394ft)

Avionics

Icom IC-A-200 radio AvMap EKP-IV colour GPS optional Garmin suite

See also

Aircraft of comparable role, configuration, and era