Tecnam P2004 Bravo
# 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.

## Specifications (P2004 Bravo)

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

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 $m^2$ (120 sq ft)
* Empty weight: 336 kg (741 lb)
* Max takeoff weight: 600 kg (1,323 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 $kg/m^2$ (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
