Engineering:Tecnam P2004 Bravo

P2004
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.

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 m² (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/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

• Tecnam P92
• Cessna 162 Skycatcher