Tecnam P2004 Bravo

P2004

Role	Two-seat ultralight monoplane Type of aircraft
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.^[1]

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)
Max takeoff weight: 600 kg (1,323 lb)
Max useful weight: 269 kg (593 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) ^{[citation needed]}
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

References

Wikimedia Commons has media related to Tecnam P2004 Bravo.

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