Tecnam P2004

The Tecnam P2004 is a high-wing, light aircraft built by the Tecnam aircraft company. It is similar to the Tecnam P92 Echo Super, but with a cantilevered wing in place of the P92's strut-braced wing.

External links

* [http://www.tecnam.com/ing/ Company web site (English)]
* [http://www.tecnamaircraft.com/ USA web site]

pecifications (P2004 Bravo)

aircraft specifications
plane or copter?=plane
jet or prop?=prop
ref=http://www.tecnam.com/ing/p_2004Bravo.cfm
crew=one, pilot
capacity=one passenger
payload main=
payload alt=
length main= 6.61 m
length alt= 21 ft 8 in
span main= 8.40 m
span alt= 27 ft 6 in
height main= 2.60 m
height alt= 8 ft 6 in
area main= 11 m2
area alt= 118.4 ft2
airfoil=
empty weight main= 331 kg
empty weight alt= 730 lbs
loaded weight main=
loaded weight alt=
useful load main= 269 kg
useful load alt= 590 lbs
max takeoff weight main= 600 kg
max takeoff weight alt= 1,320 lbs
more general=
engine (prop)= Rotax 912ULS
type of prop=
number of props=1
power main= 100 hp
power alt= 73.5 kW
power original=
max speed main= 222 km/h at sea-level
max speed alt= 120 kts
cruise speed main= 215 km/h
cruise speed alt= 116 kts
stall speed main= 64 km/h
stall speed alt= 34.5 kts
never exceed speed main= 290 km/h
never exceed speed alt= 156 kts
range main=
range alt=
ceiling main= 4000 m
ceiling alt= 13110 ft
climb rate main= 366 m/min
climb rate alt= 1,200 ft/min
loading main= 54 kg/m2
loading alt= 11.15 lbs/ft2
thrust/weight=
power/mass main=
power/mass alt=
more performance=
* Take off run: 140 m (460 ft)
* Landing distance: 120 m (394 ft)
armament=
avionics=

ee also

aircontent
related=

similar aircraft= Tecnam P92

sequence=

lists=

see also=