P2004 Bravo

The P2004 Bravo is a cantilevered high wing, twin side by side seat airplane. The P2004 Bravo features a refined aerodynamic with a tapered cantilevered wing. Laminar airfoils, large slotted flaps with up-turned wing tips lead, together with a streamlined fuselage, to a high performance airplane with increased cruise speed and range. The planes outstanding performance and flying qualities together with low operating costs, easy piloting and maintenance, make of this aircraft an excellent solution for the flying-schools and training activity, and also for many other missions as touring, territory surveillance, patrol, etc.

P2004 Bravo Specifications
DIMENSIONS	ft	m	ENGINE
Wing Span:	27.5 ft	8.40 m	Engine:	Rotax 912ULS
Length over-all:	21.7 ft	6.61m	Power max:	100 Hp @ 5800 rpm
Height over-all:	8.5 ft	2.60 m	Reduction:	2.4286 : 1
Width cabin:	45"	1.15 m	Propeller:	GT Tonini
Wing area:	118.4 sq ft	11.0 m²	Fuel:	Leaded, Unleaded or AvGas
Wing Dihedral:	1.5°	1.5º	Tanks:	100 Lt (2 x 50) 26.4 US Gal
Tailplane span:	9.5 ft	2.9 m
Wheeltrack:	6.1 ft	1.85 m
Wheel tyres:	5.00-5	5.00-5

PERFORMANCES		WEIGHT	kg
Max Speed s/l:	130 kts	MTO design weight:	600 kg
Cruising Speed 75% (19 litres/hour):	115 kts	MTOW:	600 kg (LSA)
Rate of Climb @ s/l:	1200 ft/min	Average empty weight:	340 kg
Stalling speed (flap):	34.5 kts	Load ultimate factor:	(+6 / -3)
Service Ceiling:	14000 ft
Take off run:	140m
Landing run:	121m
VNE:	138 kts