Allegro 2007 Sport Plane LSA X-Air Australia

Information and Specifications for the Allegro 2007 Model

The Allegro 2007 Sport Aircraft is a 2-seat, high-wing monoplane designed for sport and recreational flying as well as for student pilot training.

Allegro 2000 2007 Light Sport Aircraft, LSA Sport Plane, Ultralight, floatplane

Its superbly accurate and forgiving handling characteristics, aerodynamic design and interior comfort ensure that this aircraft provides many enjoyable hours of economical flying. The composite and aluminium construction will provide, with minimal routine maintenance, many years of airborne excitement.

The Allegro is available in Australia and New Zealand as a factory built, type certified aircraft for registration on the RAA or VH registers and can be used for flight training or hire if placed on the RAA register.

Allegro 2000 2007 Light Sport Aircraft, LSA Sport Plane, Ultralight, floatplane

The Allegro 2007 is also available as an RAA and VH experimental approved kit which will consume between 250 and 400 hours of construction time, depending on the ability of the builder and the level of fitout of the aircraft.

Allegro 2007 Model Specifications
Engine options	Rotax 912 UL 80hp Rotax 912 ULS 100hp
Airframe Dimensions
Wing Span	10800 mm
Airframe Length	6100 mm
Total Height	2100 mm
Wing Area	11.4 m2
Aspect Ratio	9.5
Wing Chord-max	1200 mm
Wing Chord-min	655 mm
Airfoil Section	SM 701 Profile, tapered tip wing
Performance Details Rotax 912 80hp Engine
Max Speed VNE	118 Knots
Cruise Speed	95 Knots
Stall Speed	35 knots
Rate of Climb	985 fpm
Max Range	700 Nautical Miles with LR tanks
Take off run	150 m
Take off to clear 15m	250 m
Landing run	100 m
Landing over 15m obstacle	220 m
Aileron and rudder deflection
Aileron Up	165 mm +- 5 mm
Down	55 mm +- 5 mm
Elevator Up	79 mm +- 5 mm
Down	66 mm +- 5 mm
Rudder Right	134 mm +- 5 mm
Left	134 mm +- 5 mm
Other Data
Undercarriage tricycle	Front landing gear with suspension Rear landing gear composite
Main Wheel Track	1550 mm
Maximum Service Ceiling	4500m / 14,737 feet
Tyre Dimensions
Main wheels	14 x 4 (350 x 100)
Nose wheel	14 x 4 (350 x 100)
Tyre Pressure
Nose wheel	0.10 -0,12 Mpa (15 psi - 17 psi)
Main wheels	0.18 Mpa (26 psi)
Suspension	by flexibility in the laminated undercarriage leg
Wheel brakes	hydraulic brakes
Fuel tank volume	63 Litre Standard Tanks 103 Litre Long-Range Tanks

Weights
Maximum Take-off Weight	520 Kg (600 Kgcurrently being certified)
Empty Weight	275 Kg
Maximum useful load	245 Kg
Minimum Front-Seat Pilot Weight	55 kg
Max Weight of the Crew & Fuel	245 kg
Baggage Weight	10 kg
Standard Aircraft Equipment
Compass	Climb Indicator VSI
Fuel Gauge	Tachometer
CHT Gauge	Oil temperature gauge
Engine Operating Hours	Oil pressure gauge
Airspeed	Altimeter
Slip / Skid Gauge	Flap Position Indicator
3 Blade Woodcomp Propeller	Hydraulic Disk Brakes
Fuel pressure gauge	Choke
Map box in instrument panel	First Aid kit
Fire Extinguisher
Towing Equipment
Type	TOST S.No.
Maximum weight of towed glider	500 kg
Minimum length of tow rope	40 m
Maximum length of tow rope	60 m
Tow rope safety fuse	300 Kg

Operation Limitations
Wing flaps	Lever position	Flaps Deflection	Never Exceed Speed
Cruise position	0	-4.5 degrees	VNE 118 Knots
Take-off	1	15 degrees	VFE 60 Knots
Landing	2	48 degrees	VFE 60 Knots
Stall speeds at MTOW 520 kgs - level flight
Wing Flaps Position	Engine Power Output	IAS Knots	CAS Knots
0	Engine at idle	46 Knots	43 Knots
1	Engine at idle	40 knots	39 knots
2	Engine at idle	37 knots	35 knots

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