X-Air

X-Air 3 Axis Microlight Landplane

The X Air is a high wing side-by-side seat, dual stick controlled monoplane. This popular aircraft has been designed with the beginner in mind, being very forgiving yet giving very lively performance especially when it comes to operating from short unprepared fields.  Experience has shown that students who learn on this aircraft find conversion to other aircraft much easier.  This is due firstly to the requirement to use the rudder pedals in order to fly the aircraft more precisely, and secondly, the extremely light control forces normally only found in very advanced more aerobatic type of aircraft.  This makes for a more relaxed and less strenuous flight even in very turbulent conditions. 

The main structure is made from aluminium alloy tube with steel fittings and covered with polyester (sailcloth) fabric. The aerofoil section is defined by the use of pre-formed aluminium ribs. The undercarriage has an independent sprung shock absorbing system on each of the large wheel assemblies. The fuselage keel member is fitted with a liquid cooled Rotax 582 engine of 64.4 hp driving a tractor propeller through a reduction drive. This 2-stroke, 2-cylinder upright engine has a dual spark ignition with magneto generator. It uses a pre-mix lubrication of 2% oil to unleaded petrol ratio.

Specifications & Performance

Wing Span 9.8 metres
Wing Area 16 sq. m.
Aspect Ratio 6.01
Mean Chord 1.63 metres
Length 5.65 metres
Dihedral Angle 1.2 degrees
Sweepback Angle 8 degrees
Washout 4 degrees
Wheel Track 1.6 metres
Empty Weight 243 kg
Maximum Take off Weight 450 kg
Minimum Occupant Weight 55 kg
Maximum Useable Fuel 48 litres
Maximum Bank Angle 60 degrees
Maximum Pitch Angle 30º down 45º Up
Maximum Flight Loads +4 / -2 g
Stall @ MAUW 30 mph
Manoeuvring Speed (VA) 75 mph
Maximum Permissible Speed (Vne) 95 mph
Minimum Sink Rate @ 38 mph 400 feet per min.
Best glide ratio @ 40 mph still air 6.7:1
Take off distance to 50 feet at MAUW 269 metres
Maximum rate of climb @ 45 mph (MAUW) 625 feet per min.
Landing distance from 50 feet @ MAUW 230 metres
Maximum Continuous Power 6800 rpm
Fuel Consumption @ 375 kg AUW & 50mph 15 ltrs per hour

 

X-Air Amphibian

X-Air 3 Axis Microlight Amphibian Floatplane

This aircraft is fitted with amphibian floats, therefore it is not confined to permanent water operations due to the fact that the undercarriage can be raised for water operations and lowered for land operations. Its specifications are similar to the land version except that it is fitted with the more powerful Jabiru 80 hp engine in order to overcome the extra weight and drag of the floats. This 4-stroke, 4 cylinder horizontally opposed engine has dual transistorised magneto spark ignition, integrated AC generator, electric starter and wet sump lubrication. It uses normal unleaded petrol but can operate on Aviation Gasoline (AVGAS) also.

Specifications & Performance (Differences)

Empty Weight 330 kg
Maximum Take off Weight 490 kg
Stall @ MAUW 34 mph
Minimum Sink Rate @ 40 mph 500 feet per min
Best glide ratio @ 45 mph still air 6:01
Take off distance to 50 feet at MAUW 300 metres
Maximum rate of climb @ 45 mph (MAUW) 500 feet per min
Landing distance from 50 feet @ MAUW 250 metres
Maximum Continuous Power 3300 rpm
Fuel Consumption @490 kg AUW & 50mph 12 litres per hour

 

Quantum 912

 Pegasus Quantum 912 Weightshift Microlight Aircraft

The Quantum is a tandem seat, flexible wing, weightshift controlled microlight.  This aircraft has proved itself to be one of the most popular weightshift aircraft in the world today, being used by the majority of schools in the UK.  It is extremely forgiving, having mild stall characteristics normally associated with lower performance craft, yet still producing fast cruise speeds and very high climb rates.   

The main structure of the rolling chassis (trike) is made from aluminium alloy tube. Rigid composite seats are fitted, which locate onto a tubular seat frame.  The rear undercarriage comprises of steel alloy tubes with elastomer suspension incorporated into aluminium alloy struts.  The nosewheel undercarriage is steerable and incorporates footrests with throttle and brake controls.  The ‘hang glider‘ type wing is made from aluminium alloy tubing and polyester (sailcloth) fabric with the aerofoil section defined by pre-formed aluminium and composite ribs.

The trike is fitted with a rear mounted Rotax 912, 80 hp engine, reduction drive and pusher propeller. This 4-stroke, 4 cylinder horizontally opposed engine has dual spark ignition, magneto, dry sump lubrication and electric starter system. The cylinder heads are liquid cooled and the barrels are ram-air-cooled. It uses normal unleaded petrol but can operate on Aviation Gasoline (AVGAS) also.

Specifications & Performance

Wing Span 10.35 metres
Wing Area 15.6 sq. m.
Aspect Ratio 6.86
Trike Length 2.82 metres
Trike Track 1.65 metres
Empty Weight 216.5 kg
Maximum Take off Weight 409 kg
Minimum Occupant Weight 55 kg
Maximum Useable Fuel 47.4 litres (34 kg)
Maximum Bank Angle 60 degrees
Maximum Pitch Angle 45 degrees
Maximum Flight Loads +4 / -0 g
Stall @ MAUW 32 mph
Manoeuvring Speed (VA) 59 mph
Maximum Permissible Speed (Vne) 90 mph
Minimum Sink Rate @ 40 mph 400 feet per min
Best glide ratio @ 40 mph still air 7.92:1
Take off distance to 50 feet at MAUW 130 metres
Maximum rate of climb @ 45 mph (MAUW) 1000 feet per min
Landing distance from 50 feet 190 metres
Fuel Consumption @ 375 kg AUW & 60mph 11 litres per hour
Maximum Continuous Power 5800 rpm

 

Acro Sport 2

Acro Sport 2 Aerobatic Light Aircraft

If you want to share the joy of open cockpit aerobatics, then the Acro Sport II is the airplane that fits your needs. Designed by the founder of the Experimental Aircraft Association of America, Paul Poberezny. With its large wheels, wide landing gear, light weight and responsive controls, the Acro II is a sport plane which is both docile on the ground and nimble in the air. Capable of sportsman and intermediate aerobatics, the Acro II is a competitive airplane that won't cramp your style. You won't be cramped either - the Acro Sport series of aircraft have cockpits designed to be comfortable for pilots up to 6'6" tall and weighing up to 240 lbs.

Specifications & Performance

Upper wing Span 21' 8"
Lower wing Span 20' 9"
Wing Area 152 sqft
Length 18' 10-1/4"
Height 79-3/4"
Power plant Lycoming 180 hp
Landing gear tread 6' 3/4 "
Empty weight 875 lbs
Gross weight 1520 lbs
Fuel capacity 20 gal
Baggage 30 lbs
Chord 43"
Stall Speed 53 mph
Cruise (180 hp Lyc) 123 mph
Top Speed 152 mph
Climb Rate 1500 feet per min