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 |