The A-22 is a non-aerobatic two seat ultralight aircraft designed for recreational flying and primary training in daytime VFR flight from grass or hard runways. It is a metal air-framed high-wing strut-braced monoplane with side-by-side seating and extensive cockpit glazing. The fixed tricycle landing gear has hydraulic brakes and a steerable nose wheel linked to the rudder pedals. The standard power unit is a 100 bhp Rotax 912ULS driving a ground adjustable 3-blade composite propeller. Two wing-tanks give a total fuel capacity of 92 litres. Standard A22 aircraft are fitted with a Rotax FLYdat digital engine instrument pack. Ensure you are fully familiar with the FLYdat operation before you fly this aircraft – see section 10 of this manual.
1.1 Airworthiness standards
Australia – RAA Type Accepted both as factory built and 51% kit
Germany – BFU-95 Type Certificate number 61176
UK – BCAR Section S - CAA Airworthiness Approval Note (AAN) PFA-317-432
1.2 Controls
Single centre stick (option: twin ‘Y’ handles) - elevator & flaperons
Dual rudder pedals
Central flap lever in cockpit roof – 2 positions, 10and 20
Dual side throttles
Central cold start choke control
Manual pitch trim (option: electric pitch trim)
Brake lever on control stick – hydraulic discs on main-wheels, central parking brake lock Right and left fuel taps for wing tanks
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