Jane's All the World's Aircraft

AgustaWestland ailerons Air Force Airbus aircraft Airlines Aviation avionics BAE Systems brakes cabin carbon fibre cent certification climb at S/L cockpit Conventional and manual CURRENT VERSIONS CUSTOMERS Czech Republic December delivery DESIGN FEATURES DIMENSIONS door engine equipment Eurocopter EXTERNAL FADEC flaps FLYING CONTROLS ft)/min Fuel capacity fuselage helicopter Honeywell hydraulic Imp gallons INTERNAL Jabiru kg/kW kg/m² km/h LANDING GEAR lb st lb/hp lb/sq ft leading-edge litres main rotor mainwheel max fuel Max level speed Max power loading Max rate Max T-O weight Max width miles MTOW Never-exceed speed VNE nosewheel operating optional passengers Paul Jackson POWER PLANT production PROGRAMME propeller prototype radar rate of climb rear Rockwell Collins Rotax Rotax 912 ULS rudder seats sq ft Stalling speed standard T-O run tailplane tailwheel tricycle type turbofans turboprop two-seat ultralight United weight Max WEIGHTS AND LOADINGS Wing span