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Aerospace ailerons Air Force Airbus AlliedSignal aspect ratio Aviation avionics baggage compartment brakes cabin certification climb at S/L cockpit Conventional and manual CURRENT VERSIONS DaimlerChrysler Aerospace delivery DESIGN FEATURES DIMENSIONS door dual Embraer engine EXTERNAL flaps flat-four flight deck FLYING CONTROLS ft)/min Fuel capacity fuselage Height overall hydraulic Ib/sq ft Imp gallons Jane's kg/kW km/h LANDING GEAR leading-edge Length overall litres Lockheed Martin mainwheels Max cruising speed max fuel Max level speed Max power loading Max rate Max T-O weight Max width Max wing loading miles nosewheel operating optional passengers POWER PLANT production PROGRAMME propeller prototype radar rate of climb rear retractable Rotax rotor rudder seats Service ceiling Socata TB sq ft Stalling speed standard T-O run tailplane tanks Thomson-CSF tricycle type turbofans turboprop two-seat ultralight UPDATED weight Max WEIGHTS AND LOADINGS Wing aspect ratio wing loading Wing span