UL aircraft S-WING S4 BTA TANGO
UL aircraft S-WING S4 BTA TANGO flight 1146 h Two-seat composite strut upper biplane, canvas covered wings, fixed control surfaces MTOM 450/472.5 kg Rotax 912UL engine 1146 h flight DMP propeller, aeroelastic ground adjustable New landing gear, new fuel system, replaced door overlay + one extra Instrumentation: Speedometer [km/h] , altimeter [ft;hPa], variometer [m/s], relative transverse inclinometer, mag. compass Flydat Rotax, fuel pressure gauge, fuel gauges L, P tank Radio ICOM A210E (8,33 kHz) Equipment: 2x flash beacon from the bottom of the fuselage and above rescue system U.S.H. 120 last check 2011, not extendable manual elevator trim, manual flap control, manual ram control, adjustable seats Single hydraulic brakes - pedals Dimensions: 10.2m wingspan Length 6,29m Height 2.53m VOP span 2.6m Stall speed VS0: 64 km/h Max. speed in turbulence 160 km/h Max. speed in hor. flight 175 km/h Max. uncrossed speed 195 km/h