Show photogallery 4

UL aircraft S-WING S4 BTA TANGO

Moravskoslezký
20 000 EUR

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

Advertisement type:
Offer
Manufacturer:
S-WING
Type:
S4 BTA TANGO
Date of manufacture:
1998
MTOW:
up to 450 kg
Airframe HOBBS:
1146
Engine HOBBS:
1146
Propeller HOBBS:
1146
Engine:
Rotax 912 UL
Fuel tank capacity:
2 x 30l
Propeller:
ground adjustable
Flaps:
mechanic
Cruise speed:
175
Never exceed speed (Vne):
195
Landing gear:
fidex
COM radio:
8,33kHz
Transponder (XPDR):
N/A
ELT:
No
Rescue system:
No
Instruments:
Speedometer [km/h] , altimeter [ft;hPa], variometer [m/s], relative transverse inclinometer, Flydat Rotax mag. compass, fuel pressure gauge, fuel gauges L, P tank Radio ICOM A210E (8.33 kHz)
Owners count:
1
Other equipment:
aircraft flight log book, engine log book, beacon, fuel valve, hydraulic brakes, heating
logo footer
Marketing: Michal Drásal
Technology and advertising: Vít Jirka
E: aerohangar@aerohangar.cz
aerohangar