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TL Ultralight TL 232 Condor

tl-232-condor


The TL Ultralight TL-232 Condor Plus is a two-seat ultralight. The TL-232 Condor Plus is a further development of the TL-132 Condor. It is a two-place ultralight airplane with seats side-by-side. The TL-232 Condor Plus is the first Czech ultralight aircraft certified also for towing of ultralight and light gliders. It is feasible to tow banners, too.

It is an ideal platform for flight training and touristic flying including long-distance flights as well. The basic version is powered by Rotax 503 engine, equipped by a two-blade wooden propeller and basic flight instrumentation only. Upon request it could be delivered with all other Rotax engines (including Rotax 912), various propellers (including electrically in-flight adjustable ones), a wide range of other instruments as for example a GPS set, fuel consumption computer etc. A rocket recovery system belongs to optional extras.

It is a two-place ultralight airplane of latest generation with seats side-by-side in roomy and comfortable cockpit. The seats are adjustable and have inclinable backrests.

The TL-232 Condor Plus is a further development of the TL-132 Condor.

 

TL-232-Con-Plus
TL 232 Condor Plus

 

TL-232 Condor Plus
Stall: 32 kt / 37 mph / 60 kmh
Cruise: 81 kt / 93 mph / 150 kmh
VNE: 97 kt / 112 mph / 180 kmh
Empty Weight: 280 kg / 617 lbs
MTOW Weight: 450 kg / 992 lbs
Climb Ratio: 800 ft/min / 4,6 m/s
Glide Ratio: 1:14

 

TL 232 Condor Plus
Engine: Rotax 912, 80 hp
Wing span: 10.60 m
Wing area: 14.84 sq.m
MAUW: 450 kg
Empty weight: 280 kg
Fuel capacity: 70 lt
Max speed: 180 kph
Cruise speed: 170 kph
Minimum speed: 65 kph
Climb rate: 5.4 m/s
Certification: Vz
Seats: 2
Fuel consumption: 11 lt/hr
Price (1998): 79 000 DM
 

 

 

 

 


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