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BX Aviation Cherry BX-2 Brändli BX-2 Cherry
Modified BX-2 TD
Thirty examples had been finished by 1998. The foldable wings allow it to be derigged for towing in 10 minutes.
 Engine: Continental, Rotax
Wing span: 7 m
Wing area: 8.5 sq.m
MAUW: 550 kg
Empty weight: 325 kg
Fuel capacity: 78 lt
Max speed: 265 kph
Cruise speed: 200 kph
Minimum speed: 80 kph
Climb rate: 3 m/s
Seats: 2
Fuel consumption: 14 lt/hr
Plan price (1998): 880 FrS
Engine: Continental A-65, 65 hp.
HP range: 65-90. Propeller: Brändli 1.60 m diameter Wing span: 23 ft / 7 m Wing area: 90 sq.ft. / 8.50 sq.m Airfoil: NACA 747 A 415 C.G. range: 19% - 32% (MAC=1240mm) Height: 6.6 ft / 2.02m Length: 17.5 ft / 5.23m Weight empty: 700 lb / 320 kg Gross: 1222 lb / 550 kg Fuel cap: 23 USG / 80 lt G load limit: +3.8 / -1.9 Range: 600 sm. Vno (max. struct. cruise): 219 km/h Vfe (max. flaps): 142 km/h Vne (never exceed): 275 km/h Va (max. maneuvering): 170 km/h Vh (horizontal): 200 km/h Vs (stall, clean): 96 km/h Vs0 (stall, flaps): 85 km/h Vy (best rate of climb): 145 km/h ROC: 680 fpm / 3m/s Enduranace: 5:00 hr Take-off dist: 1000 ft / 300 m T/O 15m: 560 m Landing dist: 500 ft. Service ceiling: 14,000 ft. Seats: 2. Landing gear: retractable nose wheel. Flaps: yes Silencer: Brändli
Noise Chapt. 6: 62.3 dB
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