Designed by Max Braendli, the BX-2 Cherry two-seat monoplane (first flown 1982) has detachable wings and elevator.
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
All Aero 