While the B23 retains similarities to the classic BRISTELL LSA, it features significant improvements. The fuselage is lengthened, and the tail is upgraded with a larger aluminum rudder. The flaps and stabilizer are redesigned for increased efficiency, while the composite main landing gear legs have been completely reworked to support higher loads than previous models. Enhanced handling characteristics also contribute to the overall flight experience. Additionally, the aircraft is equipped with a twin elevator trim tab system that helps optimize control stick forces for the pilot.
Standard equipment includes a steerable nose wheel and a BRS ballistic parachute rescue system. The B23 meets night-VFR requirements as standard and can be further upgraded for IFR certification.
With a maximum take-off weight of 750 kg and an empty weight of 450 kg, the B23 offers a useful load of 300 kg. The 120-liter fuel tank provides excellent cruising capability, and the airframe’s durable construction ensures a long operational life, making the BRISTELL B23 an ideal choice for flight training. BRISTELL B23 is also certified for flying at night under VFR conditions. Enjoy a quiet night flight in a certified airplane with a dual glass cockpit and Garmin autopilot.
The certification for BRISTELL B23 includes the luggage compartment capacity of 2x20 kg in both wings and 15 kg behind the seats. In total, you can load 55 kg of luggage into the aircraft, and you still have 250 kg of useful load left. This makes the b23 a global winner among ga aircraft.
This engine offers all the well-known advantages of the rotax 4-stroke engine series, which are complemented by additional features, such as the engine management system. The complete package presents the latest technology in the aircraft engine industry and will enhance the flying and ownership experience of pilots.
Reduce the noise of your BRISTELL B23 with easa certified exhaust silencer. Fly even when other aircraft have to stay on the ground.
Included in the equipment of the BRISTELL B23 airplane are
Wing span | 9.274 m |
Wing area | 11.75 m 2 |
Wing loading | 63.82 kg/m 2 |
Aircraft length | 6.585 m |
Aircraft height | 2.36 m |
Cabin width | 1.3 m |
All data at MTOW 750 kg
Empty weight | 450 kg |
Maximum take-off weight (MTOW) | 750 kg |
Useful load | 300 kg |
Fuel tanks capacity | 120 l |
Fuselage luggage compartment | 15 kg |
Wing luggage compartment | 2 x 20 kg |
Load factor | +4/-2g |
All data at MTOW 750 kg
Stall speed without flaps VS1 | 50 KCAS (MTOW 750 kg) |
Stall speed with flaps VS0 | 43 KCAS (MTOW 750 kg) |
Maneuvering speed VA | 98 KCAS |
Maximum flap speed VFE | 81 KCAS |
Maximum horizontal flight speed VH | 117 KTAS |
Never exceeded speed VNE | 156 KCAS |
Never exceeded speed VNE | 156 KCAS |
Best rate of climb speed Vy (flaps retracted), MTOP | 74 KIAS |
Best angle of climb speed Vx, MTOP | 62 KIAS |
Best rate of climb speed Vy (flaps 10°), MTOP | 76 KIAS |
Best rate of climb (flaps 10°), MTOP | 634 ft/min |
Take-off distance (ground roll) | 365 m/min |
Take-off distance over 15 m (50 ft) obstacle | 479 m |
Landing distance (ground roll) | 146 m |
Landing distance from 15 m (50 ft) height | 391 m |
All data at MTOW 750 kg