sailplane MCR CLUB The MCR CLUB is a direct evolution of the MCR VLA. It is also a side by side two-seater airplane, it is designed around the same fuselage with an identical cockpit and engine installation. The MCR Club appears for the first time in 1998. Its construction and design was developed in partnership with an Aviation club for its own use. The MCR CLUB has been designed around high safety standards and wings efficiency, providing both extreme flexibility and easy flight characteristics.
Equipped with a 80 HP engine and a fix pitch propeller, it is the ideal airplane for intensive use in flight school operations or aviation clubs. With a 100 HP engine and a constant speed propeller, it becomes an efficient high performance airplane combining fast cruising speed and easy handle characteristics.
The MCR CLUB can be equipped with a choice of different power plants, but may also be fitted with other options such as:
Ballistic Recovery System parachute Oil Pneumatic under carriage (for intensive use) Extended range fuel tanks in the fuselage, (particularly for school or training operations) Toe operated Hydraulic brakes Fuselage footsteps.
The MCR CLUB is available in kit form in respect with the CNSK regulation (specific kit airworthiness certificate) or in the “experimental” category, depending on the registration country.

Technische Daten:

Wing span 6,72 m
Wing area 6,45 m²
Aspect ratio 7,00
Cabin Width 1,12
Fuel capacity standard 80 l
Extended range fuel tanks 2 x 40 l
Empty weight (Basic version) 220 kg
Equipped empty weight 260 kg
Max. Takeoff weight 490 kg
Wing loading 76 kg/m²
Propeller Two, or three blades
fix pitch or constant speed
Rotax 912 Engine 80 hp
Rotax 912S Engine 100 hp
Rotax 914 turbo charged Engine 100 hp
Jabiru 2200 Engine
(still in development)
80 hp
V Speed  
VSO (stall speed landing configuration) 79 km/h
Va (Maneuvering speed) 202 km/h
Vne (Never exceeding speed) 300 km/h
Design maneuvering speed 330 km/h
Vno (Normal Operation Speed) 255 km/h
G loading +4 /-2 g
Vfe (Flaps extended speed) 165 km/h
ENGINE R 912 R 912S
Power plant hp 80 100
Cruising 75%, FL 0 (km/h) 252 274
Cruising 75%, FL 80 (km/h) 271 295
Fuel consumption 75% (liters/h) 17.1 21.3
Range ,std Tanks 75% (km) 1253 1105
Cruising 65% FL110 (km/h) 265 290
Fuel consumption 65% (liters/h) 14.8 18.5
Range ,std Tanks 65% (km) 1432 1269
Takeoff roll; CS. Prop (m) 200 160
Climb rate FL 0, CS. Prop (ft/min) 1450 1650
For further information please visit Dyn'Aéro