Two seat advents 3 Views Video UK

Video DE Sportster TCI

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“Info pilote” 2001

“Aviation et pilote” 1998 “Aviasport” 1997

“Today’s pilot” 2004 “Aero magazine” 2004
“Custom Planes” 2001 “Popular flying” 2000
“Plein vol” 2000 “Aviazione sportiva” 1999
“Popular flying” 1999 “Revista do ar” 1999
“Volare sport” 1999 “Popular flying” 1998
“Pilot” 1998 “Aero” 1997
“Aerokurier” 1997 “Kitplanes” 1997
“Volare sport” 1997 “Volar” 1997
Two seat advents 3 Views
Sportster TCI Option TCI
English MCR Video (9′, 21.9 Mo)
German MCR Video (9′, 21.9 Mo) Codec vidéo
The MCR Sportster is a direct evolution of Michel COLOMBANT MC 100, but with a technology that made possible the development of a kit airplane available to any pilot.

The initial design program started in early 1994, and the Sportster flew for the first time in July 1996

The MCR Sportster is a side by side two-seater airplane with incredible performance and capability. Fast and agile, the VLA was specially designed to reach top speed while providing the most enjoyable experience to pilots

The MCR Sportster is a very high performance aircraft, that can cruise as fast as 300 km/h with only a 100 hp engine, at very low cost.
Thanks to the highest level of technology available, and very light material, the Sportster has a very efficient direct control system that guarantees the same satisfaction as flying a fighter jet.

The MCR Sportster can be equipped with a choice of different power plants, but may also be fitted with other options such as :

Ballistic Recovery System parachute
Extended range wing tanks.
Toe operated Hydraulic brakes
The MCR Sportster 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.

GENERAL CARACTERISTICS

Wing span 6.63 m
Wing aera 5.20 m²
Aspect ratio 8.45
Cabin Width 1.12 m
Fuel capacity standard 80 l
Extended range fuel tanks 2 x 50 l
Empty weight (Basic version 220 kg
Equipped empty weight 260 kg
Max. Takeoff weight 490 kg
Wing loading 86 kg/m²
ENGINE OPTIONS

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 80 hp
V SPEED

VSO (stall speed landing configuration) 87 km/h
Va (Maneuvering speed) 225 km/h
Vne ( Never exceeding speed) 320 km/h
Design maneuvering speed 355 km/h
Vno (Normal Operation Speed) 260 km/h
G loading +4 /-2 g
Vfe (Flaps extended speed) 170 km/h

PERFORMANCES

Engine
R 912

R 912S

Power plant (hp)
80

100

Cruising 75%, FL 0 (km/h)
272

295

Cruising 75%, FL 80 (km/h)
292

318

Fuel consumption 75% (liters/h)
17,1

21,3

Range ,std Tanks 75% (km)
1 366

1 194

Cruising 65% FL110 (km/h)
286

312

Fuel consumption 65% (liters/h)
14,8

18,5

Range ,std Tanks 65% (km)
1 545

1 375

Takeoff roll; CS. Prop (m)
190

152

Climb rate FL 0, CS. Prop (ft/min)
1 550

1 750