Colomban MC-100 Ban-Bi
| MC-100 Ban-Bi | |
|---|---|
| Role | Amateur-built aircraft |
| National origin | France |
| Designer | Michel Colomban |
| Status | Plans available (2011) |
| Number built | 22 (1998) |
| Unit cost |
€540 (plans only, 2011) |
| Variants | Dyn'Aéro MCR01 |
The Colomban MC-100 Ban-Bi is a French amateur-built aircraft that was designed by Michel Colomban. The aircraft is supplied as plans for amateur construction with some parts and sub assemblies available.[1]
Design and development
The MC-100 features a cantilever low-wing, a two-seats-in-side-by-side configuration enclosed cockpit under a bubble canopy, a T-tail, fixed tricycle landing gear and a single engine in tractor configuration.[1] The wings are easily disassembled, allowing the whole aircraft to be loaded into a trailer in about 10 to 15 minutes.
The aircraft's 6.63 m (21.8 ft) span wing has an area of 5.2 m2 (56 sq ft). The standard engine used is the 80 hp (60 kW) Rotax 912UL four-stroke powerplant. The design is noted for its high speed on low installed power as it has a top level speed of 305 km/h (190 mph) on just 80 hp (60 kW).[1]
The aircraft is built from plans, with the wings constructed at the factory by the builder with assistance. Sub-assemblies and parts are available from both Dyn'Aéro in France and Arplast.[1]
The MC-100 was developed into a whole series of derivative designs, the Dyn'Aéro MCR01 series.[1]
Specifications (MC-100 Ban-Bi)
Data from Bayerl and Aerocrafter[1][2]
General characteristics
- Crew: one
- Capacity: one passenger
- Length: 5.49 m (18 ft 0 in)
- Wingspan: 6.63 m (21 ft 9 in)
- Wing area: 5.2 m2 (56 sq ft)
- Empty weight: 202 kg (445 lb)
- Gross weight: 450 kg (992 lb)
- Fuel capacity: 54 litres (12 imp gal; 14 US gal)
- Powerplant: 1 × Rotax 912UL four cylinder, liquid and air-cooled, four stroke aircraft engine, 60 kW (80 hp)
- Propellers: 3-bladed composite
Performance
- Maximum speed: 305 km/h (190 mph; 165 kn)
- Cruising speed: 270 km/h (168 mph; 146 kn)
- Stall speed: 87 km/h (54 mph; 47 kn)
- Range: 2,309 km; 1,247 nmi (1,435 mi)
- Service ceiling: 5,182 m (17,000 ft)
- g limits: +9/-4.5
- Rate of climb: 10.1 m/s (1,990 ft/min)
- Wing loading: 86.5 kg/m2 (17.7 lb/sq ft)
References
- ↑ 1.0 1.1 1.2 1.3 1.4 1.5 Bayerl, Robby; Martin Berkemeier; et al: World Directory of Leisure Aviation 2011-12, page 109. WDLA UK, Lancaster UK, 2011. ISSN 1368-485X
- ↑ Purdy, Don: AeroCrafter - Homebuilt Aircraft Sourcebook, Fifth Edition, page 115. BAI Communications, 15 July 1998. ISBN 0-9636409-4-1
External links
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Wikimedia Commons has media related to Colomban aircraft. |
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