Mudry CAP 20
| Mudry CAP 20 | |
|---|---|
 Mudry CAP 20 |
|
| Type: | Aerobatic plane |
| Design country: | |
| Manufacturer: | |
| First flight: |
July 1969 |
| Number of pieces: |
9+ |
The Mudry CAP 20 was a single-seat aerobatic aircraft manufactured by Apex Group .
history
The prototype took to the skies for the first time in July 1969. The next 8 machines had an AVCO-LYcoming-AIO-360-B1B engine with an output of 149 kW (202 PS). The successor model, the Mudry CAP 20 L , was modified and had a lighter body. In January 1976 the Mudry CAP 20 L-180 model was equipped with a 134 kW (182 PS) AEIO-360 engine. The model with the designation Mudry CAP 20 LS-200 with a 149 kW (202 PS) AIO-360-B1B engine had an adjustable propeller with a constant speed and a better ratio of engine power to total weight, which significantly improved the aerobatic properties. The roll speed was 130 ° / s.
Technical specifications
| Parameter | |
|---|---|
| crew | 1 |
| length | 6.46 m |
| span | 7.57 m |
| Max. Takeoff mass | 650 kg |
| drive | Avco Lycoming AEIO-360-B1B with an output of 202 PS (149 kW) |
| Top speed | 265 km / h at sea level |
| Max. Flight duration | 2 h |
Incidents
During the period in which this type of aircraft was in use, there has been an accident without fatalities at an air show in Oua Tom / La Foa Airfield in New Caledonia .
literature
- Susan Harris: Encyclopedia of Aircraft Technology, Models, Data. Weltbild Verlag GmbH, Augsburg 1994, ISBN 3-89350-055-3 , p. 301
Web links
Individual evidence
- ↑ Accidents with the Mudry CAP 20 , Aviation Safety Network WikiBase , accessed on January 2, 2019