Robin HR.100
| Avions Pierre Robin HR.100 | |
|---|---|
.jpg) Robin HR.100 / 210 |
|
| Type: | light sport aircraft and touring aircraft |
| Design country: | |
| Manufacturer: | |
| First flight: |
April 1969 |
| Production time: |
1970-1976 |
| Number of pieces: |
178 |
The Avions Pierre Robin HR.100 is a light sport and touring aircraft for four people.
variants
The first version of this machine, named HR.100 / 180 , had an Avco Lycoming O-360 engine with an output of 132 kW (180 hp). The second series HR.100 / 200 had an IO-360 engine with 147 kW (200 PS). The HR.100 / 320/4 + 2 , a touring aircraft for six people, was only produced as a prototype. The next expansion stage of this model was the HR.100 / 210 with retractable landing gear and Continental engine. The next expansion stage, the HR.100 / 285 , had a Tiara-6-285B engine with 210 kW (285 hp). As a further model in this series, the HR.100 / 250TR had an Avco Lycoming IO-540 engine with 184 kW (250 PS).
Incidents
There have been a total of 19 accidents with 10 deaths with this aircraft type.
Technical specifications
| Data | Parameter |
|---|---|
| crew | 1 + 3 |
| length | 7.59 m |
| span | 9.08 m |
| Max. Takeoff mass | 1,400 kg |
| drive | a Teledyne Continental Tiara 6-285 B; 210 kW (285 hp) |
| Top speed | 325 km / h at sea level |
| Range | 2,100 km |
literature
- Susan Harris Encyclopedia of Aircraft Technology, Models, Data. Weltbild Verlag GmbH, Augsburg 1994, p. 287, ISBN 3-89350-055-3
Web links
Individual evidence
- ↑ Robin HR.100. flugzeuginfo.net, accessed February 2, 2020 .
- ↑ Accidents with Robin HR.100 , Aviation Safety Network (English), accessed on December 27, 2018