Robin HR.200
Touring Aircraft
Photo ©: Karsten Palt
The Robin HR.200 is a single-engine two-seat light touring aircraft produced by the French manufacturer Avions Pierre Robin.
| Propulsion | 1 Piston Engine |
| Engine Model | Lycoming IO-320-D |
| Engine Power | 119 kW | 160 hp |
| Speed | 259 km/h | 140 kts
161 mph |
| Service Ceiling | 5.000 m | 16.404 ft |
| Range | 935 km | 505 NM
581 mi. |
| Empty Weight | 530 kg | 1.169 lbs |
| max. Takeoff Weight | 800 kg | 1.737 lbs |
| Wing Span | 8,33 m | 27 ft 4 in |
| Wing Area | 12,6 m² | 136 ft² |
| Length | 6,64 m | 21 ft 9 in |
| Height | 1,94 m | 6 ft 4 in |
| First Flight | 19.07.1971 |
| Production Status | out of production |
| Total Production | ca. 160 |
| ICAO Code | HR20 |
| EASA TCDS | A.086 |
| Data for (Version) | Robin HR.200/160 |
| Variants | HR.200-100, HR.200-120, HR.200-120B, HR.200-160, HR.200-100S |
