Robin HR.100
Touring Aircraft

Photo ©: Karsten Palt
The Robin HR.100 is a light single engine four seat touring aircraft produced by the French manufacturer Avions Pierre Robin.
| Propulsion | 1 Piston Engine |
| Engine Model | Continental Tiara 6-285B |
| Engine Power | 213 kW | 286 hp |
| Speed | 324 km/h | 175 kts 201 mph |
| Service Ceiling | 5.700 m | 18.701 ft |
| Range | 2.130 km | 1.150 NM 1.323 mi. |
| Empty Weight | 840 kg | 1.852 lbs |
| max. Takeoff Weight | 1.400 kg | 3.086 lbs |
| Wing Span | 9,08 m | 29 ft 9 in |
| Wing Area | 15,2 m² | 164 ft² |
| Length | 7,59 m | 24 ft 11 in |
| Height | 2,71 m | 8 ft 11 in |
| First Flight | 03.06.1969 |
| Production Status | out of production |
| Production Range | 1970-1976 |
| Total Production | 178 |
| Developed from | Robin DR.253 |
| ICAO Code | HR10 |
| Data for (Version) | Robin HR.100/285TR |
| Variants | HR.100/200B Royal, HR.100/210 Safari, HR.100/250TR, HR.100/285TR Tiara |