Robin HR.100
Photo ©: Karsten Palt
HR.100
Touring Aircraft
The Robin HR.100 is a light single engine four seat touring aircraft produced by the French manufacturer Avions Pierre Robin.
| Crew | 1 | |
| Passengers | 3 | |
| 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 | 29,8 ft |
| Wing Area | 15,2 m² | 164 ft² |
| Length | 7,59 m | 24,9 ft |
| Height | 2,71 m | 8,9 ft |
| 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 | |
Remarks
The Robin HR.100 is a development of the Robin DR.253 Regent with metal wings.
| Extras | |
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