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 |