Robin / Alpha Aviation / Apex R 2100, R 2112, R 2160, Alpha
Touring / Aerobatic Aircraft
The Robin R 2000 is a single-engine two-seat light touring and aerobatic aircraft produced by the French manufacturer Avions Pierre Robin, later Apex Aircraft and today by Alpha Aviation, New Zealand.
The Robin R 2100 is a development of the
Robin HR.200. The Robin R 2100 is today in production by Alpha Aviation as Alpha 120T, Alpha 160A & Alpha 160Ai.
Propulsion | 1 Piston Engine |
Engine Model | Lycoming O-320-D2A |
Engine Power | 119 kW | 160 hp |
Speed | 330 km/h | 178 kts 205 mph |
Service Ceiling | 4.570 m | 14.993 ft |
Range | 795 km | 429 NM 494 mi. |
Empty Weight | 550 kg | 1.213 lbs |
max. Takeoff Weight | 900 kg | 1.984 lbs |
Wing Span | 8,33 m | 27 ft 4 in |
Wing Area | 13,0 m² | 140 ft² |
Length | 7,10 m | 23 ft 4 in |
Height | 2,13 m | 6 ft 12 in |
First Flight | 15. Jan. 1976 |
Production Status | in production |
Developed from | Robin HR.200 |
ICAO Code | R200 |
Data for (Version) | Robin R 2160 (Alpha 160A) |
Variants | R2160, R2100, R2100A / Alpha 160A, R2160D, R2112, R2160i / Alpha 160Ai, R2120U / Alpha 120T |