Robin HR200

Key Specifications

Overview

The Robin HR200 is a French-designed, high-wing, single-engine aircraft that has established itself as a reliable platform for flight training, personal transportation, and utility operations since its introduction. Originally developed by Avions Pierre Robin, the HR200 series represents a modernized evolution of earlier Robin designs, offering improved performance and comfort compared to preceding models. The aircraft features a conventional fixed tricycle landing gear, accommodating four to five occupants depending on configuration. Its high-wing design provides excellent visibility and stability, making it particularly suitable for training operations and recreational flying. The HR200 has gained recognition for its docile handling characteristics, fuel efficiency, and relatively economical operating costs. The aircraft is primarily powered by Lycoming engines in various configurations, offering flexibility in performance requirements. Known for robust construction and straightforward maintenance, the Robin HR200 remains popular in flight schools throughout Europe and has found niche adoption in North America. The design emphasizes practical utility without compromising safety or comfort, making it an attractive option for operators seeking a versatile, honest performer rather than cutting-edge technology.

Technical Specifications

Maximum Speed: 125 knots
Cruise Speed: 110 knots
Range: 750 nautical miles
Service Ceiling: 13,500 feet
Engine: Lycoming O-235 or O-320 (depending on variant)
Maximum Takeoff Weight: 1,050 lbs (476 kg)
Empty Weight: 650 lbs (295 kg)
Fuel Capacity: 40 US gallons
Power Output: 100-160 horsepower (depending on variant)