Specifications (CH 701)
Data from Jane's All The World's Aircraft 1993-94 and Zenith Aircraft
General characteristics
- Crew: 2
- Length: 20 ft 11 in (6.38 m)
- Wingspan: 27 ft 0 in (8.23 m)
- Height: 8 ft 7 in (2.62 m)
- Wing area: 122.0 sq ft (11.33 m2)
- Aspect ratio: 5.98:1
- Empty weight: 580 lb (263 kg)
- Max takeoff weight: 1,100 lb (499 kg)
- Fuel capacity: 20 US Gal (76 L)
- Powerplant: 1 × Rotax 912 four-cylinder liquid cooled piston engine, 80 hp (60 kW)
Performance
- Maximum speed: 85 mph (137 km/h; 74 kn) at sea level
- Cruise speed: 80 mph (70 kn; 129 km/h)
- Stall speed: 30 mph (26 kn; 48 km/h)
- Never exceed speed: 110 mph (96 kn; 177 km/h)
- Range: 372 mi (323 nmi; 599 km) with standard fuel
- Endurance: 4.6 hours
- Service ceiling: 12,000 ft (3,658 m)
- G limits: +6/-3 (ultimate)
- Rate of climb: 1,000 ft/min (5.1 m/s)
- Wing loading: 9.0 lb/sq ft (44 kg/m²)
Read more about this topic: Zenith STOL CH 701