Specifications (G 115E/EG)
Data from http://www.grob-aircraft.eu/index.php/18.html
General characteristics
- Crew: Max two (typically 1 student & 1 instructor)
- Length: 7.54 m (24 ft 9 in)
- Wingspan: 10.0 m (32 ft 8 in)
- Height: 2.4 m (7 ft 10 in)
- Wing area: 12.2 m² (131.4 ft²)
- Empty weight: 690 kg (1,518 lb)
- Loaded weight: 55kg (121lbs)
- Useful load: 320kg (705lbs)
- Max. takeoff weight: 990 kg (2,183 lb)
- Powerplant: 1 × Lycoming O-360-A1B6 4-cylinder air-cooled piston engine, 139 kW (180 hp)
- Max Fuel Capacity: 143 l
Performance
- Never exceed speed: 343 km/h (185 knots, 213 mph)
- Cruise speed: 230 km/h (124 kn, 143 mph)
- Stall speed: 96km/h (52 Kn, 60 mph)
- Range: 1,150 km (620 nm, 710 miles)
- Service ceiling: 3,050 m (10,000 ft)
- Rate of climb: 5.3 m/s (1050 ft/min)
- Wing loading: 81.1 kg/m² (16.6 lb/ft²)
- Power/mass: 5.5 kg/hp (12.1 lbs/hp)
- g limits +6.0/-3.0g
Read more about this topic: Grob G 115