Technical parameters - Helicopter R22 BETA II:
| Motors | Lycoming O-360 air-cooled, carburetor-equipped engine |
|---|---|
| Number of cylinders | 4 |
| Cruising speed | 1370 lb |
| Empty weight | 855 lb |
| The volume of the tank | 115 lb |
| The volume of the secondary tank | 63 lb |
| Maximum weight of passengers and baggage | 400 lb |
| Maximum speed | 118 mph (102kts) |
| Flight speed | 110 mph (96kts) |
| Range | over 200 miles |
| Range of ancillary tank | over 300 miles |
| Service ceiling | 9400 ft |
| Rate of climb (at 0 meters) | over 1,000 fpm |
| Rate of climb (at 10 000 ft) | over 600 fpm |
| Maximum operating altitude | 14,000 ft |
| The dashboard panel | standard |
| Electric system | 14V |
Scheme - Helicopter R22 BETA II:
