Brantly B-2
Photo ©: John Allan (Photos at airliners.net)
B-2
Light Helicopter
| Crew | 1 | |
| Passengers | 1 | |
| Propulsion | 1 Piston Engine | |
| Engine Model | Lycoming IVO-360-A1A | |
| Engine Power | 134 kW | 180 hp |
| Speed | 161 km/h | 87 kts |
| Service Ceiling | 3.292 m | 10.800 ft |
| Range | 402 km | 217 nm |
| Empty Weight | 481 kg | 1.060 lbs |
| max. Takeoff Weight | 757 kg | 1.669 lbs |
| Rotor Blades (main/tail) | 3/2 | 3/2 |
| Main Rotor Diameter | 7,24 m | 23,8 ft |
| Tail Rotor Diameter | 1,29 m | 4,2 ft |
| Rotor Disc Area | 41,2 m² | 445 ft² |
| Length (Fuselage) | 6,43 m | 21,1 ft |
| Length | 8,53 m | 28,0 ft |
| Height | 2,11 m | 6,9 ft |
| First Flight | 21.02.1953 | |
| Production Status | out of production | |
| Total Production | >400 | |
| ICAO Code | BRB2 | |
| FAA TCDS | 2H2 | |
| Data for (Version) | Brantly B-2B | |
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