Brantly B-2
Light Helicopter
The Brantly B-2 is a single-engine two-seat light helicopter produced by the US-American manufacturer Brantly Helicopter Corporation, later by Brantly-Hynes Helicopter Inc. (today Brantly International).
| Propulsion | 1 Piston Engine |
| Engine Model | Lycoming IVO-360-A1A |
| Engine Power | 134 kW | 180 hp |
| max. Cruise Speed | 144 km/h | 78 kts
90 mph |
| max. Speed (vne) | 161 km/h | 87 kts
100 mph |
| Service Ceiling | 3.292 m | 10.800 ft |
| Rate of climb | 579 m/min | 1900 ft/min |
| Range | 402 km | 217 NM
250 mi. |
| Empty Weight | 481 kg | 1.060 lbs |
| max. Takeoff Weight | 757 kg | 1.669 lbs |
| Rotor Blades (main/tail) | 3/2 |
| Main Rotor Diameter | 7,24 m | 23 ft 9 in |
| Tail Rotor Diameter | 1,29 m | 4 ft 3 in |
| Rotor Disc Area | 41,2 m² | 443 ft² |
| Length (Fuselage) | 6,43 m | 21 ft 1 in |
| Length | 8,53 m | 27 ft 12 in |
| Height | 2,11 m | 6 ft 11 in |
| 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 |
| Variants | Brantly YHO-3, B-2A, B-2B |
