Bell 47G
Overview
The Bell 47G is a helicopter aircraft manufactured by Bell, with the profile centered on its civil helicopter role. It first flew in 1945-12 and entered service in 1953. Production is recorded as ending in 1974. The listed configuration provides for a crew of 1 and passenger capacity of 3. Power is provided by 1 Lycoming TVO-435 series (200-280hp) engine. Recorded dimensions include length 31 ft 7 in, wingspan 37 ft 2 in, height 9 ft 4 in. Maximum takeoff weight is listed as 2950. Listed performance includes cruise speed 78 mph kt, maximum speed 90 kt, range 215 nautical miles, service ceiling 11000 ft. Its ICAO type designator is B47G. Figures shown here describe the listed type or configuration and may vary by sub-variant, certification basis, or operator fit.
Quick Facts
Specifications
| ICAO Type Code | B47G |
|---|---|
| Military Designation | H-13 Sioux |
| First Flight | Dec 1945 |
| Introduction Date | 1953 |
| Crew | 1 |
| Passenger Capacity | 3 |
| Length | 31 ft 7 in |
| Wingspan / Rotor Diameter | 37 ft 2 in |
| Height | 9 ft 4 in |
| Empty Weight | 1893 lb |
| Max Takeoff Weight | 2950 lb |
| Cruise Speed | 78 mph |
| Max Speed | 90 kt |
| Range | 215 nm |
| Service Ceiling | 11000 ft |
| Engine Manufacturer | Lycoming |
| Engine Model | TVO-435 series (200-280hp) |
| Engine Count | 1 |
Data verification status: Verified
Source: Airliners.net - Bell 47