|
Twin Engine Helicopter B222 |
 |
 |
 |
 
The Bell222 will carry 6 sets of Golfbags and 6 pieces of small carry on sports bags (not cabin cases) or 6 medium sized cases dimensions 26:18:10
A luggage delivery services is available by road €200
The Bell 222 is a twin-engined max. 8-seat light utility helicopter produced by the
US-American manufacturer Bell Helicopter Textron.
| Crew |
1 / 2 |
| Passengers |
6 - 7, max. 9 |
| Propulsion |
2 Turboshaft Engines |
| Engine Model |
Lycoming LTS-101-650C-2 |
| Engine Power (each) |
503 kW |
675 shp |
| Speed |
265 km/h |
143 kts
165 mph |
| Service Ceiling |
4.816 m |
15.800 ft |
| Range |
650 km |
351 NM
404 mi. |
| Empty Weight |
2.204 kg |
4.859 lbs |
| max. Takeoff Weight |
3.650 kg |
8.047 lbs |
| Rotor Blades (main/tail) |
2/2 |
2/2 |
| Main Rotor Diameter |
12,12 m |
39,8 ft |
| Tail Rotor Diameter |
1,98 m |
6,5 ft |
| Rotor Disc Area |
115,4 m² |
1242 ft² |
| Length (Fuselage) |
12,85 m |
42,2 ft |
| Length |
15,10 m |
49,5 ft |
| Height |
3,51 m |
11,5 ft |
| First Flight |
13.08.1974 |
| Production Status |
out of production |
| Production Range |
1980-1991 |
| Total Production |
184 |
| ICAO Code |
B222 |
| FAA TCDS |
H9SW |
| Data for (Version) |
Bell 222 |
| Variants |
222, 222B, 222U |
|
