Helicopter Specifications & Performance
| Fuselage Dimensions | BELL 205A-1 |
|---|---|
| Length (ft): | 42.3 |
| Height (ft): | 11.1 |
| Width (ft): | 9.3 |
| Typical Configuration | |
| Crew: | 1 |
| Passengers: | 14 |
| Fuel Capacity | |
| Standard (lbs): | 1,441 |
| Standard (gal): | 215 |
| Optional (lbs): | 1,206 |
| Optional (gal): | 180 |
| Weight | |
| Max. Takeoff (lbs): | 9,500 |
| Empty Operating Weight (EOW): | 5,323 |
| Speed Knots | |
| Normal Cruise TAS: | 110 |
| Vmo (Max Op) IAS: | 110 |
| IFR Certification: | |
| (IFR): | Not Specified |
| Climb | |
| Normal (fpm): | |
| Engine Out (fpm): | |
| Ceiling (ft): | 14,700 |
| (HOGE) Out of Ground Effect: | 6,000 |
| (HIGE) In Ground Effect: | 2,000 |
| Takeoff Performance | |
| SL ISA BFL: | 0 |
| 5000′ +20C BFL: | 0 |
| Range (Nautical Miles) | |
| Tanks Full (nm): | 270 |
| Seats Full (nm): | 0 |
| Engines | |
| Number of: | 1 |
| Model(s): | T5313B |
| T5317A | |
| Thrust (lbs per Engine): | T5317B |
| Shaft (hp per Engine): | T53517BCV |
| Common TBO Hours: | 0 |
| 1,400 |