Helicopter Specifications & Performance
| Fuselage Dimensions | AGUSTA/WESTLAND A109A |
|---|---|
| Length (ft): | 35.1 |
| Height (ft): | 10.8 |
| Width (ft): | 9.5 |
| Typical Configuration | |
| Crew: | 1 |
| Passengers: | 7 |
| Fuel Capacity | |
| Standard (lbs): | 978 |
| Standard (gal): | 146 |
| Optional (lbs): | 151 |
| Optional (gal): | 40 |
| Weight | |
| Max. Takeoff (lbs): | 5,730 |
| Empty Operating Weight (EOW): | 2,612 |
| Speed Knots | |
| Normal Cruise TAS: | 126 |
| Vmo (Max Op) IAS: | 142 |
| IFR Certification: | |
| (IFR): | 1 Pilot |
| Climb | |
| Normal (fpm): | 1,480 |
| Engine Out (fpm): | |
| Ceiling (ft): | 1,500 |
| (HOGE) Out of Ground Effect: | 4,900 |
| (HIGE) In Ground Effect: | 7,900 |
| Takeoff Performance | |
| SL ISA BFL: | 0 |
| 5000′ +20C BFL: | 0 |
| Range (Nautical Miles) | |
| Tanks Full (nm): | 332 |
| Seats Full (nm): | 332 |
| Engines | |
| Number of: | 2 |
| Model(s): | 250-C20B |
| 250-C20R | |
| Thrust (lbs per Engine): | 0 |
| Shaft (hp per Engine): | 450 |
| Common TBO Hours: | 3,500 |