Airbus Helicopters H155 vs Leonardo Aw109 Grand New vs Leonardo Sh09
In category, the Airbus Helicopters H155 is a medium twin-engine helicopter typically positioned for offshore support, EMS, and high-end corporate transport, offering more cabin volume and payload than light twins. The Leonardo AW109 GrandNew is a light twin-engine helicopter optimized for speed and executive missions, with a smaller cabin and generally lower operating weight than the H155. The “Leonardo SH09” is not a recognized, current Leonardo helicopter model designation in mainstream civil product lines; if you meant the Swiss Helicopter/Helvetic SH09 (often referred to as a light single), it would sit in a lighter category than both the H155 and AW109. On range, the H155 generally offers the longest practical range of the three due to larger fuel capacity and medium-class performance, commonly in the mid-hundreds of nautical miles depending on configuration. The AW109 GrandNew offers strong range for a light twin, typically somewhat less than the H155 but competitive for executive point-to-point flying. A light single in the SH09 class would typically have a shorter range than both twins, varying widely with fuel and payload. On passenger capacity, the H155 usually seats more passengers in a spacious layout (often around 8–13 depending on mission), the AW109 GrandNew typically carries fewer (commonly 6–8), and an SH09-class light single generally carries the least (often around 5–6).
| Spec | AIRBUS H155 | AGUSTA / LEONARDO AW109 Grand New | AGUSTA / LEONARDO SH09 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 11.06 | $ 7.31 | $4.48 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 14 | 8 | 8 |
| Flight Rules | IFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Leonardo | Leonardo |
| Aircraft Name | H155 | AW109 Grand New | SH09 |
| Certification | FAA / EASA | FAA / EASA | In-Development |
| Max Range (nm) | 423 | 464 | 430 |
| DOC / nm / Seat | $ 0.74 | $ 0.91 | $0.56 |
| Max Cabin Seats | 12 | 6 | 6 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4012 | — | — |
| Standard Cabin Seats | 12 | 6 | 6 |
| Direct Operating Cost | $ 1,593 | $ 1,140 | $627 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 144 | 156 | 140 |
| Base Aircraft Price (USD) | $14,800,000 | $ 7,800,000 | $3,500,000 |
| Max Passengers | — | — | 7 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 14 | 8 | 8 |
| Configuration | Green Interior | — | — |
| Max Cabin Seats | 12 | 6 | — |
| Standard Cabin Seats | 12 | 6 | 6 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2C2 | PW207C | HTS 900 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 5500 |
| Horsepower | 943 | 735 | 1020 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 332 | 152 | — |
| Dimensions | |||
| Length (ft) | 46.9 | 42.5 | — |
| Overall Height (ft) | 14.3 | 11.5 | — |
| Rotor Diameter (ft) | 41.1 | 35.5 | — |
| Cabin Volume (cu. ft) | 235.2 | — | — |
| Baggage Volume Ext. (cu. ft) | 88.3 | — | — |