Airbus Helicopters H160 vs Airbus Helicopters H175 vs Bell 525 Relentless vs Leonardo Aw109 Grand New vs Leonardo Aw139
By category, the Airbus H160 and Leonardo AW109 Grand New sit in the light to medium-twin space, optimized for fast, efficient passenger transport and utility roles, while the Airbus H175, Leonardo AW139, and Bell 525 Relentless are larger “super-medium” class helicopters aimed at offshore, SAR, and higher-capacity missions. On range, the AW109 Grand New generally offers the shortest typical mission range among these, reflecting its lighter class. The H160 is competitive for a modern medium twin and often matches or exceeds many peers in practical cruise efficiency. The H175 and AW139, designed for longer offshore sectors, typically provide longer operational reach than the lighter machines. The Bell 525, also a super-medium, is positioned for long-range offshore profiles and can be comparable to or better than other super-mediums depending on configuration and reserves. For passenger capacity, the AW109 is the smallest, commonly configured for fewer passengers. The H160 usually carries a moderate passenger load, while the H175 and AW139 commonly seat more passengers in offshore layouts. The Bell 525 is also in the higher-capacity bracket, generally comparable to the H175/AW139 class.
| Spec | AIRBUS H160 | AIRBUS H175 | Bell 525 Relentless | AGUSTA / LEONARDO AW109 Grand New | AGUSTA / LEONARDO AW139 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 | 2 |
| Total Seats | 14 | 18 | 18 | 8 | 17 |
| Flight Rules | IFR | IFR | IFR | VFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Bell | Leonardo | Leonardo |
| Aircraft Name | H160 | H175 | 525 Relentless | AW109 Grand New | AW139 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 573 | 580 | 464 | 573 |
| Max Cabin Seats | 12 | 18 | 16 | 6 | 15 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3992 | 6797 | 6675 | — | 4701 |
| Standard Cabin Seats | 12 | 16 | 16 | 6 | 15 |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G5000H | EFIS | EFIS |
| Max Cruise Speed (ktas) | 155 | 149 | 160 | 156 | 165 |
| Base Aircraft Price (USD) | $14,000,000 | $17,900,000 | $15,000,000 | $ 7,800,000 | $15,900,000 |
| DOC / nm | — | $ 13.53 | — | $ 7.31 | $ 11.69 |
| DOC / nm / Seat | — | $ 0.75 | — | $ 0.91 | $ 0.69 |
| Direct Operating Cost | — | $ 2,016 | — | $ 1,140 | $ 1,929 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 | 2 |
| Total Seats | 14 | 18 | 18 | 8 | 17 |
| Configuration | Green Interior | — | — | — | — |
| Max Cabin Seats | 12 | 18 | 16 | 6 | 15 |
| Standard Cabin Seats | 12 | 16 | 16 | 6 | 15 |
| Engine | |||||
| FADEC | Yes | Yes | Dual-Channel | Yes | Yes |
| Model | HE Arrano | PT6A-67E | CT7-2F1 | PW207C | PT6C-67C |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 | 4000 | 4000 | 5000 |
| No. of Engines | 2 | 2 | 2 | 2 | 2 |
| Horsepower | — | 1775 | 1800 | 735 | 1679 |
| Fuel Capacity (gal) | — | — | 641 | 152 | 414 |
| Dimensions | |||||
| Length (ft) | 39.4 | 59.2 | 61.58 | 42.5 | 54.7 |
| Overall Height (ft) | 13.1 | 17.5 | 18.18 | 11.5 | 16.4 |
| Rotor Diameter (ft) | 45.2 | 48.5 | 54.5 | 35.5 | 54.7 |
| Cabin Volume (cu. ft) | — | 423.8 | — | — | 282 |
| Baggage Volume Ext. (cu. ft) | — | 81.9 | 128 | — | 120 |
| Width (ft) | — | — | 25.77 | — | — |
| Cabin Width (ft) | — | — | 7.58 | — | — |
| Cabin Height (ft) | — | — | 4.5 | — | — |
| Cabin Length (ft) | — | — | 15.5 | — | — |