Airbus Helicopters H155 vs Airbus Helicopters H160 vs Airbus Helicopters H175 vs Bell 525 Relentless vs Leonardo Aw139
All five are twin‑engine, IFR-capable medium helicopters, but they span the light‑medium to super‑medium class. The Airbus H155 is the lightest option here, typically configured for about 12 passengers, with generally the shortest range of the group; it’s often chosen for corporate, EMS, and short‑to‑mid offshore sectors. The Airbus H160 is a newer-generation medium helicopter, usually seating around 12, offering a step up in range and efficiency versus older light‑medium types, aiming at longer legs with lower noise and fuel burn. The Leonardo AW139 sits in the core medium category, commonly arranged for 12–15 passengers, with solid mid-to-long range that has made it a workhorse for EMS, SAR, and offshore transport. The Airbus H175 moves into the super‑medium class, typically carrying about 16–18 passengers and offering longer offshore-oriented range than the H155/H160/AW139. Bell’s 525 Relentless also targets the super‑medium segment, generally accommodating roughly 16–20 passengers and designed for longer-range, higher-payload missions comparable to the H175, often emphasizing modern avionics and offshore capability.
| Spec | AIRBUS H155 | AIRBUS H160 | AIRBUS H175 | Bell 525 Relentless | AGUSTA / LEONARDO AW139 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 11.06 | — | $ 13.53 | — | $ 11.69 |
| Min Crew | 2 | 2 | 2 | 2 | 2 |
| Total Seats | 14 | 14 | 18 | 18 | 17 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Bell | Leonardo |
| Aircraft Name | H155 | H160 | H175 | 525 Relentless | AW139 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 423 | 460 | 573 | 580 | 573 |
| DOC / nm / Seat | $ 0.74 | — | $ 0.75 | — | $ 0.69 |
| Max Cabin Seats | 12 | 12 | 18 | 16 | 15 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 4012 | 3992 | 6797 | 6675 | 4701 |
| Standard Cabin Seats | 12 | 12 | 16 | 16 | 15 |
| Direct Operating Cost | $ 1,593 | — | $ 2,016 | — | $ 1,929 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | Garmin G5000H | EFIS |
| Max Cruise Speed (ktas) | 144 | 155 | 149 | 160 | 165 |
| Base Aircraft Price (USD) | $14,800,000 | $14,000,000 | $17,900,000 | $15,000,000 | $15,900,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 | 2 |
| Total Seats | 14 | 14 | 18 | 18 | 17 |
| Configuration | Green Interior | Green Interior | — | — | — |
| Max Cabin Seats | 12 | 12 | 18 | 16 | 15 |
| Standard Cabin Seats | 12 | 12 | 16 | 16 | 15 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Dual-Channel | Yes |
| Model | Arriel 2C2 | HE Arrano | PT6A-67E | CT7-2F1 | PT6C-67C |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 3500 | 4000 | 5000 |
| Horsepower | 943 | — | 1775 | 1800 | 1679 |
| No. of Engines | 2 | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 332 | — | — | 641 | 414 |
| Dimensions | |||||
| Length (ft) | 46.9 | 39.4 | 59.2 | 61.58 | 54.7 |
| Overall Height (ft) | 14.3 | 13.1 | 17.5 | 18.18 | 16.4 |
| Rotor Diameter (ft) | 41.1 | 45.2 | 48.5 | 54.5 | 54.7 |
| Cabin Volume (cu. ft) | 235.2 | — | 423.8 | — | 282 |
| Baggage Volume Ext. (cu. ft) | 88.3 | — | 81.9 | 128 | 120 |
| Width (ft) | — | — | — | 25.77 | — |
| Cabin Width (ft) | — | — | — | 7.58 | — |
| Cabin Height (ft) | — | — | — | 4.5 | — |
| Cabin Length (ft) | — | — | — | 15.5 | — |