Airbus Helicopters H175 vs Airbus Helicopters H225 vs Bell 525 Relentless vs Leonardo Aw139 vs Leonardo Aw189
Airbus Helicopters H175 and Leonardo AW189 sit in the “super-medium” class, typically configured around 16–19 passengers, balancing cabin volume with long overwater legs; their practical mission ranges are broadly comparable, with the AW189 often advertised with slightly stronger long-range capability in offshore fit while the H175 is commonly positioned similarly for North Sea–style sectors. The Leonardo AW139 is a “medium” helicopter with a smaller cabin and usually about 12–15 passengers in offshore/commercial layouts; its range is generally shorter than the super-medium pair, though it remains highly versatile and efficient for regional and shuttle work. The Airbus Helicopters H225 is a “heavy” twin with the largest cabin of this group and commonly the highest passenger counts (often around 19+ in offshore seating), and it is typically selected when payload and cabin volume matter most; range can be competitive but is often traded against higher lift capability. The Bell 525 Relentless is a newer “super-medium” design aimed at the H175/AW189 segment, generally targeting similar passenger capacities and long-range offshore performance, with configurations and achieved ranges depending on certification status and operator fit.
| Spec | AIRBUS H175 | AIRBUS H225 | Bell 525 Relentless | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 13.53 | $ 20.87 | — | $ 11.69 | $ 15.57 |
| Min Crew | 2 | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 21 | 18 | 17 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Bell | Leonardo | Leonardo |
| Aircraft Name | H175 | H225 | 525 Relentless | AW139 | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 454 | 580 | 573 | 651 |
| DOC / nm / Seat | $ 0.75 | $ 0.99 | — | $ 0.69 | $ 0.74 |
| Max Cabin Seats | 18 | 28 | 16 | 15 | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 11929 | 6675 | 4701 | — |
| Standard Cabin Seats | 16 | 19 | 16 | 15 | 19 |
| Direct Operating Cost | $ 2,016 | $ 2,963 | — | $ 1,929 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G5000H | EFIS | EFIS |
| Max Cruise Speed (ktas) | 149 | 142 | 160 | 165 | 155 |
| Base Aircraft Price (USD) | $17,900,000 | $ 29,500,000 | $15,000,000 | $15,900,000 | $2,413,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 21 | 18 | 17 | 21 |
| Max Cabin Seats | 18 | 28 | 16 | 15 | 19 |
| Standard Cabin Seats | 16 | 19 | 16 | 15 | 19 |
| Engine | |||||
| FADEC | Yes | Yes | Dual-Channel | Yes | Yes |
| Model | PT6A-67E | Makila 2A1 | CT7-2F1 | PT6C-67C | CT7-2E1 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 3500 | 4000 | 5000 | 4000 |
| Horsepower | 1775 | 2100 | 1800 | 1679 | 1983 |
| No. of Engines | 2 | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 684 | 641 | 414 | — |
| Dimensions | |||||
| Length (ft) | 59.2 | 63.4 | 61.58 | 54.7 | 57.8 |
| Overall Height (ft) | 17.5 | 16.3 | 18.18 | 16.4 | 16.6 |
| Rotor Diameter (ft) | 48.5 | 53.2 | 54.5 | 54.7 | 48 |
| Cabin Volume (cu. ft) | 423.8 | 547 | — | 282 | 395 |
| Baggage Volume Ext. (cu. ft) | 81.9 | — | 128 | 120 | 85 |
| Width (ft) | — | — | 25.77 | — | — |
| Cabin Width (ft) | — | — | 7.58 | — | — |
| Cabin Height (ft) | — | — | 4.5 | — | — |
| Cabin Length (ft) | — | — | 15.5 | — | — |