Airbus Helicopters H225 vs Bell 525 Relentless vs Leonardo Aw189 vs Leonardo Aw609 Tiltrotor vs Sikorsky S 92
Airbus Helicopters’ H225 and Sikorsky’s S‑92 sit in the heavy/large medium twin category used widely for offshore transport and SAR. Both typically carry around 19 passengers in high-density seating (with room for fewer in more spacious layouts) and offer long, practical offshore ranges on the order of roughly 450–600 nautical miles depending on reserves, payload, and configuration. Bell’s 525 Relentless is a modern “super‑medium” twin aimed at similar missions, generally in the 16–19 passenger class, with comparable offshore reach often cited around the 500 nautical mile neighborhood. Leonardo’s AW189 is a large medium twin, usually configured for about 16–19 passengers, and delivers solid offshore range broadly similar to the 525, commonly in the ~450–500 nautical mile class. Leonardo’s AW609 is different: it’s a tiltrotor rather than a conventional helicopter, typically carrying about 6–9 passengers, but trading cabin capacity for much higher cruise speed and longer point‑to‑point range, often roughly 700 nautical miles or more in mission-dependent planning.
| Spec | AIRBUS H225 | Bell 525 Relentless | AGUSTA / LEONARDO AW189 | AGUSTA / LEONARDO AW609 Tiltrotor | Sikorsky S-92 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | — | 2 |
| DOC / nm | $ 20.87 | — | $ 15.57 | — | $ 19.79 |
| Min Crew | 2 | 2 | 1 | — | 2 |
| Total Seats | 21 | 18 | 21 | — | 21 |
| Flight Rules | IFR | IFR | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Leonardo | Sikorsky |
| Aircraft Name | H225 | 525 Relentless | AW189 | AW609 Tiltrotor | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | — | FAA / EASA |
| Max Range (nm) | 454 | 580 | 651 | — | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.74 | — | $ 0.94 |
| Max Cabin Seats | 28 | 16 | 19 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | — | Un-Verified |
| Useful Load (lbs) | 11929 | 6675 | — | — | 7417 |
| Standard Cabin Seats | 19 | 16 | 19 | — | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 2,413 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | EFIS | — | EFIS |
| Max Cruise Speed (ktas) | 142 | 160 | 155 | — | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $2,413,000 | $20,000,000 | $30,650,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | — | 2 |
| Min Crew | 2 | 2 | 1 | — | 2 |
| Total Seats | 21 | 18 | 21 | — | 21 |
| Max Cabin Seats | 28 | 16 | 19 | — | 19 |
| Standard Cabin Seats | 19 | 16 | 19 | — | 19 |
| Engine | |||||
| FADEC | Yes | Dual-Channel | Yes | — | Yes |
| Model | Makila 2A1 | CT7-2F1 | CT7-2E1 | — | CT7-8A |
| Fuel Type | JetFuel | JetFuel | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 4000 | 4000 | — | 4000 |
| Horsepower | 2100 | 1800 | 1983 | — | 2520 |
| No. of Engines | 2 | 2 | 2 | — | 1 |
| Fuel Capacity (gal) | 684 | 641 | — | — | 760 |
| Dimensions | |||||
| Length (ft) | 63.4 | 61.58 | 57.8 | — | — |
| Overall Height (ft) | 16.3 | 18.18 | 16.6 | — | 17.8 |
| Rotor Diameter (ft) | 53.2 | 54.5 | 48 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 395 | — | 775 |
| Width (ft) | — | 25.77 | — | — | — |
| Cabin Width (ft) | — | 7.58 | — | — | — |
| Cabin Height (ft) | — | 4.5 | — | — | — |
| Cabin Length (ft) | — | 15.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | — | 128 | 85 | — | 140 |