Airbus Helicopters H225 vs Enstrom 480b vs Leonardo Aw189 vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Airbus H225 and the Agusta/Leonardo AW189 are in the heavy/upper-medium twin-engine class, aimed at offshore transport and SAR; both typically offer the longest mission capability here, with practical ranges commonly in the roughly 450–500+ nautical mile class depending on fit, and they can carry the most people. In high-density layouts the H225 is often configured around 19 passengers, while the AW189 is commonly around 16–18, with both offering substantial cabin volume for mixed passengers/cargo. The MD Helicopters (McDonnell Douglas) 902 Explorer is a lighter twin designed more for corporate, utility, and law-enforcement roles. It generally seats about 8–10 passengers and has a shorter range than the H225/AW189, often in the ~300–350 nautical mile class. The Enstrom 480B is a light single-engine utility helicopter, best suited to shorter-range work, training, patrol, and light lift. It typically carries about 4–5 passengers and has the shortest overall range and payload capability of the group, commonly around the ~250–300 nautical mile class depending on configuration and reserves.
| Spec | AIRBUS H225 | AGUSTA / LEONARDO AW189 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 15.57 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 21 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo |
| Aircraft Name | H225 | AW189 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 0.74 |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — |
| Standard Cabin Seats | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $2,413,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 21 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 19 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | CT7-2E1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 2100 | 1983 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Dimensions | ||
| Length (ft) | 63.4 | 57.8 |
| Overall Height (ft) | 16.3 | 16.6 |
| Rotor Diameter (ft) | 53.2 | 48 |
| Cabin Volume (cu. ft) | 547 | 395 |
| Baggage Volume Ext. (cu. ft) | — | 85 |