Airbus Helicopters H175 vs Airbus Helicopters H215 vs Leonardo Aw139 vs Leonardo Aw169 vs Leonardo Aw189
The Airbus H175 and Leonardo AW189 sit in the super‑medium class, aimed at longer offshore and SAR-style missions. Both typically offer roughly 500–550 nautical miles of range depending on configuration and payload, and commonly seat about 16–19 passengers in high-density layouts, with executive or mission kits reducing seats. The Airbus H215 is a heavy-class helicopter (Super Puma family) optimized for lift and robustness rather than speed; it generally offers a similar or slightly greater practical range than super‑mediums in many offshore fits, and commonly carries around 19 passengers, with some layouts accommodating more, at the expense of range or comfort. The Leonardo AW139 is a medium twin, usually selected for EMS, law enforcement, and short-to-mid offshore legs; typical range is around 500–600 nautical miles with auxiliary fuel options, and seating is commonly about 12–15 passengers. The Leonardo AW169 is a light‑intermediate twin, optimized for smaller cabins and lower operating cost; it generally ranges about 400–450 nautical miles and typically carries about 6–10 passengers depending on interior and mission equipment.
| Spec | AIRBUS H175 | AIRBUS H215 | AGUSTA / LEONARDO AW139 | AGUSTA / LEONARDO AW169 | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 13.53 | $ 19.07 | $ 11.69 | $ 11.84 | $ 15.57 |
| Min Crew | 2 | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 21 | 17 | 12 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo | Leonardo | Leonardo |
| Aircraft Name | H175 | H215 | AW139 | AW169 | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 573 | 468 | 573 | 440 | 651 |
| DOC / nm / Seat | $ 0.75 | $ 0.91 | $ 0.69 | $ 0.99 | $ 0.74 |
| Max Cabin Seats | 18 | 22 | 15 | 10 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6797 | 8903 | 4701 | — | — |
| Standard Cabin Seats | 16 | 19 | 15 | 10 | 19 |
| Direct Operating Cost | $ 2,016 | $ 2,708 | $ 1,929 | $ 1,658 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 149 | 142 | 165 | 140 | 155 |
| Base Aircraft Price (USD) | $17,900,000 | $27,500,000 | $15,900,000 | $9,450,000 | $2,413,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 | 1 |
| Total Seats | 18 | 21 | 17 | 12 | 21 |
| Max Cabin Seats | 18 | 22 | 15 | 10 | 19 |
| Standard Cabin Seats | 16 | 19 | 15 | 10 | 19 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | PT6A-67E | Makila 1A1 | PT6C-67C | PW210A | CT7-2E1 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 3000 | 5000 | 4000 | 4000 |
| Horsepower | 1775 | 1820 | 1679 | 1000 | 1983 |
| No. of Engines | 2 | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | — | 540 | 414 | — | — |
| Dimensions | |||||
| Length (ft) | 59.2 | 61.4 | 54.7 | 48.1 | 57.8 |
| Overall Height (ft) | 17.5 | 16.2 | 16.4 | 14.8 | 16.6 |
| Rotor Diameter (ft) | 48.5 | 51.2 | 54.7 | — | 48 |
| Cabin Volume (cu. ft) | 423.8 | 473.9 | 282 | 222.5 | 395 |
| Baggage Volume Ext. (cu. ft) | 81.9 | — | 120 | 49.5 | 85 |