Airbus Helicopters H160 vs Airbus Helicopters H175 vs Airbus Helicopters H215 vs Airbus Helicopters H225
The Airbus Helicopters H160 is a medium twin positioned for efficient corporate, EMS, and offshore shuttle work. It typically carries about 12 passengers and offers a moderate-to-long range for its class, roughly in the 850 km order depending on fit and reserves. The H175 steps up into the super-medium category, aimed heavily at offshore transport; it commonly seats around 16 passengers and generally provides longer legs than the H160, often around the 1,200–1,300 km class. The H215 is a heavy, long-range helicopter derived from the Super Puma family, used for utility, government, and passenger missions. It is usually configured for roughly 19 passengers and has range broadly comparable to other heavy twins, around the 1,000–1,100 km class depending on payload and tanks. The H225 is the larger, more capable heavy twin in the same family, optimized for offshore and SAR; it commonly carries about 19 passengers as well, but with higher performance and typically similar-to-better range than the H215, often around 1,100 km class, mission-equipped dependent.
| Spec | AIRBUS H160 | AIRBUS H175 | AIRBUS H215 | AIRBUS H225 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 14 | 18 | 21 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H160 | H175 | H215 | H225 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 573 | 468 | 454 |
| Max Cabin Seats | 12 | 18 | 22 | 28 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3992 | 6797 | 8903 | 11929 |
| Standard Cabin Seats | 12 | 16 | 19 | 19 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 155 | 149 | 142 | 142 |
| Base Aircraft Price (USD) | $14,000,000 | $17,900,000 | $27,500,000 | $ 29,500,000 |
| DOC / nm | — | $ 13.53 | $ 19.07 | $ 20.87 |
| DOC / nm / Seat | — | $ 0.75 | $ 0.91 | $ 0.99 |
| Direct Operating Cost | — | $ 2,016 | $ 2,708 | $ 2,963 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 14 | 18 | 21 | 21 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 12 | 18 | 22 | 28 |
| Standard Cabin Seats | 12 | 16 | 19 | 19 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | HE Arrano | PT6A-67E | Makila 1A1 | Makila 2A1 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 | 3000 | 3500 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Horsepower | — | 1775 | 1820 | 2100 |
| Fuel Capacity (gal) | — | — | 540 | 684 |
| Dimensions | ||||
| Length (ft) | 39.4 | 59.2 | 61.4 | 63.4 |
| Overall Height (ft) | 13.1 | 17.5 | 16.2 | 16.3 |
| Rotor Diameter (ft) | 45.2 | 48.5 | 51.2 | 53.2 |
| Cabin Volume (cu. ft) | — | 423.8 | 473.9 | 547 |
| Baggage Volume Ext. (cu. ft) | — | 81.9 | — | — |