Airbus Helicopters H125 vs Airbus Helicopters H130 vs Airbus Helicopters H145 vs Airbus Helicopters H160 vs Airbus Helicopters H215
The Airbus Helicopters H125 and H130 are light single‑engine helicopters. The H125 is typically used as a rugged utility platform with a common passenger configuration around five to six plus one pilot and a practical range on the order of about 600 km, varying with fuel tanks and load. The H130 is a quieter, comfort‑oriented light single, often arranged for about six to seven passengers plus one pilot, with a broadly similar range, commonly around 600 km. The H145 is a light twin‑engine helicopter aimed at EMS, law enforcement, and corporate missions, generally seating about seven to nine passengers (or mission equipment) with a typical range roughly in the 600–700 km class. The H160 is a newer medium twin focused on higher speed and efficiency, usually configured around eight to twelve passengers, with range commonly around 800–850 km depending on fit. The H215 is a heavy twin derived from the Super Puma family, used for offshore and transport roles, commonly carrying about 19 passengers, with range typically around 800–900 km, mission dependent.
| Spec | AIRBUS H125 | AIRBUS H130 | AIRBUS H145 | AIRBUS H160 | AIRBUS H215 |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 3 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 9.31 | — | $ 19.07 |
| Min Crew | 1 | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 7 | 10 | 14 | 21 |
| Flight Rules | VFR | VFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters |
| Aircraft Name | H125 | H130 | H145 | H160 | H215 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 333 | 352 | 460 | 468 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.93 | — | $ 0.91 |
| Max Cabin Seats | 5 | 5 | 9 | 12 | 22 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | 4200 | 3992 | 8903 |
| Standard Cabin Seats | 4 | 4 | 8 | 12 | 19 |
| Direct Operating Cost | $ 627 | $ 640 | $ 1,210 | — | $ 2,708 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | EFIS | EFIS | EFIS |
| Max Cruise Speed (ktas) | 136 | 128 | 130 | 155 | 142 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $10,200,000 | $14,000,000 | $27,500,000 |
| Cabin | |||||
| Cockpit | 2 | 3 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 7 | 10 | 14 | 21 |
| Max Cabin Seats | 5 | 5 | 9 | 12 | 22 |
| Standard Cabin Seats | 4 | 4 | 8 | 12 | 19 |
| Configuration | — | — | Green Interior | Green Interior | — |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | Arriel 2D | Arriel 2E | HE Arrano | Makila 1A1 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 5000 | 4000 | 4000 | 3000 |
| Horsepower | 847 | 952 | 894 | — | 1820 |
| No. of Engines | 1 | 1 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 143 | 143 | — | — | 540 |
| Dimensions | |||||
| Length (ft) | 42.5 | 41.5 | 44.8 | 39.4 | 61.4 |
| Overall Height (ft) | 10 | 11.1 | 13 | 13.1 | 16.2 |
| Rotor Diameter (ft) | 36.1 | 35.1 | 36.1 | 45.2 | 51.2 |
| Cabin Volume (cu. ft) | — | — | 166 | — | 473.9 |
| Baggage Volume Ext. (cu. ft) | — | — | 46.8 | — | — |