Airbus Helicopters H125 vs Airbus Helicopters H130 vs Airbus Helicopters H135 vs Airbus Helicopters H145 vs Sikorsky S 76d
The Airbus H125 and H130 are single‑engine light helicopters. The H125 is typically configured for about five to six passengers and is valued for utility work; its range is roughly in the 330–360 nautical mile class depending on fit. The H130 is a quieter, tourism‑oriented single with a wider cabin; it commonly carries about six to seven passengers and offers a similar overall range, generally around the mid‑300 nautical mile class. The Airbus H135 and H145 are twin‑engine light helicopters suited to EMS, police, and corporate missions. The H135 usually seats about five to six passengers in a corporate layout (more in utility/EMS) and tends to offer around 330–350 nautical miles of range. The larger H145 typically carries about seven to eight passengers and has range broadly in the mid‑300 nautical mile class. The Sikorsky S‑76D is a twin‑engine medium helicopter aimed at offshore and executive transport. It commonly seats eight passengers and generally provides a longer range than the light twins, often around the 400+ nautical mile class.
| Spec | AIRBUS H125 | AIRBUS H130 | AIRBUS H135 | AIRBUS H145 | Sikorsky S-76D |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 3 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 6.33 | $ 9.31 | $ 11.49 |
| Min Crew | 1 | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 7 | 9 | 10 | 12 |
| Flight Rules | VFR | VFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Sikorsky |
| Aircraft Name | H125 | H130 | H135 | H145 | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 333 | 342 | 352 | 441 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.79 | $ 0.93 | $ 0.96 |
| Max Cabin Seats | 5 | 5 | 7 | 9 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | 3124 | 4200 | — |
| Standard Cabin Seats | 4 | 4 | 7 | 8 | 10 |
| Direct Operating Cost | $ 627 | $ 640 | $ 861 | $ 1,210 | $ 1,781 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | Helionix | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 136 | 128 | 136 | 130 | 155 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $6,150,000 | $10,200,000 | $14,900,000 |
| Cabin | |||||
| Cockpit | 2 | 3 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 7 | 9 | 10 | 12 |
| Max Cabin Seats | 5 | 5 | 7 | 9 | 10 |
| Standard Cabin Seats | 4 | 4 | 7 | 8 | 10 |
| Configuration | — | — | Green Interior | Green Interior | — |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2D | Arriel 2D | Arrius 2B2+ | Arriel 2E | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 5000 | 4000 | 4000 | 4000 |
| Horsepower | 847 | 952 | 660 | 894 | 1077 |
| No. of Engines | 1 | 1 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 143 | 143 | — | — | 296 |
| Dimensions | |||||
| Length (ft) | 42.5 | 41.5 | 33.5 | 44.8 | 52.5 |
| Overall Height (ft) | 10 | 11.1 | 12.6 | 13 | 14.5 |
| Rotor Diameter (ft) | 36.1 | 35.1 | 34 | 36.1 | 44 |
| Cabin Volume (cu. ft) | — | — | 173 | 166 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 46.8 | — |