Airbus Helicopters H125 vs Airbus Helicopters H145 vs Bell 505 Jetranger X vs Leonardo Aw139 vs Sikorsky S 76d
The Airbus H125 and Bell 505 JetRanger X sit in the light single‑engine category. The H125 typically offers the longest practical range of the two and can carry more people, commonly around five to six passengers plus a pilot depending on configuration. The Bell 505 is generally shorter‑range and lower‑capacity, most often suited to about four passengers plus a pilot, emphasizing simplicity and cost efficiency. The Airbus H145 is a light twin‑engine helicopter, a step up in category for redundancy and utility. It usually delivers a moderate range and a noticeably larger cabin than the H125/505, commonly accommodating about seven to eight passengers in typical layouts. The Sikorsky S‑76D and Leonardo AW139 are medium twin‑engine helicopters aimed at corporate and offshore/utility missions. Both provide longer ranges than the lighter aircraft and higher passenger capacity. The S‑76D is often configured around eight passengers (with options higher), while the AW139 is generally the larger-capacity and often longer‑range platform, frequently arranged for about 10 to 12 passengers, with higher-density layouts possible.
| Spec | AIRBUS H125 | AIRBUS H145 | Bell 505 JetRanger X | AGUSTA / LEONARDO AW139 | Sikorsky S-76D |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 9.31 | $ 3.53 | $ 11.69 | $ 11.49 |
| Min Crew | 1 | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 10 | 5 | 17 | 12 |
| Flight Rules | VFR | IFR | VFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Bell | Leonardo | Sikorsky |
| Aircraft Name | H125 | H145 | 505 JetRanger X | AW139 | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 352 | 306 | 573 | 441 |
| DOC / nm / Seat | $ 0.77 | $ 0.93 | $ 0.71 | $ 0.69 | $ 0.96 |
| Max Cabin Seats | 5 | 9 | — | 15 | 10 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 4200 | 1500 | 4701 | — |
| Standard Cabin Seats | 4 | 8 | 3 | 15 | 10 |
| Direct Operating Cost | $ 627 | $ 1,210 | $ 441 | $ 1,929 | $ 1,781 |
| Flight Deck (Base Spec) | Garmin G500H | EFIS | Garmin G1000H | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 136 | 130 | 125 | 165 | 155 |
| Base Aircraft Price (USD) | $3,200,000 | $10,200,000 | $1,445,000 | $15,900,000 | $14,900,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 2 | 2 |
| Total Seats | 6 | 10 | 5 | 17 | 12 |
| Max Cabin Seats | 5 | 9 | — | 15 | 10 |
| Standard Cabin Seats | 4 | 8 | 3 | 15 | 10 |
| Configuration | — | Green Interior | — | — | — |
| Engine | |||||
| FADEC | Yes | Yes | Dual-Channel | Yes | Yes |
| Model | Arriel 2D | Arriel 2E | Arrius 2R | PT6C-67C | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 4000 | 5000 | 4000 |
| Horsepower | 847 | 894 | 505 | 1679 | 1077 |
| No. of Engines | 1 | 2 | 1 | 2 | 1 |
| Fuel Capacity (gal) | 143 | — | 84.85 | 414 | 296 |
| Fuel Burn (gph) | — | — | 32.3 | — | — |
| Dimensions | |||||
| Length (ft) | 42.5 | 44.8 | 42.48 | 54.7 | 52.5 |
| Overall Height (ft) | 10 | 13 | 10.65 | 16.4 | 14.5 |
| Rotor Diameter (ft) | 36.1 | 36.1 | 37 | 54.7 | 44 |
| Cabin Volume (cu. ft) | — | 166 | 137 | 282 | — |
| Baggage Volume Ext. (cu. ft) | — | 46.8 | 18 | 120 | — |
| Width (ft) | — | — | 6.51 | — | — |
| Cabin Width (ft) | — | — | 4.66 | — | — |
| Cabin Height (ft) | — | — | 2.75 | — | — |
| Cabin Length (ft) | — | — | 7.17 | — | — |