Airbus Helicopters H130 vs Bell 525 Relentless vs Leonardo Aw119kx vs Sikorsky S 76d
The Airbus Helicopters H130 and Leonardo AW119Kx sit in the light single‑engine category, typically used for sightseeing, training, utility, and short‑to‑medium hops. The H130 generally offers seating for about six to seven passengers (depending on configuration) and a practical range on the order of a few hundred nautical miles, while the AW119Kx is similarly a light single but often arranged for about six to seven passengers and can deliver a comparable medium range, with some missions benefiting from its cruise efficiency. The Bell 525 Relentless is a super‑medium, twin‑engine helicopter designed for longer, higher‑payload missions such as offshore transport and corporate travel. It typically carries a larger cabin load—often around a dozen-plus passengers in common layouts—and supports a substantially longer range than light singles, generally in the mid‑hundreds of nautical miles with reserves depending on configuration. The Sikorsky S‑76D is a medium twin, widely used for offshore and VIP roles, commonly seating about eight to twelve passengers and offering a medium‑to‑long range that typically exceeds light singles but is often less than a 525 in long‑range configurations.
| Spec | AIRBUS H130 | Bell 525 Relentless | AGUSTA / LEONARDO AW119Kx | Sikorsky S-76D |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| DOC / nm | $ 5.00 | — | $ 6.76 | $ 11.49 |
| Min Crew | 1 | 2 | 1 | 2 |
| Total Seats | 7 | 18 | 8 | 12 |
| Flight Rules | VFR | IFR | VFR | IFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Sikorsky |
| Aircraft Name | H130 | 525 Relentless | AW119Kx | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 333 | 580 | 515 | 441 |
| DOC / nm / Seat | $ 0.71 | — | $ 0.84 | $ 0.96 |
| Max Cabin Seats | 5 | 16 | 6 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2299 | 6675 | — | — |
| Standard Cabin Seats | 4 | 16 | 6 | 10 |
| Direct Operating Cost | $ 640 | — | $ 885 | $ 1,781 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G5000H | Garmin G1000H | Thales TopDeck |
| Max Cruise Speed (ktas) | 128 | 160 | 131 | 155 |
| Base Aircraft Price (USD) | $3,450,000 | $15,000,000 | $3,850,000 | $14,900,000 |
| Cabin | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 | 2 |
| Total Seats | 7 | 18 | 8 | 12 |
| Max Cabin Seats | 5 | 16 | 6 | 10 |
| Standard Cabin Seats | 4 | 16 | 6 | 10 |
| Engine | ||||
| FADEC | Yes | Dual-Channel | Yes | Yes |
| Model | Arriel 2D | CT7-2F1 | PT6B-37A | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 4500 | 4000 |
| Horsepower | 952 | 1800 | 917 | 1077 |
| No. of Engines | 1 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 641 | 160 | 296 |
| Dimensions | ||||
| Length (ft) | 41.5 | 61.58 | 42.5 | 52.5 |
| Overall Height (ft) | 11.1 | 18.18 | 11.9 | 14.5 |
| Rotor Diameter (ft) | 35.1 | 54.5 | 35.5 | 44 |
| Width (ft) | — | 25.77 | — | — |
| Cabin Width (ft) | — | 7.58 | — | — |
| Cabin Height (ft) | — | 4.5 | — | — |
| Cabin Length (ft) | — | 15.5 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 128 | — | — |