Airbus Helicopters H145 vs Airbus Helicopters H160 vs Leonardo Aw119kx vs Leonardo Aw169 vs Sikorsky S 76d
In category terms, the Airbus H145 and Leonardo AW119Kx sit in the light segment, with the H145 being a light twin-engine utility helicopter and the AW119Kx a light single-engine model often chosen where twin-engine redundancy isn’t required. The Airbus H160 and Leonardo AW169 are generally in the intermediate/light‑medium class, offering larger cabins and higher overall capability for corporate, EMS, and offshore-style missions. The Sikorsky S‑76D is a medium twin widely associated with executive and offshore transport, typically positioned above the H160 and AW169 in prestige and, often, operating footprint. For range, the H160 and S‑76D generally lead among these five, with the AW169 also competitive, while the H145 is solid but typically shorter-legged than the larger twins. The AW119Kx’s range can be good for a light single, but it depends heavily on payload and reserve requirements. For passenger capacity, the AW119Kx and H145 usually seat fewer, the AW169 and H160 offer more cabin volume and typically higher seating counts, and the S‑76D commonly supports the highest practical passenger loads in typical transport layouts.
| Spec | AIRBUS H145 | AIRBUS H160 | AGUSTA / LEONARDO AW119Kx | AGUSTA / LEONARDO AW169 | Sikorsky S-76D |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | — | $ 6.76 | $ 11.84 | $ 11.49 |
| Min Crew | 1 | 2 | 1 | 1 | 2 |
| Total Seats | 10 | 14 | 8 | 12 | 12 |
| Flight Rules | IFR | IFR | VFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Leonardo | Leonardo | Sikorsky |
| Aircraft Name | H145 | H160 | AW119Kx | AW169 | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 460 | 515 | 440 | 441 |
| DOC / nm / Seat | $ 0.93 | — | $ 0.84 | $ 0.99 | $ 0.96 |
| Max Cabin Seats | 9 | 12 | 6 | 10 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 3992 | — | — | — |
| Standard Cabin Seats | 8 | 12 | 6 | 10 | 10 |
| Direct Operating Cost | $ 1,210 | — | $ 885 | $ 1,658 | $ 1,781 |
| Flight Deck (Base Spec) | EFIS | EFIS | Garmin G1000H | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 130 | 155 | 131 | 140 | 155 |
| Base Aircraft Price (USD) | $10,200,000 | $14,000,000 | $3,850,000 | $9,450,000 | $14,900,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 | 1 | 2 |
| Total Seats | 10 | 14 | 8 | 12 | 12 |
| Configuration | Green Interior | Green Interior | — | — | — |
| Max Cabin Seats | 9 | 12 | 6 | 10 | 10 |
| Standard Cabin Seats | 8 | 12 | 6 | 10 | 10 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2E | HE Arrano | PT6B-37A | PW210A | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 4500 | 4000 | 4000 |
| Horsepower | 894 | — | 917 | 1000 | 1077 |
| No. of Engines | 2 | 2 | 1 | 2 | 1 |
| Fuel Capacity (gal) | — | — | 160 | — | 296 |
| Dimensions | |||||
| Length (ft) | 44.8 | 39.4 | 42.5 | 48.1 | 52.5 |
| Overall Height (ft) | 13 | 13.1 | 11.9 | 14.8 | 14.5 |
| Rotor Diameter (ft) | 36.1 | 45.2 | 35.5 | — | 44 |
| Cabin Volume (cu. ft) | 166 | — | — | 222.5 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | — | — | 49.5 | — |