Airbus Helicopters H160 vs Leonardo Aw169 vs Leonardo Aw189 vs Sikorsky S 76d
In category terms, the Airbus Helicopters H160 and Sikorsky S‑76D sit primarily in the medium twin segment optimized for corporate, EMS, and offshore missions, while the Leonardo AW169 is a lighter intermediate twin aimed at similar roles with slightly smaller footprint and operating economics. The Leonardo AW189 is the clear step up into the larger “super-medium” class, designed with offshore transport and higher payload/cabin volume as priorities. On range, the AW189 generally offers the longest legs in typical offshore configurations, making it the most oriented to extended overwater sectors. The H160 is also range-competitive in the medium class, commonly exceeding what is typical for lighter intermediates. The S‑76D delivers solid medium-range capability but is usually not positioned as the longest-range option versus newer designs. The AW169 tends to have the shortest range of this group, reflecting its smaller class, though it remains suitable for many regional EMS and utility missions. For passenger capacity, the AW189 typically carries the most (often around 16–19 depending on fit), the H160 and S‑76D are commonly in the low-to-mid teens, and the AW169 is generally in the high single digits to low teens depending on layout.
| Spec | AIRBUS H160 | AGUSTA / LEONARDO AW169 | AGUSTA / LEONARDO AW189 | Sikorsky S-76D |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 14 | 12 | 21 | 12 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Leonardo | Leonardo | Sikorsky |
| Aircraft Name | H160 | AW169 | AW189 | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 440 | 651 | 441 |
| Max Cabin Seats | 12 | 10 | 19 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3992 | — | — | — |
| Standard Cabin Seats | 12 | 10 | 19 | 10 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 155 | 140 | 155 | 155 |
| Base Aircraft Price (USD) | $14,000,000 | $9,450,000 | $2,413,000 | $14,900,000 |
| DOC / nm | — | $ 11.84 | $ 15.57 | $ 11.49 |
| DOC / nm / Seat | — | $ 0.99 | $ 0.74 | $ 0.96 |
| Direct Operating Cost | — | $ 1,658 | $ 2,413 | $ 1,781 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 14 | 12 | 21 | 12 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 12 | 10 | 19 | 10 |
| Standard Cabin Seats | 12 | 10 | 19 | 10 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | HE Arrano | PW210A | CT7-2E1 | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 4000 | 4000 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Horsepower | — | 1000 | 1983 | 1077 |
| Fuel Capacity (gal) | — | — | — | 296 |
| Dimensions | ||||
| Length (ft) | 39.4 | 48.1 | 57.8 | 52.5 |
| Overall Height (ft) | 13.1 | 14.8 | 16.6 | 14.5 |
| Rotor Diameter (ft) | 45.2 | — | 48 | 44 |
| Cabin Volume (cu. ft) | — | 222.5 | 395 | — |
| Baggage Volume Ext. (cu. ft) | — | 49.5 | 85 | — |