Airbus Helicopters H145 vs Airbus Helicopters H155 vs Airbus Helicopters H160 vs Leonardo Aw169 vs Sikorsky S 76d
The Airbus H145 and Leonardo AW169 sit in the light twin category, typically configured for about 6–9 passengers (plus crew) in corporate layouts, with practical ranges commonly around 300–450 nautical miles depending on interior, fuel options, and reserves. The H145 tends to emphasize utility and cabin access in a compact footprint, while the AW169 is often positioned slightly “upmarket” in cabin volume and speed, with similar mission radii. The Sikorsky S‑76D and Airbus H155 are medium twins aimed more squarely at offshore, corporate, and EMS roles. They usually carry roughly 8–12 passengers in executive/offshore configurations and commonly deliver about 350–500 nautical miles of range, again varying with payload and reserves. The S‑76D is known for strong cruise performance, while the H155 is valued for cabin comfort and rotorcraft IFR utility. The Airbus H160 is a newer-generation medium twin, generally accommodating about 8–12 passengers and offering competitive range, often around 400–550 nautical miles depending on configuration, with a focus on efficiency, reduced noise, and modern avionics.
| Spec | AIRBUS H145 | AIRBUS H155 | AIRBUS H160 | AGUSTA / LEONARDO AW169 | Sikorsky S-76D |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | $ 11.06 | — | $ 11.84 | $ 11.49 |
| Min Crew | 1 | 2 | 2 | 1 | 2 |
| Total Seats | 10 | 14 | 14 | 12 | 12 |
| Flight Rules | IFR | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Airbus Helicopters | Leonardo | Sikorsky |
| Aircraft Name | H145 | H155 | H160 | AW169 | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 423 | 460 | 440 | 441 |
| DOC / nm / Seat | $ 0.93 | $ 0.74 | — | $ 0.99 | $ 0.96 |
| Max Cabin Seats | 9 | 12 | 12 | 10 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 4200 | 4012 | 3992 | — | — |
| Standard Cabin Seats | 8 | 12 | 12 | 10 | 10 |
| Direct Operating Cost | $ 1,210 | $ 1,593 | — | $ 1,658 | $ 1,781 |
| Flight Deck (Base Spec) | EFIS | EFIS | EFIS | EFIS | Thales TopDeck |
| Max Cruise Speed (ktas) | 130 | 144 | 155 | 140 | 155 |
| Base Aircraft Price (USD) | $10,200,000 | $14,800,000 | $14,000,000 | $9,450,000 | $14,900,000 |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 2 | 1 | 2 |
| Total Seats | 10 | 14 | 14 | 12 | 12 |
| Configuration | Green Interior | Green Interior | Green Interior | — | — |
| Max Cabin Seats | 9 | 12 | 12 | 10 | 10 |
| Standard Cabin Seats | 8 | 12 | 12 | 10 | 10 |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | Yes |
| Model | Arriel 2E | Arriel 2C2 | HE Arrano | PW210A | PW210S |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 4000 | 4000 | 4000 | 4000 |
| Horsepower | 894 | 943 | — | 1000 | 1077 |
| No. of Engines | 2 | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | — | 332 | — | — | 296 |
| Dimensions | |||||
| Length (ft) | 44.8 | 46.9 | 39.4 | 48.1 | 52.5 |
| Overall Height (ft) | 13 | 14.3 | 13.1 | 14.8 | 14.5 |
| Rotor Diameter (ft) | 36.1 | 41.1 | 45.2 | — | 44 |
| Cabin Volume (cu. ft) | 166 | 235.2 | — | 222.5 | — |
| Baggage Volume Ext. (cu. ft) | 46.8 | 88.3 | — | 49.5 | — |