Airbus Helicopters H145 vs Airbus Helicopters H160 vs Beechcraft King Air 360er vs Leonardo Aw169
Airbus Helicopters’ H145 and Leonardo’s AW169 are light twin-engine helicopters aimed at short‑to‑medium missions such as EMS, utility, and corporate shuttle. In category terms they sit below the larger, more long‑range H160. Typical passenger capacity for an H145 is about 8 to 9 in a standard corporate layout (more in high‑density configurations), while the AW169 is usually around 8 to 10, depending on cabin fit. Their practical ranges are broadly similar in the “few hundred nautical miles” class, commonly around roughly 350–450 nm with reserves depending on payload and tanks. The Airbus H160 is a medium twin with a larger cabin and higher cruise efficiency, often configured for about 10 to 12 passengers, and it generally offers a longer reach than H145/AW169, commonly on the order of roughly 450–650 nm depending on configuration. The Beechcraft King Air 360ER is not a helicopter but a pressurized twin‑turboprop fixed‑wing aircraft in the light transport/business category. It typically seats about 8 to 11 passengers and delivers the greatest range of this group, commonly around roughly 1,500+ nm, at higher cruise speeds but without vertical‑lift capability.
| Spec | AIRBUS H145 | AIRBUS H160 | Beechcraft King Air 360ER | AGUSTA / LEONARDO AW169 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 9.31 | — | $ 4.37 | $ 11.84 |
| Min Crew | 1 | 2 | 1 | 1 |
| Total Seats | 10 | 14 | 10 | 12 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Beechcraft | Leonardo |
| Aircraft Name | H145 | H160 | KingAir 350ER | AW169 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 352 | 460 | 2338 | 440 |
| DOC / nm / Seat | $ 0.93 | — | $ 0.55 | $ 0.99 |
| Max Cabin Seats | 9 | 12 | 9 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 4200 | 3992 | 6585 | — |
| Standard Cabin Seats | 8 | 12 | 8 | 10 |
| Direct Operating Cost | $ 1,210 | — | $ 1,324 | $ 1,658 |
| Flight Deck (Base Spec) | EFIS | EFIS | Rockwell Collins Pro Line Fusion | EFIS |
| Max Cruise Speed (ktas) | 130 | 155 | 303 | 140 |
| Base Aircraft Price (USD) | $10,200,000 | $14,000,000 | $8,750,000 | $9,450,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 2 | 1 | 1 |
| Total Seats | 10 | 14 | 10 | 12 |
| Configuration | Green Interior | Green Interior | — | — |
| Max Cabin Seats | 9 | 12 | 9 | 10 |
| Standard Cabin Seats | 8 | 12 | 8 | 10 |
| Lavatory | — | — | Yes (Belted Optional) | — |
| Cargo Door | — | — | Optional | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | AFT | — |
| Cabin Pressure (psi) | — | — | 6.5 | — |
| Galley / Refreshment | — | — | Refreshment Center | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Arriel 2E | HE Arrano | PT6A-60A | PW210A |
| Fuel Type | JetFuel | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 4000 | 3600 | 4000 |
| Horsepower | 894 | — | 1050 | 1000 |
| No. of Engines | 2 | 2 | 1 | 2 |
| Flat Rating | — | — | ISA + 10 | — |
| Fuel Capacity (gal) | — | — | 775 | — |
| Dimensions | ||||
| Length (ft) | 44.8 | 39.4 | 46.7 | 48.1 |
| Overall Height (ft) | 13 | 13.1 | 14.4 | 14.8 |
| Rotor Diameter (ft) | 36.1 | 45.2 | — | — |
| Cabin Volume (cu. ft) | 166 | — | — | 222.5 |
| Baggage Volume Ext. (cu. ft) | 46.8 | — | — | 49.5 |
| Wingspan (ft) | — | — | 57.9 | — |
| Cabin Width (ft) | — | — | 4.5 | — |
| Cabin Height (ft) | — | — | 4.8 | — |
| Cabin Length (ft) | — | — | 19.5 | — |
| Cabin Width - Floor (ft) | — | — | 4.1 | — |
| Cabin Length - Seating (ft) | — | — | 19.5 | — |
| Baggage Volume Int. (cu. ft) | — | — | 71 | — |