Airbus Helicopters H160 vs Beechcraft Bonanza G36 vs Cessna 182 Skylane vs Sikorsky S 76d
The Airbus Helicopters H160 and Sikorsky S‑76D are twin‑engine helicopters aimed at corporate, offshore, and public‑service roles, while the Beechcraft Bonanza G36 and Cessna Skylane are single‑engine piston fixed‑wing airplanes primarily used for personal and business travel, training, and utility flying. In passenger capacity, the Bonanza G36 and Skylane typically seat about four to six people including the pilot, whereas the H160 generally carries roughly five to twelve depending on configuration, and the S‑76D commonly carries about eight to twelve with crew depending on layout. For range, the fixed‑wing airplanes generally offer longer point‑to‑point endurance for their size: the Bonanza G36 is typically around 900–1,000 nautical miles, and the Skylane often falls roughly in the 800–1,000 nautical mile range depending on version and fuel options. The helicopters trade range for vertical lift and landing flexibility: the H160 is typically on the order of 450–650 nautical miles, while the S‑76D is commonly around 400–500 nautical miles, both varying with payload and reserves.
| Spec | AIRBUS H160 | Beechcraft Bonanza G36 | Cessna Skylane | Sikorsky S-76D |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | — | 2 |
| Min Crew | 2 | — | — | 2 |
| Total Seats | 14 | 6 | 4 | 12 |
| Flight Rules | IFR | VFR | VFR | IFR |
| Manufacturer | Airbus Helicopters | Beechcraft | Cessna | Sikorsky |
| Aircraft Name | H160 | Bonanza G36 | 182 Skylane | S-76D |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 460 | 920 | 915 | 441 |
| Max Cabin Seats | 12 | — | — | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3992 | 1050 | — | — |
| Standard Cabin Seats | 12 | 4 | — | 10 |
| Flight Deck (Base Spec) | EFIS | Garmin G1000 NXi | Garmin G1000 NXi | Thales TopDeck |
| Max Cruise Speed (ktas) | 155 | 176 | 145 | 155 |
| Base Aircraft Price (USD) | $14,000,000 | $925,000 | $530,000 | $14,900,000 |
| DOC / nm | — | $ 1.16 | $ 1.01 | $ 11.49 |
| DOC / nm / Seat | — | $ 0.19 | $ 0.25 | $ 0.96 |
| Direct Operating Cost | — | $ 204 | $ 146 | $ 1,781 |
| Cabin | ||||
| Cockpit | 2 | 2 | — | 2 |
| Min Crew | 2 | — | — | 2 |
| Total Seats | 14 | 6 | 4 | 12 |
| Configuration | Green Interior | — | — | — |
| Max Cabin Seats | 12 | — | — | 10 |
| Standard Cabin Seats | 12 | 4 | — | 10 |
| Engine | ||||
| FADEC | Yes | No | No | Yes |
| Model | HE Arrano | IO-550-B | IO-540-AB1A5 | PW210S |
| Fuel Type | JetFuel | AvGas | AvGas | JetFuel |
| TBO (hrs) | 4000 | 1700 | 2000 | 4000 |
| No. of Engines | 2 | 1 | 1 | 1 |
| TBO (yrs) | — | 12 | 12 | — |
| Horsepower | — | 300 | 245 | 1077 |
| Fuel Delivery | — | Fuel Injected | Fuel Injected | — |
| Fuel Capacity (gal) | — | 74 | 87 | 296 |
| Dimensions | ||||
| Length (ft) | 39.4 | 27.5 | 29 | 52.5 |
| Overall Height (ft) | 13.1 | 8.6 | 9.4 | 14.5 |
| Rotor Diameter (ft) | 45.2 | — | — | 44 |
| Wingspan (ft) | — | 33.5 | 36 | — |
| Cabin Width (ft) | — | 3.5 | 3.5 | — |
| Cabin Height (ft) | — | 4.2 | 4.1 | — |
| Cabin Length (ft) | — | 12.6 | 11.2 | — |
| Cabin Volume (cu. ft) | — | 100 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 32 | — |