Beechcraft King Air 360 Er vs Daher Tbm 960 vs Piaggio Avanti Evo vs Sikorsky S 92
The Beechcraft King Air 360ER is a pressurized, twin‑engine turboprop business aircraft positioned for versatile regional missions. It typically offers roughly 1,500–1,800 nautical miles of range depending on payload and conditions, and commonly carries about 6–9 passengers in executive layouts. The Daher TBM 960 is a high‑performance, single‑engine turboprop optimized for speed and efficiency with fewer seats; it generally flies about 1,500–1,700 nautical miles and usually carries 4–6 passengers (up to around 6–7 with an aft seat option). The Piaggio Avanti EVO is a twin‑engine turboprop known for fast cruise and a roomy cabin relative to its class; it commonly provides about 1,400–1,800 nautical miles of range and seats about 6–9 passengers. The Sikorsky S‑92 is a twin‑engine, medium helicopter used for offshore and utility/VIP roles; compared with the fixed‑wing aircraft it has a much shorter range, typically around 500–600 nautical miles, but can carry far more people, often 12–19 passengers depending on configuration and mission.
| Spec | Daher TBM 960 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | — | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 6 | 8 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Daher TBM | Piaggio | Sikorsky |
| Aircraft Name | TBM 960 | Avanti EVO | S-92 |
| Aircraft Type | Turbo Prop | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1530 | 439 |
| DOC / nm / Seat | $ 0.56 | — | $ 0.94 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2908 | 3775 | 7417 |
| Standard Cabin Seats | 4 | 6 | 19 |
| Direct Operating Cost | $ 744 | — | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 330 | 400 | 155 |
| Base Aircraft Price (USD) | $4,450,000 | $ 7,695,000 | $30,650,000 |
| Max Cabin Seats | — | 7 | 19 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | No | — |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 6 | 8 | 21 |
| Galley Location | MID | — | — |
| Cabin Pressure (psi) | 6.2 | 9 | — |
| Standard Cabin Seats | 4 | 6 | 19 |
| SL Cabin Altitude (ft) | 14390 | 24000 | — |
| Max Cabin Seats | — | 7 | 19 |
| Galley / Refreshment | — | No | — |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | TBM 960 | PT6A–66B | CT7-8A |
| TBO (hrs) | 3500 | 3600 | 4000 |
| Horsepower | 850 | 850 | 2520 |
| Flat Rating | ISA + 49 | ISA + 28 | — |
| No. of Engines | — | 2 | 1 |
| Fuel Burn (gph) | — | 100 | — |
| Fuel Type | — | — | JetFuel |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 35.3 | 47.3 | — |
| Wingspan (ft) | 42.1 | 47.1 | — |
| Cabin Width (ft) | 4 | 6.1 | — |
| Cabin Height (ft) | 4.1 | 5.8 | — |
| Cabin Length (ft) | 13.4 | 14.9 | — |
| Cabin Volume (cu. ft) | 123 | — | 775 |
| Overall Height (ft) | — | 13.1 | 17.8 |
| Cabin Width - Floor (ft) | — | 3.5 | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |