Beechcraft King Air 360er vs Daher Tbm 960 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360ER and Pilatus PC-12 NGX sit in the “large single/entry twin utility turboprop” space aimed at flexible missions and short-runway capability, while the Daher TBM 960 is a high-performance, pressurized single-engine turboprop optimized for owner-pilot speed and efficiency, and the Piaggio Avanti EVO is a faster, distinctive pusher-turboprop positioned as a light business aircraft alternative. On range, the King Air 360ER is generally the longest-legged of the group, designed for extended missions and special-mission endurance. The PC-12 NGX offers long range in a similar practical category, typically competitive but usually not exceeding the 360ER’s “ER” profile. The TBM 960 delivers strong range for a fast single, but is more oriented to rapid point-to-point trips than maximum endurance. The Avanti EVO’s range is typically in the same broad band as the TBM/PC-12 class, with emphasis on higher cruise speeds rather than the very longest reach. On passenger capacity, the King Air 360ER commonly seats the most in standard layouts (often around 8–9), the PC-12 NGX is close behind (commonly 6–9 depending on configuration), while the Avanti EVO and TBM 960 are typically configured for fewer passengers (often about 4–7, layout dependent).
| Spec | Beechcraft King Air 360ER | Daher TBM 960 | Piaggio Avanti EVO | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 2.25 | — | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 8 | 8 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Piaggio | Pilatus |
| Aircraft Name | KingAir 350ER | TBM 960 | Avanti EVO | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 1730 | 1530 | 1803 |
| DOC / nm / Seat | $ 0.55 | $ 0.56 | — | $ 0.46 |
| Max Cabin Seats | 9 | — | 7 | 9 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6585 | 2908 | 3775 | — |
| Standard Cabin Seats | 8 | 4 | 6 | 6 |
| Direct Operating Cost | $ 1,324 | $ 744 | — | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Rockwell Collins Pro Line 21 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 303 | 330 | 400 | 290 |
| Base Aircraft Price (USD) | $8,750,000 | $4,450,000 | $ 7,695,000 | $5,350,000 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | No | No | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | Optional | — | — | Yes |
| Total Seats | 10 | 6 | 8 | 8 |
| Galley Location | FWD | MID | — | — |
| Max Cabin Seats | 9 | — | 7 | 9 |
| Lavatory Location | AFT | — | — | FWD |
| Cabin Pressure (psi) | 6.5 | 6.2 | 9 | 5.8 |
| Galley / Refreshment | Refreshment Center | — | No | No |
| Standard Cabin Seats | 8 | 4 | 6 | 6 |
| SL Cabin Altitude (ft) | — | 14390 | 24000 | 13100 |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PT6A-60A | TBM 960 | PT6A–66B | PT6E-67XP |
| TBO (hrs) | 3600 | 3500 | 3600 | 5000 |
| Horsepower | 1050 | 850 | 850 | 1200 |
| Flat Rating | ISA + 10 | ISA + 49 | ISA + 28 | ISA + 35 |
| No. of Engines | 1 | — | 2 | 1 |
| Fuel Capacity (gal) | 775 | — | — | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 46.7 | 35.3 | 47.3 | 47.25 |
| Wingspan (ft) | 57.9 | 42.1 | 47.1 | 53.33 |
| Cabin Width (ft) | 4.5 | 4 | 6.1 | 5 |
| Cabin Height (ft) | 4.8 | 4.1 | 5.8 | 4.9 |
| Cabin Length (ft) | 19.5 | 13.4 | 14.9 | 16.9 |
| Overall Height (ft) | 14.4 | — | 13.1 | 14 |
| Cabin Width - Floor (ft) | 4.1 | — | 3.5 | 4.25 |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | — | 35.2 | 40 |
| Cabin Volume (cu. ft) | — | 123 | — | — |