Beechcraft King Air 360er vs Daher Tbm 960 vs Pilatus Pc 12 Ngx vs Piper M600 Sls
In category, the Beechcraft King Air 360ER is a pressurized, twin‑engine turboprop typically positioned as a higher‑capacity utility/corporate platform with strong runway and redundancy advantages. The Daher TBM 960 and Piper M600 SLS are pressurized single‑engine turboprops oriented toward owner‑pilots seeking high speed and efficiency, with the TBM generally competing as the faster, longer‑leg personal/business single. The Pilatus PC‑12 NGX is also a pressurized single‑engine turboprop but sits in a larger “utility/business” class than the TBM and M600, emphasizing cabin volume, cargo flexibility, and short/rough‑field capability. On range, the King Air 360ER is the long‑range standout among these, designed for extended missions. The TBM 960 typically offers long legs for a single, usually ahead of the M600 SLS, while the PC‑12 NGX delivers solid real‑world range that can vary notably with payload and mission profile. For passenger capacity, the PC‑12 NGX and King Air 360ER generally accommodate the most people comfortably, while the TBM 960 and M600 SLS are more commonly configured for fewer passengers in a smaller cabin.
| Spec | Beechcraft King Air 360ER | Daher TBM 960 | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | $ 2.25 | $ 2.78 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Beechcraft | Daher TBM | Pilatus | Piper |
| Aircraft Name | KingAir 350ER | TBM 960 | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2338 | 1730 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.55 | $ 0.56 | $ 0.46 | $ 0.55 |
| Max Cabin Seats | 9 | — | 9 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6585 | 2908 | — | 2200 |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| Direct Operating Cost | $ 1,324 | $ 744 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 303 | 330 | 290 | 274 |
| Base Aircraft Price (USD) | $8,750,000 | $4,450,000 | $5,350,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | Yes (Belted Optional) | No | Optional | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Cargo Door | Optional | — | Yes | — |
| Total Seats | 10 | 6 | 8 | 5 |
| Galley Location | FWD | MID | — | MID |
| Max Cabin Seats | 9 | — | 9 | — |
| Lavatory Location | AFT | — | FWD | — |
| Cabin Pressure (psi) | 6.5 | 6.2 | 5.8 | 5.6 |
| Galley / Refreshment | Refreshment Center | — | No | Refreshment Centre |
| Standard Cabin Seats | 8 | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | — | 14390 | 13100 | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | PT6A-60A | TBM 960 | PT6E-67XP | PT6A-42A |
| TBO (hrs) | 3600 | 3500 | 5000 | 3600 |
| Horsepower | 1050 | 850 | 1200 | 600 |
| Flat Rating | ISA + 10 | ISA + 49 | ISA + 35 | ISA + 55 |
| No. of Engines | 1 | — | 1 | 1 |
| Fuel Capacity (gal) | 775 | — | — | 260 |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 46.7 | 35.3 | 47.25 | 29.7 |
| Wingspan (ft) | 57.9 | 42.1 | 53.33 | 43.2 |
| Cabin Width (ft) | 4.5 | 4 | 5 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.1 | 4.9 | 4 |
| Cabin Length (ft) | 19.5 | 13.4 | 16.9 | 12.3 |
| Overall Height (ft) | 14.4 | — | 14 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — | 4.25 | — |
| Cabin Length - Seating (ft) | 19.5 | — | — | — |
| Baggage Volume Int. (cu. ft) | 71 | — | 40 | 20 |
| Cabin Volume (cu. ft) | — | 123 | — | 165 |