Beechcraft Kingair Denali vs Daher Tbm 960 vs Pilatus Pc 12 Ngx vs Piper M600 Sls
The Beechcraft King Air Denali and Pilatus PC-12 NGX sit in the larger, more utility‑oriented single‑engine turboprop class, while the Daher TBM 960 and Piper M600 SLS are closer to the “owner‑pilot personal transport” end of the spectrum, typically prioritizing speed and cockpit sophistication over cabin volume. In range terms, the TBM 960 is generally the long‑leg specialist among these, often flown on very long nonstop segments, with the PC‑12 NGX and Denali also offering strong IFR cross‑country capability and flexible mission profiles. The M600 SLS is usually the shortest‑range of the four, though still capable for regional trips. For passenger capacity, the PC‑12 NGX and King Air Denali typically offer the most usable cabin space and loading flexibility, commonly configured for about six to nine occupants depending on layout and mission. The TBM 960 is usually arranged for about four to six passengers plus a pilot in a tighter, more streamlined cabin. The M600 SLS is also commonly a five‑to‑six‑seat aircraft, emphasizing comfort for fewer passengers rather than maximum cabin volume.
| Spec | Beechcraft KingAir Denali | Daher TBM 960 | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 2.25 | $ 2.78 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 6 | 8 | 6 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | GE® Aerospace | Daher TBM | Pilatus | Piper |
| Aircraft Name | KingAir Denali | TBM 960 | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1730 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.68 | $ 0.56 | $ 0.46 | $ 0.55 |
| Max Cabin Seats | 9 | — | 9 | — |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3280 | 2908 | — | 2200 |
| Standard Cabin Seats | 7 | 4 | 6 | 4 |
| Direct Operating Cost | $ 1,111 | $ 744 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 285 | 330 | 290 | 274 |
| Base Aircraft Price (USD) | $4,150,000 | $4,450,000 | $5,350,000 | $3,081,400 |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | No | Optional | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 6 | 8 | 5 |
| Max Cabin Seats | 9 | — | 9 | — |
| Lavatory Location | AFT | — | FWD | — |
| Cabin Pressure (psi) | 5 | 6.2 | 5.8 | 5.6 |
| Galley / Refreshment | No | — | No | Refreshment Centre |
| Standard Cabin Seats | 7 | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 11065 | 14390 | 13100 | 12600 |
| Galley Location | — | MID | — | MID |
| Cargo Door | — | — | Yes | — |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| Model | Catalyst™ | TBM 960 | PT6E-67XP | PT6A-42A |
| No. of Engines | 1 | — | 1 | 1 |
| FADEC | — | Yes | Yes | No |
| TBO (hrs) | — | 3500 | 5000 | 3600 |
| Horsepower | — | 850 | 1200 | 600 |
| Flat Rating | — | ISA + 49 | ISA + 35 | ISA + 55 |
| Usable Fuel (gal) | — | — | 402 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 14.86 | 35.3 | 47.25 | 29.7 |
| Wingspan (ft) | 54.3 | 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) | 12.6 | 13.4 | 16.9 | 12.3 |
| Overall Height (ft) | 4.65 | — | 14 | 11.3 |
| Cabin Width - Floor (ft) | 4.1 | — | 4.25 | — |
| Cabin Length - Seating (ft) | 12.6 | — | — | — |
| Baggage Volume Int. (cu. ft) | 48 | — | 40 | 20 |
| Cabin Volume (cu. ft) | — | 123 | — | 165 |