Daher Tbm 960 vs Pilatus Pc 12 Ngx vs Pilatus Pc 24 vs Piper M600 Sls
The Daher TBM 960 and Piper M600 SLS are high-performance single‑engine turboprops aimed at owner‑pilots, while the Pilatus PC‑12 NGX is a larger, utility‑oriented single‑engine turboprop and the Pilatus PC‑24 is a light business jet. In range terms, the PC‑12 NGX generally leads among the turboprops at roughly 1,800–1,900 nautical miles, the TBM 960 is typically around 1,700–1,800 nautical miles, and the M600 SLS is usually about 1,400–1,500 nautical miles. The PC‑24’s range varies by load but is commonly around 2,000 nautical miles, often exceeding the single‑engine turboprops when operated with typical passenger loads. For passenger capacity, the M600 SLS is commonly configured for about 4–6 passengers plus pilot, the TBM 960 for about 4–6 passengers plus pilot, and the PC‑12 NGX for up to about 6–9 passengers plus pilot depending on interior and payload. The PC‑24 typically seats about 6–8 passengers in executive layouts, with maximum seating options higher in dense configurations.
| Spec | Daher TBM 960 | Pilatus PC-12 NGX | Pilatus PC-24 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 2.78 | $ 3.71 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 6 | 6 |
| Flight Rules | IFR | IFR | — | IFR |
| Manufacturer | Daher TBM | Pilatus | Pilatus | Piper |
| Aircraft Name | TBM 960 | PC-12 NGX | PC-24 | M600 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 1803 | 2076 | 1406 |
| DOC / nm / Seat | $ 0.56 | $ 0.46 | $ 0.62 | $ 0.55 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 2908 | — | 6680 | 2200 |
| Standard Cabin Seats | 4 | 6 | 6 | 4 |
| Direct Operating Cost | $ 744 | $ 793 | $ 1,619 | $ 603 |
| Flight Deck (Base Spec) | Garmin G3000 | Honeywell Primus Apex | Pilatus ACE (Primus Apex) | Garmin G3000 |
| Max Cruise Speed (ktas) | 330 | 290 | 440 | 274 |
| Base Aircraft Price (USD) | $4,450,000 | $5,350,000 | $11,800,000 | $3,081,400 |
| Max Cabin Seats | — | 9 | 10 | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | Optional | 1 Enclosed Flushing | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 8 | 6 | 5 |
| Galley Location | MID | — | FWD | MID |
| Cabin Pressure (psi) | 6.2 | 5.8 | 9.3 | 5.6 |
| Standard Cabin Seats | 4 | 6 | 6 | 4 |
| SL Cabin Altitude (ft) | 14390 | 13100 | 23500 | 12600 |
| Cargo Door | — | Yes | Yes | — |
| Max Cabin Seats | — | 9 | 10 | — |
| Lavatory Location | — | FWD | FWD | — |
| Galley / Refreshment | — | No | Optional Refreshment Center | Refreshment Centre |
| Crew Rest | — | — | No | — |
| Jump Seat | — | — | No | — |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | TBM 960 | PT6E-67XP | FJ44-4A-QPM | PT6A-42A |
| TBO (hrs) | 3500 | 5000 | 5000 | 3600 |
| Horsepower | 850 | 1200 | — | 600 |
| Flat Rating | ISA + 49 | ISA + 35 | ISA + 23 | ISA + 55 |
| No. of Engines | — | 1 | 2 | 1 |
| Usable Fuel (gal) | — | 402 | — | — |
| Thrust (lbs) | — | — | 3435 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 35.3 | 47.25 | 52.2 | 29.7 |
| Wingspan (ft) | 42.1 | 53.33 | 55.8 | 43.2 |
| Cabin Width (ft) | 4 | 5 | 5.6 | 4.1 |
| Cabin Height (ft) | 4.1 | 4.9 | 5.1 | 4 |
| Cabin Length (ft) | 13.4 | 16.9 | 23 | 12.3 |
| Cabin Volume (cu. ft) | 123 | — | — | 165 |
| Overall Height (ft) | — | 14 | 17.4 | 11.3 |
| Cabin Width - Floor (ft) | — | 4.25 | 3.8 | — |
| Baggage Volume Int. (cu. ft) | — | 40 | 90 | 20 |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |