Daher Tbm 960 vs Pilatus Pc 24 vs Piper M600 Sls vs Sikorsky S 92
The Daher TBM 960 and Piper M600 SLS are single‑engine turboprop airplanes best suited to fast, owner‑flown point‑to‑point travel. The TBM 960 is typically the quicker, longer‑leg option, with a range around 1,400–1,700 nautical miles depending on mission, and it generally carries 4–6 passengers in addition to the pilot (up to about 6 occupants total in many real‑world layouts). The M600 SLS is a step down in size and reach, commonly around 1,000–1,400 nautical miles, and usually seats about 4–5 passengers plus the pilot. The Pilatus PC‑24 is a twin‑engine light jet aimed at corporate and charter use, offering higher payload flexibility and speed, with typical ranges roughly 1,700–2,000 nautical miles and seating commonly 6–8 passengers (with higher‑density configurations possible). The Sikorsky S‑92 is a large twin‑engine helicopter for offshore, SAR, and VIP transport. It trades speed and range for vertical lift, typically flying roughly 400–600 nautical miles, while carrying far more people—often 12–19 passengers (and up to more depending on configuration).
| Spec | Daher TBM 960 | Pilatus PC-24 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.25 | $ 3.71 | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 6 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Daher TBM | Pilatus | Piper | Sikorsky |
| Aircraft Name | TBM 960 | PC-24 | M600 | S-92 |
| Aircraft Type | Turbo Prop | — | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1730 | 2076 | 1406 | 439 |
| DOC / nm / Seat | $ 0.56 | $ 0.62 | $ 0.55 | $ 0.94 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2908 | 6680 | 2200 | 7417 |
| Standard Cabin Seats | 4 | 6 | 4 | 19 |
| Direct Operating Cost | $ 744 | $ 1,619 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | Garmin G3000 | Pilatus ACE (Primus Apex) | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 330 | 440 | 274 | 155 |
| Base Aircraft Price (USD) | $4,450,000 | $11,800,000 | $3,081,400 | $30,650,000 |
| Max Cabin Seats | — | 10 | — | 19 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | 1 Enclosed Flushing | No | — |
| Min Crew | 1 | 1 | 1 | 2 |
| Total Seats | 6 | 6 | 5 | 21 |
| Galley Location | MID | FWD | MID | — |
| Cabin Pressure (psi) | 6.2 | 9.3 | 5.6 | — |
| Standard Cabin Seats | 4 | 6 | 4 | 19 |
| SL Cabin Altitude (ft) | 14390 | 23500 | 12600 | — |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Cargo Door | — | Yes | — | — |
| Max Cabin Seats | — | 10 | — | 19 |
| Lavatory Location | — | FWD | — | — |
| Galley / Refreshment | — | Optional Refreshment Center | Refreshment Centre | — |
| Max Cabin Altitude (ft) | — | — | 8644 | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | TBM 960 | FJ44-4A-QPM | PT6A-42A | CT7-8A |
| TBO (hrs) | 3500 | 5000 | 3600 | 4000 |
| Horsepower | 850 | — | 600 | 2520 |
| Flat Rating | ISA + 49 | ISA + 23 | ISA + 55 | — |
| Thrust (lbs) | — | 3435 | — | — |
| No. of Engines | — | 2 | 1 | 1 |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Fuel Type | — | — | — | JetFuel |
| Dimensions | ||||
| Length (ft) | 35.3 | 52.2 | 29.7 | — |
| Wingspan (ft) | 42.1 | 55.8 | 43.2 | — |
| Cabin Width (ft) | 4 | 5.6 | 4.1 | — |
| Cabin Height (ft) | 4.1 | 5.1 | 4 | — |
| Cabin Length (ft) | 13.4 | 23 | 12.3 | — |
| Cabin Volume (cu. ft) | 123 | — | 165 | 775 |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Overall Height (ft) | — | 17.4 | 11.3 | 17.8 |
| Cabin Width - Floor (ft) | — | 3.8 | — | — |
| Cabin Length - Seating (ft) | — | 17 | — | — |
| Baggage Volume Int. (cu. ft) | — | 90 | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |