Piper M350 vs Cessna Denali vs Pilatus Pc 12 Ngx
The Piper M350 is a pressurized, piston‑engine single positioned as an owner‑flown step‑up from high‑performance pistons, with shorter range and lower cruise efficiency than the two turboprops. Typical missions are regional trips rather than long, heavy legs; cabin seating is usually arranged for about five to six passengers, depending on configuration and payload. The Cessna Denali is a single‑engine turboprop in the modern, high‑end utility/exec class, aimed between light twins and larger turboprops. It is designed for longer legs than the M350 and generally targets roughly six to eight passengers in an executive layout, with range intended to cover many nonstop city pairs that would be a stretch for a piston single. The Pilatus PC‑12 NGX is a larger, more capable single‑engine turboprop known for strong payload, flexibility, and short/rough‑field utility. It typically carries six to nine passengers in executive configurations and offers long‑range capability that is competitive at the top of the class, generally exceeding both the M350 and many projected Denali mission profiles.
| Spec | Pilatus PC-12 NGX | Piper M350 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 2.78 | $ 1.34 |
| Min Crew | 1 | — |
| Total Seats | 8 | 6 |
| Flight Rules | IFR | VFR |
| Manufacturer | Pilatus | Piper |
| Aircraft Name | PC-12 NGX | M350 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1803 | 1343 |
| DOC / nm / Seat | $ 0.46 | $ 0.22 |
| Max Cabin Seats | 9 | — |
| OEM Verification | VERIFIED | Un-Verified |
| Standard Cabin Seats | 6 | 4 |
| Direct Operating Cost | $ 793 | $ 285 |
| Flight Deck (Base Spec) | Honeywell Primus Apex | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 290 | 213 |
| Base Aircraft Price (USD) | $5,350,000 | $1,195,000 |
| Useful Load (lbs) | — | 1308 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | Optional | — |
| Min Crew | 1 | — |
| Cargo Door | Yes | — |
| Total Seats | 8 | 6 |
| Max Cabin Seats | 9 | — |
| Lavatory Location | FWD | — |
| Cabin Pressure (psi) | 5.8 | 5.6 |
| Galley / Refreshment | No | — |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 13100 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | PT6E-67XP | TIO-540-AE2A |
| TBO (hrs) | 5000 | 2000 |
| Horsepower | 1200 | 350 |
| Flat Rating | ISA + 35 | — |
| No. of Engines | 1 | 1 |
| Usable Fuel (gal) | 402 | — |
| Fuel Type | — | AvGas |
| TBO (yrs) | — | 12 |
| Fuel Delivery | — | Fuel Injected |
| Fuel Capacity (gal) | — | 120 |
| Dimensions | ||
| Length (ft) | 47.25 | 29 |
| Wingspan (ft) | 53.33 | 43 |
| Cabin Width (ft) | 5 | 4.1 |
| Cabin Height (ft) | 4.9 | 4 |
| Cabin Length (ft) | 16.9 | 12.3 |
| Overall Height (ft) | 14 | 11.4 |
| Cabin Width - Floor (ft) | 4.25 | — |
| Baggage Volume Int. (cu. ft) | 40 | 20 |
| Cabin Volume (cu. ft) | — | 165 |
| Baggage Volume Ext. (cu. ft) | — | 13 |