Pilatus Pc 12 Ngx vs Piper M350 vs Piper M600
The Pilatus PC-12 NGX, Piper M350, and Piper M600 SLS sit in different categories despite overlapping missions. The PC-12 NGX is a single‑engine turboprop utility/business aircraft, optimized for short and rougher runway capability, flexible cabin use, and high payload for its class. The M350 is a pressurized piston single aimed at owner‑pilots, typically used for personal and business travel where lower acquisition and operating complexity matter more than speed or payload. The M600 SLS is a single‑engine turboprop positioned as a step up from piston singles, pairing higher cruise performance with simplified systems and automation. On range, the PC-12 NGX and M600 SLS generally offer longer legs than the M350, with typical IFR ranges roughly around 1,500–1,800 nm for the turboprops versus about 1,200–1,400 nm for the M350 depending on reserves, loading, and conditions. For passenger capacity, the PC-12 NGX usually seats the most in practical configurations, often 6–9 passengers plus one or two pilots. The M600 SLS commonly carries about 4–6 passengers plus a pilot, while the M350 is typically 3–5 passengers plus a pilot.
| 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 |