Pilatus Pc 24 vs Piper M350
The Pilatus PC-24 and Piper M350 sit in different aircraft categories and are built for different missions. The PC-24 is a light business jet, optimized for higher cruise speeds and jet performance, while also being known for operational flexibility, including the ability to use shorter runways than many comparable jets. The Piper M350 is a pressurized, single‑engine piston aircraft, typically chosen for lower operating costs and efficient personal or small-business travel rather than pure speed. In range, the PC-24 generally offers a longer typical mission capability than the M350, enabling farther nonstop trips with higher cruise speeds, though exact numbers vary by payload, winds, and reserves. The M350 provides solid cross-country range for a piston platform, but it is usually more limited on longer legs compared with a light jet. For passenger capacity, the PC-24 commonly accommodates around 6 to 8 passengers in a business configuration (often with optional seating variations), whereas the M350 typically carries about 5 to 6 occupants including the pilot, making it better suited to smaller groups.
| Spec | Pilatus PC-24 | Piper M350 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.71 | $ 1.34 |
| Min Crew | 1 | — |
| Total Seats | 6 | 6 |
| Manufacturer | Pilatus | Piper |
| Aircraft Name | PC-24 | M350 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2076 | 1343 |
| DOC / nm / Seat | $ 0.62 | $ 0.22 |
| Max Cabin Seats | 10 | — |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6680 | 1308 |
| Standard Cabin Seats | 6 | 4 |
| Direct Operating Cost | $ 1,619 | $ 285 |
| Flight Deck (Base Spec) | Pilatus ACE (Primus Apex) | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 440 | 213 |
| Base Aircraft Price (USD) | $11,800,000 | $1,195,000 |
| Flight Rules | — | VFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | — |
| Min Crew | 1 | — |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Cargo Door | Yes | — |
| Total Seats | 6 | 6 |
| Galley Location | FWD | — |
| Max Cabin Seats | 10 | — |
| Lavatory Location | FWD | — |
| Cabin Pressure (psi) | 9.3 | 5.6 |
| Galley / Refreshment | Optional Refreshment Center | — |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 23500 | — |
| Engine | ||
| FADEC | Yes | No |
| Model | FJ44-4A-QPM | TIO-540-AE2A |
| TBO (hrs) | 5000 | 2000 |
| Flat Rating | ISA + 23 | — |
| Thrust (lbs) | 3435 | — |
| No. of Engines | 2 | 1 |
| Fuel Type | — | AvGas |
| TBO (yrs) | — | 12 |
| Horsepower | — | 350 |
| Fuel Delivery | — | Fuel Injected |
| Fuel Capacity (gal) | — | 120 |
| Dimensions | ||
| Length (ft) | 52.2 | 29 |
| Wingspan (ft) | 55.8 | 43 |
| Aisle Step (ft) | Flat Floor | — |
| Cabin Width (ft) | 5.6 | 4.1 |
| Cabin Height (ft) | 5.1 | 4 |
| Cabin Length (ft) | 23 | 12.3 |
| Overall Height (ft) | 17.4 | 11.4 |
| Cabin Width - Floor (ft) | 3.8 | — |
| Cabin Length - Seating (ft) | 17 | — |
| Baggage Volume Int. (cu. ft) | 90 | 20 |
| Cabin Volume (cu. ft) | — | 165 |
| Baggage Volume Ext. (cu. ft) | — | 13 |