Beechcraft Kingair 350i vs Cessna Citation M2 vs Pilatus Pc 12 Ngx
The Beechcraft King Air 360 and Pilatus PC-12 NGX are both pressurized single/twin‑turboprop business aircraft, while the Cessna Citation M2 is a light business jet. In category terms, the King Air 360 is a twin‑engine turboprop optimized for short-field versatility and efficient regional missions; the PC-12 NGX is a single‑engine turboprop known for rugged field capability and cargo/flex cabin use; the Citation M2 is a twin‑engine jet aimed at faster point‑to‑point travel between paved airports. For range, the PC-12 NGX and King Air 360 generally sit in a similar “regional-to-medium” band, typically around the mid‑1,000‑nautical‑mile class depending on payload and reserves, while the Citation M2 is also in a comparable general range class but tends to trade some endurance flexibility for higher cruise speed. For passenger capacity, all three commonly seat around 6 to 8 in typical executive layouts. The PC-12 NGX can be configured for more seats in commuter-style arrangements, while the King Air 360 often offers the most conventional multi-seat business cabin feel; the Citation M2 usually carries fewer people most comfortably due to a smaller light-jet cabin.
| Spec | Cessna Citation M2 | Pilatus PC-12 NGX |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.45 | $ 2.78 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 8 |
| Manufacturer | Cessna Citation | Pilatus |
| Aircraft Name | M2 | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1803 |
| DOC / nm / Seat | $ 0.58 | $ 0.46 |
| Max Cabin Seats | 7 | 9 |
| OEM Verification | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3810 | — |
| Standard Cabin Seats | 6 | 6 |
| Direct Operating Cost | $ 1,395 | $ 793 |
| Flight Deck (Base Spec) | Garmin G3000 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 404 | 290 |
| Base Aircraft Price (USD) | $5,150,000 | $5,350,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | Optional |
| Min Crew | 1 | 1 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 8 | 8 |
| Max Cabin Seats | 7 | 9 |
| Lavatory Location | AFT | FWD |
| Cabin Pressure (psi) | 8.5 | 5.8 |
| Galley / Refreshment | No | No |
| Standard Cabin Seats | 6 | 6 |
| SL Cabin Altitude (ft) | 22027 | 13100 |
| Cargo Door | — | Yes |
| Engine | ||
| FADEC | Yes | Yes |
| Model | FJ44-1AP-21 | PT6E-67XP |
| TBO (hrs) | 3500 | 5000 |
| Flat Rating | ISA + 7 | ISA + 35 |
| Thrust (lbs) | 1965 | — |
| No. of Engines | 2 | 1 |
| Fuel Burn (lbph) | 516 | — |
| Fuel Capacity (gal) | 492 | — |
| Horsepower | — | 1200 |
| Usable Fuel (gal) | — | 402 |
| Dimensions | ||
| Length (ft) | 42.6 | 47.25 |
| Wingspan (ft) | 47.3 | 53.33 |
| Aisle Step (ft) | 0.4 | — |
| Cabin Width (ft) | 4.8 | 5 |
| Cabin Height (ft) | 4.8 | 4.9 |
| Cabin Length (ft) | 11 | 16.9 |
| Overall Height (ft) | 14 | 14 |
| Cabin Width - Floor (ft) | 3.1 | 4.25 |
| Cabin Length - Seating (ft) | 8.8 | — |
| Baggage Volume Ext. (cu. ft) | 46 | — |
| Baggage Volume Int. (cu. ft) | — | 40 |