Cessna Citation M2 vs Cirrus Vision Jet G2 vs Embraer Phenom 100ev vs Pilatus Pc 12 Ngx
The Cessna Citation M2 and Embraer Phenom 100EV are very light jets, the Cirrus Vision Jet G2 is a single‑engine “personal jet,” and the Pilatus PC‑12 NGX is a single‑engine turboprop, so it trades jet speed for strong utility. In range, the PC‑12 NGX generally leads this group, offering the longest typical IFR legs, while the Phenom 100EV and Citation M2 sit in the middle with similar real‑world mission capability; the Vision Jet G2 is usually shorter‑legged than the twin‑engine VLJs, though still suitable for many regional trips. For passenger capacity, the PC‑12 NGX typically carries the most people comfortably and has the most cabin flexibility. The Citation M2 and Phenom 100EV usually seat around five to seven depending on configuration, fitting the classic owner‑operator or small charter mission. The Vision Jet G2 is often configured with up to seven seats including the side‑facing “jump” seats, but in practical use it’s best viewed as a smaller‑cabin option optimized for personal travel rather than maximum payload.
| Spec | Cessna Citation M2 | Cirrus Vision Jet G2 | Embraer Phenom 100EV | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 3.45 | $ 2.37 | $ 2.84 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 5 | 7 | 8 |
| Manufacturer | Cessna Citation | Cirrus | Embraer | Pilatus |
| Aircraft Name | M2 | SF50 G2 | Phenom 100EV | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1219 | 1,178 | 1803 |
| DOC / nm / Seat | $ 0.58 | $ 0.79 | $ 0.71 | $ 0.46 |
| Max Cabin Seats | 7 | 5 | 7 | 9 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3810 | 2450 | 3451 | — |
| Standard Cabin Seats | 6 | 3 | 5 | 6 |
| Direct Operating Cost | $ 1,395 | $ 711 | $ 1,152 | $ 793 |
| Flight Deck (Base Spec) | Garmin G3000 | Cirrus Perspective Touch+ (G3000) | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 404 | 311 | 406 | 290 |
| Base Aircraft Price (USD) | $5,150,000 | $2,315,000 | $4,250,000 | $5,350,000 |
| Flight Rules | — | — | — | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | 1 Flushing | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Crew Rest | No | — | No | — |
| Jump Seat | No | — | No | — |
| Total Seats | 8 | 5 | 6 | 8 |
| Max Cabin Seats | 7 | 5 | 6 | 9 |
| Lavatory Location | AFT | — | AFT | FWD |
| Cabin Pressure (psi) | 8.5 | 6.4 | 8.3 | 5.8 |
| Galley / Refreshment | No | No | No | No |
| Standard Cabin Seats | 6 | 3 | 4 | 6 |
| SL Cabin Altitude (ft) | 22027 | — | 21280 | 13100 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | FJ44-1AP-21 | FJ33-5A | PW617F1-E | PT6E-67XP |
| TBO (hrs) | 3500 | 4000 | 3500 | 5000 |
| Flat Rating | ISA + 7 | ISA + 10 | ISA + 8 | ISA + 35 |
| Thrust (lbs) | 1965 | 1846 | 1730 | — |
| No. of Engines | 2 | 1 | 2 | 1 |
| Fuel Burn (lbph) | 516 | 358 | 543 | — |
| Fuel Capacity (gal) | 492 | 320 | — | — |
| Horsepower | — | — | — | 1200 |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 42.6 | 30.7 | 42.1 | 47.25 |
| Wingspan (ft) | 47.3 | 38.7 | 40.4 | 53.33 |
| Aisle Step (ft) | 0.4 | — | 0.3 | — |
| Cabin Width (ft) | 4.8 | 5.1 | 5.1 | 5 |
| Cabin Height (ft) | 4.8 | — | 4.9 | 4.9 |
| Cabin Length (ft) | 11 | 11.5 | 11 | 16.9 |
| Overall Height (ft) | 14 | 10.9 | 14.3 | 14 |
| Cabin Width - Floor (ft) | 3.1 | 3.1 | 3.6 | 4.25 |
| Cabin Length - Seating (ft) | 8.8 | 9.8 | 9 | — |
| Baggage Volume Ext. (cu. ft) | 46 | 30 | 60 | — |
| Baggage Volume Int. (cu. ft) | — | 24 | 10 | 40 |