Cirrus Vision Jet G2 vs Embraer Phenom 100ev vs Honda Aircraft Hondajet Elite vs Pilatus Pc 12 Ngx
The Cirrus Vision Jet G2 is the lightest, simplest option in this group, best suited to shorter regional missions. Its range is roughly 1,200 nautical miles, and it typically carries 4–5 passengers in real-world comfort (up to about 7 occupants including the pilot in certain configurations). The Embraer Phenom 100EV is a small very light jet aimed at faster point-to-point travel with a range around 1,170–1,180 nautical miles and usually seats 4–6 passengers (often up to 7 including pilot, depending on layout). The HondaJet Elite is also a very light jet, generally similar mission class, with a range around 1,200–1,220 nautical miles and commonly carries 4–5 passengers (up to 6 including pilot). The Pilatus PC-12 NGX is a single‑engine turboprop rather than a jet, trading some cruise speed for flexibility and payload; it offers the longest range here at roughly 1,800 nautical miles and typically seats 6–8 passengers, with high utility for shorter runways and more rugged operations.
| Spec | Cirrus Vision Jet G2 | Embraer Phenom 100EV | Honda Aircraft HondaJet Elite | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.37 | $ 2.84 | $ 2.73 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 5 | 7 | 6 | 8 |
| Manufacturer | Cirrus | Embraer | Honda Aircraft | Pilatus |
| Aircraft Name | SF50 G2 | Phenom 100EV | HondaJet Elite | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1219 | 1,178 | 1495 | 1803 |
| DOC / nm / Seat | $ 0.79 | $ 0.71 | $ 0.68 | $ 0.46 |
| Max Cabin Seats | 5 | 7 | 6 | 9 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2450 | 3451 | 3432 | — |
| Standard Cabin Seats | 3 | 5 | 4 | 6 |
| Direct Operating Cost | $ 711 | $ 1,152 | $ 1,135 | $ 793 |
| Flight Deck (Base Spec) | Cirrus Perspective Touch+ (G3000) | Prodigy Touch (G3000) | Garmin G3000 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 311 | 406 | 419 | 290 |
| Base Aircraft Price (USD) | $2,315,000 | $4,250,000 | $ 5,400,000 | $5,350,000 |
| Flight Rules | — | — | — | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | No | 1 Flushing | 1 Enclosed Flushing | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 5 | 6 | 6 | 8 |
| Max Cabin Seats | 5 | 6 | 6 | 9 |
| Cabin Pressure (psi) | 6.4 | 8.3 | 8.8 | 5.8 |
| Galley / Refreshment | No | No | Galley | No |
| Standard Cabin Seats | 3 | 4 | 4 | 6 |
| Crew Rest | — | No | No | — |
| Jump Seat | — | No | No | — |
| Lavatory Location | — | AFT | AFT | FWD |
| SL Cabin Altitude (ft) | — | 21280 | 23060 | 13100 |
| Galley Location | — | — | FWD | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | FJ33-5A | PW617F1-E | HF120-H1A | PT6E-67XP |
| TBO (hrs) | 4000 | 3500 | 5000 | 5000 |
| Flat Rating | ISA + 10 | ISA + 8 | ISA + 10 | ISA + 35 |
| Thrust (lbs) | 1846 | 1730 | 2050 | — |
| No. of Engines | 1 | 2 | 2 | 1 |
| Fuel Burn (lbph) | 358 | 543 | — | — |
| Fuel Capacity (gal) | 320 | — | 439 | — |
| Horsepower | — | — | — | 1200 |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 30.7 | 42.1 | 42.7 | 47.25 |
| Wingspan (ft) | 38.7 | 40.4 | 39.8 | 53.33 |
| Cabin Width (ft) | 5.1 | 5.1 | 5 | 5 |
| Cabin Length (ft) | 11.5 | 11 | 12.1 | 16.9 |
| Overall Height (ft) | 10.9 | 14.3 | 14.9 | 14 |
| Cabin Width - Floor (ft) | 3.1 | 3.6 | — | 4.25 |
| Cabin Length - Seating (ft) | 9.8 | 9 | 10.2 | — |
| Baggage Volume Ext. (cu. ft) | 30 | 60 | 66 | — |
| Baggage Volume Int. (cu. ft) | 24 | 10 | — | 40 |
| Aisle Step (ft) | — | 0.3 | 0.4 | — |
| Cabin Height (ft) | — | 4.9 | 4.8 | 4.9 |