Embraer Phenom 100ev vs Embraer Phenom 300e vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx
By category, the Embraer Phenom 100EV is an entry-level very light jet, the Phenom 300E is a light jet (often considered “super-light”), the Piaggio Avanti EVO is a high-speed twin‑turboprop, and the Pilatus PC‑12 NGX is a single‑engine turboprop utility/business aircraft. On range, the Phenom 100EV is the shortest-legged of the group at roughly 1,100–1,200 nautical miles. The Phenom 300E typically reaches about 1,900–2,000 nautical miles, giving it the longest range among the two jets and usually edging the turboprops. The Avanti EVO generally sits in the mid-to-upper range around 1,700–1,800 nautical miles, while the PC‑12 NGX is commonly around 1,700–1,800 nautical miles depending on configuration and reserves. For passenger capacity, the Phenom 100EV is usually configured for about 4–6 passengers, the Phenom 300E for about 6–8, the Avanti EVO typically about 6–8, and the PC‑12 NGX commonly about 6–9 in executive layouts, with higher-density seating possible in utility configurations.
| Spec | Embraer Phenom 100EV | Embraer Phenom 300E | Piaggio Avanti EVO | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.84 | $ 3.88 | — | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 7 | 10 | 8 | 8 |
| Manufacturer | Embraer | Embraer | Piaggio | Pilatus |
| Aircraft Name | Phenom 100EV | Phenom 300E | Avanti EVO | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1,178 | 2,010 | 1530 | 1803 |
| DOC / nm / Seat | $ 0.71 | $ 0.55 | — | $ 0.46 |
| Max Cabin Seats | 7 | 10 | 7 | 9 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3451 | 6914 | 3775 | — |
| Standard Cabin Seats | 5 | 6 | 6 | 6 |
| Direct Operating Cost | $ 1,152 | $ 1,758 | — | $ 793 |
| Flight Deck (Base Spec) | Prodigy Touch (G3000) | Prodigy Touch (G3000) | Rockwell Collins Pro Line 21 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 406 | 464 | 400 | 290 |
| Base Aircraft Price (USD) | $4,250,000 | $9,650,000 | $ 7,695,000 | $5,350,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Enclosed Flushing | No | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Crew Rest | No | No | — | — |
| Jump Seat | No | No | — | — |
| Total Seats | 6 | 9 | 8 | 8 |
| Max Cabin Seats | 6 | 9 | 7 | 9 |
| Lavatory Location | AFT | AFT | — | FWD |
| Cabin Pressure (psi) | 8.3 | 9.4 | 9 | 5.8 |
| Galley / Refreshment | No | Galley | No | No |
| Standard Cabin Seats | 4 | 7 | 6 | 6 |
| SL Cabin Altitude (ft) | 21280 | 25560 | 24000 | 13100 |
| Galley Location | — | FWD | — | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | PW617F1-E | Canada PW535E1 | PT6A–66B | PT6E-67XP |
| TBO (hrs) | 3500 | 5000 | 3600 | 5000 |
| Flat Rating | ISA + 8 | ISA + 15 | ISA + 28 | ISA + 35 |
| Thrust (lbs) | 1730 | 3360 | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Burn (lbph) | 543 | 757 | — | — |
| Horsepower | — | — | 850 | 1200 |
| Fuel Burn (gph) | — | — | 100 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 42.1 | 51.2 | 47.3 | 47.25 |
| Wingspan (ft) | 40.4 | 52.16 | 47.1 | 53.33 |
| Aisle Step (ft) | 0.3 | 0.3 | — | — |
| Cabin Width (ft) | 5.1 | 5.1 | 6.1 | 5 |
| Cabin Height (ft) | 4.9 | 4.9 | 5.8 | 4.9 |
| Cabin Length (ft) | 11 | 17.2 | 14.9 | 16.9 |
| Overall Height (ft) | 14.3 | 16.75 | 13.1 | 14 |
| Cabin Width - Floor (ft) | 3.6 | 3.6 | 3.5 | 4.25 |
| Cabin Length - Seating (ft) | 9 | 14.8 | — | — |
| Baggage Volume Ext. (cu. ft) | 60 | 74 | — | — |
| Baggage Volume Int. (cu. ft) | 10 | 10 | 35.2 | 40 |