Embraer Phenom 300e vs Embraer Praetor 600 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx
By category, the Embraer Phenom 300E is a light jet optimized for short-to-mid missions, the Embraer Praetor 600 is a super‑midsize jet built for longer, higher‑end trips, the Piaggio Avanti EVO is a fast twin‑turboprop with a cabin feel closer to a light jet, and the Pilatus PC‑12 NGX is a single‑engine turboprop known for utility and short/rough‑field flexibility. On range, the Praetor 600 leads at roughly 4,000+ nautical miles, enabling true long‑haul city pairs. The Phenom 300E typically offers about 2,000–2,200 nautical miles, suited to regional and transcontinental-light missions. The Avanti EVO is generally around 1,700–1,900 nautical miles, and the PC‑12 NGX is in a similar ballpark at about 1,700–1,800 nautical miles, though real‑world range varies with payload and winds. For passenger capacity, the Phenom 300E commonly seats 6–8, the Praetor 600 typically 8–12 depending on configuration, the Avanti EVO usually 7–9, and the PC‑12 NGX often 6–9 with flexible layouts.
| Spec | Embraer Phenom 300E | Embraer Praetor 600 | Piaggio Avanti EVO | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 3.88 | $ 6.74 | — | $ 2.78 |
| Min Crew | 1 | 2 | 1 | 1 |
| Total Seats | 10 | 10 | 8 | 8 |
| Manufacturer | Embraer | Embraer | Piaggio | Pilatus |
| Aircraft Name | Phenom 300E | Praetor 600 | Avanti EVO | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2,010 | 4018 | 1530 | 1803 |
| DOC / nm / Seat | $ 0.55 | $ 0.84 | — | $ 0.46 |
| Max Cabin Seats | 10 | 12 | 7 | 9 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6914 | — | 3775 | — |
| Standard Cabin Seats | 6 | 8 | 6 | 6 |
| Direct Operating Cost | $ 1,758 | $ 3,141 | — | $ 793 |
| Flight Deck (Base Spec) | Prodigy Touch (G3000) | Rockwell Collins Pro Line Fusion | Rockwell Collins Pro Line 21 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 464 | 542 | 400 | 290 |
| Base Aircraft Price (USD) | $9,650,000 | $20,995,000 | $ 7,695,000 | $5,350,000 |
| Flight Rules | — | — | IFR | IFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Flushing | 1 Enclosed Belted Flushing | No | Optional |
| Min Crew | 1 | 2 | 1 | 1 |
| Crew Rest | No | No | — | — |
| Jump Seat | No | No | — | — |
| Total Seats | 9 | 10 | 8 | 8 |
| Galley Location | FWD | FWD | — | — |
| Max Cabin Seats | 9 | 12 | 7 | 9 |
| Lavatory Location | AFT | AFT | — | FWD |
| Cabin Pressure (psi) | 9.4 | 9.7 | 9 | 5.8 |
| Galley / Refreshment | Galley | Galley | No | No |
| Standard Cabin Seats | 7 | 8 | 6 | 6 |
| SL Cabin Altitude (ft) | 25560 | 27140 | 24000 | 13100 |
| Connectivity | — | Gogo AVANCE L5 | — | — |
| Max Cabin Altitude (ft) | — | 5800 | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Canada PW535E1 | HTF7500E | PT6A–66B | PT6E-67XP |
| TBO (hrs) | 5000 | On-Condition | 3600 | 5000 |
| Flat Rating | ISA + 15 | ISA + 18 | ISA + 28 | ISA + 35 |
| Thrust (lbs) | 3360 | 7528 | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Burn (lbph) | 757 | — | — | — |
| Fuel Capacity (gal) | — | 1963 | — | — |
| Horsepower | — | — | 850 | 1200 |
| Fuel Burn (gph) | — | — | 100 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 51.2 | 68.1 | 47.3 | 47.25 |
| Wingspan (ft) | 52.16 | 70.5 | 47.1 | 53.33 |
| Aisle Step (ft) | 0.3 | Flat Floor | — | — |
| Cabin Width (ft) | 5.1 | 6.8 | 6.1 | 5 |
| Cabin Height (ft) | 4.9 | 6 | 5.8 | 4.9 |
| Cabin Length (ft) | 17.2 | 24.1 | 14.9 | 16.9 |
| Overall Height (ft) | 16.75 | 21 | 13.1 | 14 |
| Cabin Width - Floor (ft) | 3.6 | 4.7 | 3.5 | 4.25 |
| Cabin Length - Seating (ft) | 14.8 | 21.3 | — | — |
| Baggage Volume Ext. (cu. ft) | 74 | 110 | — | — |
| Baggage Volume Int. (cu. ft) | 10 | 45 | 35.2 | 40 |