Embraer Phenom 100ev vs Embraer Phenom 300e vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Piper M600 Sls
By category, the Embraer Phenom 100EV is a very light jet, the Phenom 300E is a light jet, the Piaggio Avanti EVO is a high-speed twin‑turboprop, the Pilatus PC‑12 NGX is a single‑engine turboprop utility aircraft, and the Piper M600 SLS is a single‑engine turboprop personal/owner‑pilot aircraft. On range, the Phenom 100EV is typically around 1,100–1,200 nm, the Phenom 300E about 1,900–2,000 nm, the Avanti EVO roughly 1,700–1,800 nm, the PC‑12 NGX around 1,700–1,800 nm, and the M600 SLS about 1,400–1,500 nm, with real-world range varying by payload, winds, and reserves. For passenger capacity, the Phenom 100EV usually seats 4–6 in the cabin (often marketed up to 7 including optional arrangements), the Phenom 300E generally 6–8, the Avanti EVO commonly 7–9, the PC‑12 NGX typically 6–9 with flexible cabin layouts (and higher maximum seating in airline-style configs), and the M600 SLS usually 4–6.
| Spec | Embraer Phenom 100EV | Embraer Phenom 300E | Piaggio Avanti EVO | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|---|
| Summary | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 2.84 | $ 3.88 | — | $ 2.78 | $ 2.19 |
| Min Crew | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 7 | 10 | 8 | 8 | 6 |
| Manufacturer | Embraer | Embraer | Piaggio | Pilatus | Piper |
| Aircraft Name | Phenom 100EV | Phenom 300E | Avanti EVO | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1,178 | 2,010 | 1530 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.71 | $ 0.55 | — | $ 0.46 | $ 0.55 |
| Max Cabin Seats | 7 | 10 | 7 | 9 | — |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3451 | 6914 | 3775 | — | 2200 |
| Standard Cabin Seats | 5 | 6 | 6 | 6 | 4 |
| Direct Operating Cost | $ 1,152 | $ 1,758 | — | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Prodigy Touch (G3000) | Prodigy Touch (G3000) | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 406 | 464 | 400 | 290 | 274 |
| Base Aircraft Price (USD) | $4,250,000 | $9,650,000 | $ 7,695,000 | $5,350,000 | $3,081,400 |
| Flight Rules | — | — | IFR | IFR | IFR |
| Cabin | |||||
| Cockpit | 2 | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Enclosed Flushing | No | Optional | No |
| Min Crew | 1 | 1 | 1 | 1 | 1 |
| Crew Rest | No | No | — | — | — |
| Jump Seat | No | No | — | — | — |
| Total Seats | 6 | 9 | 8 | 8 | 5 |
| Max Cabin Seats | 6 | 9 | 7 | 9 | — |
| Lavatory Location | AFT | AFT | — | FWD | — |
| Cabin Pressure (psi) | 8.3 | 9.4 | 9 | 5.8 | 5.6 |
| Galley / Refreshment | No | Galley | No | No | Refreshment Centre |
| Standard Cabin Seats | 4 | 7 | 6 | 6 | 4 |
| SL Cabin Altitude (ft) | 21280 | 25560 | 24000 | 13100 | 12600 |
| Galley Location | — | FWD | — | — | MID |
| Max Cabin Altitude (ft) | — | — | 6600 | — | 8644 |
| Cargo Door | — | — | — | Yes | — |
| Engine | |||||
| FADEC | Yes | Yes | Yes | Yes | No |
| Model | PW617F1-E | Canada PW535E1 | PT6A–66B | PT6E-67XP | PT6A-42A |
| TBO (hrs) | 3500 | 5000 | 3600 | 5000 | 3600 |
| Flat Rating | ISA + 8 | ISA + 15 | ISA + 28 | ISA + 35 | ISA + 55 |
| Thrust (lbs) | 1730 | 3360 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 1 | 1 |
| Fuel Burn (lbph) | 543 | 757 | — | — | — |
| Horsepower | — | — | 850 | 1200 | 600 |
| Fuel Burn (gph) | — | — | 100 | — | — |
| Usable Fuel (gal) | — | — | — | 402 | — |
| Fuel Capacity (gal) | — | — | — | — | 260 |
| Dimensions | |||||
| Length (ft) | 42.1 | 51.2 | 47.3 | 47.25 | 29.7 |
| Wingspan (ft) | 40.4 | 52.16 | 47.1 | 53.33 | 43.2 |
| Aisle Step (ft) | 0.3 | 0.3 | — | — | — |
| Cabin Width (ft) | 5.1 | 5.1 | 6.1 | 5 | 4.1 |
| Cabin Height (ft) | 4.9 | 4.9 | 5.8 | 4.9 | 4 |
| Cabin Length (ft) | 11 | 17.2 | 14.9 | 16.9 | 12.3 |
| Overall Height (ft) | 14.3 | 16.75 | 13.1 | 14 | 11.3 |
| 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 | 20 |
| Cabin Volume (cu. ft) | — | — | — | — | 165 |