Cessna Citation Cj4 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Cessna Citation CJ4 and Pilatus PC-24 are light jets, the Piaggio Avanti EVO is a twin‑turboprop with jet-like cruising characteristics, and the Pilatus PC-12 NGX is a single‑engine turboprop utility aircraft. In range, the CJ4 typically offers roughly 2,000 nautical miles class capability, the Avanti EVO is generally in the high‑1,000s to about 2,000 nautical miles, the PC-12 NGX is commonly around the 1,700–1,800 nautical mile range depending on reserves and load, and the PC-24 is often cited around 2,000 nautical miles, varying with passenger count and mission profile. For passenger capacity, the CJ4 is usually configured for about 7–8 passengers, the Avanti EVO commonly seats around 7–9 in executive layouts, the PC-12 NGX typically carries about 6–9 in comfort (with higher-density options), and the PC-24 is often arranged for about 6–10 passengers. Overall, the CJ4 emphasizes efficient light-jet travel, the Avanti EVO targets fast turboprop economics, the PC-12 NGX prioritizes versatility and short/rough-field utility, and the PC-24 blends light-jet speed with strong runway flexibility.
| Spec | Cessna Citation CJ4 | Piaggio Avanti EVO | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.37 | — | $ 2.78 | $ 3.71 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 9 | 8 | 8 | 6 |
| Manufacturer | Cessna Citation | Piaggio | Pilatus | Pilatus |
| Aircraft Name | CJ4 | Avanti EVO | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 2170 | 1530 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.62 | — | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 8 | 7 | 9 | 10 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6914 | 3775 | — | 6680 |
| Standard Cabin Seats | 7 | 6 | 6 | 6 |
| Direct Operating Cost | $ 1,970 | — | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 440 | 400 | 290 | 440 |
| Base Aircraft Price (USD) | $11,290,000 | $ 7,695,000 | $5,350,000 | $11,800,000 |
| Flight Rules | — | IFR | IFR | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | Optional | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 1 |
| Crew Rest | No | — | — | No |
| Jump Seat | No | — | — | No |
| Total Seats | 9 | 8 | 8 | 6 |
| Galley Location | FWD | — | — | FWD |
| Max Cabin Seats | 8 | 7 | 9 | 10 |
| Lavatory Location | AFT | — | FWD | FWD |
| Cabin Pressure (psi) | 9 | 9 | 5.8 | 9.3 |
| Galley / Refreshment | Galley | No | No | Optional Refreshment Center |
| Standard Cabin Seats | 7 | 6 | 6 | 6 |
| SL Cabin Altitude (ft) | 24005 | 24000 | 13100 | 23500 |
| Max Cabin Altitude (ft) | — | 6600 | — | — |
| Cargo Door | — | — | Yes | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | FJ44-4A | PT6A–66B | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | 5000 | 3600 | 5000 | 5000 |
| Flat Rating | ISA + 11 | ISA + 28 | ISA + 35 | ISA + 23 |
| Thrust (lbs) | 3621 | — | — | 3435 |
| No. of Engines | 2 | 2 | 1 | 2 |
| Fuel Burn (lbph) | 757 | — | — | — |
| Fuel Capacity (gal) | 870 | — | — | — |
| Horsepower | — | 850 | 1200 | — |
| Fuel Burn (gph) | — | 100 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 53.4 | 47.3 | 47.25 | 52.2 |
| Wingspan (ft) | 50 | 47.1 | 53.33 | 55.8 |
| Aisle Step (ft) | 0.4 | — | — | Flat Floor |
| Cabin Width (ft) | 4.8 | 6.1 | 5 | 5.6 |
| Cabin Height (ft) | 4.8 | 5.8 | 4.9 | 5.1 |
| Cabin Length (ft) | 17.2 | 14.9 | 16.9 | 23 |
| Overall Height (ft) | 15.5 | 13.1 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 3.1 | 3.5 | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | 14.8 | — | — | 17 |
| Baggage Volume Ext. (cu. ft) | 70 | — | — | — |
| Baggage Volume Int. (cu. ft) | 7 | 35.2 | 40 | 90 |