Gulfstream G280 vs Gulfstream G650er vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Gulfstream G280 and G650ER are long-range business jets, while the Pilatus PC-12 NGX is a single‑engine turboprop and the PC-24 is a light jet. In category and capability, the G650ER sits at the top as an ultra‑long‑range, large‑cabin jet designed for intercontinental missions, offering roughly 7,500 nautical miles of range and typically carrying about 12–16 passengers. The G280 is a super‑midsize jet aimed at transcontinental flying, with about 3,600 nautical miles of range and a typical capacity around 8–10 passengers. The PC-12 NGX prioritizes efficiency and access to shorter or less‑developed runways; it generally carries about 6–9 passengers (up to 10 in some layouts) with roughly 1,800 nautical miles of range. The PC-24 bridges utility and jet speed as a light jet with semi‑rugged operational flexibility; it typically seats about 6–10 passengers and offers around 2,000 nautical miles of range.
| Spec | Gulfstream G280 | Gulfstream G650ER | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 6.57 | $ 9.39 | $ 2.78 | $ 3.71 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 10 | 14 | 8 | 6 |
| Manufacturer | Gulfstream | Gulfstream | Pilatus | Pilatus |
| Aircraft Name | G280 | G650ER | PC-12 NGX | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 3600 | 7500 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.82 | $ 0.78 | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 10 | 19 | 9 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 15550 | 49500 | — | 6680 |
| Standard Cabin Seats | 8 | 12 | 6 | 6 |
| Direct Operating Cost | $ 3,168 | $ 4,844 | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Gulfstream PlaneView (Pro Line Fusion) | Gulfstream PlaneView II (Primus Epic) | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 481 | 516 | 290 | 440 |
| Base Aircraft Price (USD) | $24,900,000 | $60,000,000 | $5,350,000 | $11,800,000 |
| Flight Rules | — | — | IFR | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | 2 Enclosed Flushing | Optional | 1 Enclosed Flushing |
| Min Crew | 2 | 4 | 1 | 1 |
| Crew Rest | No | Yes | — | No |
| Jump Seat | No | Yes | — | No |
| Total Seats | 10 | 14 | 8 | 6 |
| Galley Location | FWD | FWD | — | FWD |
| Max Cabin Seats | 10 | 19 | 9 | 10 |
| Lavatory Location | AFT | FWD / AFT | FWD | FWD |
| Cabin Pressure (psi) | 9.2 | 10.7 | 5.8 | 9.3 |
| Galley / Refreshment | Galley | Galley | No | Optional Refreshment Center |
| Standard Cabin Seats | 8 | 12 | 6 | 6 |
| SL Cabin Altitude (ft) | 25000 | 31900 | 13100 | 23500 |
| Max Cabin Altitude (ft) | 5800 | — | — | — |
| Cargo Door | — | — | Yes | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | HTF7250G | BR725 A1-12 | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | On-Condition | On-Condition | 5000 | 5000 |
| Flat Rating | ISA + 17 | ISA + 15 | ISA + 35 | ISA + 23 |
| Thrust (lbs) | 7624 | 16900 | — | 3435 |
| No. of Engines | 2 | 2 | 1 | 2 |
| Horsepower | — | — | 1200 | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 66.9 | 99.8 | 47.25 | 52.2 |
| Wingspan (ft) | 63 | 99.6 | 53.33 | 55.8 |
| Aisle Step (ft) | 0.3 | Flat Floor | — | Flat Floor |
| Cabin Width (ft) | 6.9 | 8.2 | 5 | 5.6 |
| Cabin Height (ft) | 6.3 | 6.5 | 4.9 | 5.1 |
| Cabin Length (ft) | 25.9 | 46.9 | 16.9 | 23 |
| Overall Height (ft) | 21.4 | 25.7 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 5.4 | 6.7 | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | 17.7 | 32.7 | — | 17 |
| Baggage Volume Int. (cu. ft) | 154 | 235 | 40 | 90 |