Gulfstream G700 vs Leonardo Aw189 vs Piaggio Avanti Evo vs Pilatus Pc 24
The Gulfstream G700 is a long‑range ultra‑long‑haul business jet designed for intercontinental travel, typically carrying around 12–19 passengers (and certified for more) with a range of roughly 7,500 nautical miles. The Leonardo (Agusta) AW189 is a medium twin‑engine helicopter optimized for offshore, SAR, and utility/VIP roles; it generally carries about 16–19 passengers in high‑density layouts, but its practical range is far shorter than the jets, typically a few hundred nautical miles depending on payload and reserves. The Piaggio P.180 Avanti EVO is a high‑speed twin‑turboprop business aircraft, usually configured for about 7–9 passengers, offering midrange capability around 1,500–1,800 nautical miles. The Pilatus PC‑24 is a light “super versatile” business jet with strong short/rough‑field capability; it commonly seats about 6–10 passengers and has a range around 2,000 nautical miles. Overall, the G700 leads in range and cabin size, the AW189 trades speed and range for vertical access, the Avanti EVO emphasizes efficient turboprop speed, and the PC‑24 balances jet performance with exceptional airport flexibility.
| Spec | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 1 |
| Total Seats | 16 | 21 | 8 | 6 |
| Manufacturer | Gulfstream | Leonardo | Piaggio | Pilatus |
| Aircraft Name | G700 | AW189 | Avanti EVO | PC-24 |
| Certification | In Development | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7500 | 651 | 1530 | 2076 |
| Max Cabin Seats | 19 | 19 | 7 | 10 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Standard Cabin Seats | 12 | 19 | 6 | 6 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 516 | 155 | 400 | 440 |
| Base Aircraft Price (USD) | $78,000,000 | $2,413,000 | $ 7,695,000 | $11,800,000 |
| DOC / nm | — | $ 15.57 | — | $ 3.71 |
| Flight Rules | — | IFR | IFR | — |
| DOC / nm / Seat | — | $ 0.74 | — | $ 0.62 |
| Direct Operating Cost | — | $ 2,413 | — | $ 1,619 |
| Useful Load (lbs) | — | — | 3775 | 6680 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 1 |
| Crew Rest | Optional | — | — | No |
| Jump Seat | Yes | — | — | No |
| Total Seats | 16 | 21 | 8 | 6 |
| Galley Location | FWD | — | — | FWD |
| Max Cabin Seats | 19 | 19 | 7 | 10 |
| Lavatory Location | FWD / AFT | — | — | FWD |
| Standard Cabin Seats | 12 | 19 | 6 | 6 |
| Lavatory | — | — | No | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | — | 9 | 9.3 |
| Galley / Refreshment | — | — | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| Model | Pearl 700 | CT7-2E1 | PT6A–66B | FJ44-4A-QPM |
| TBO (hrs) | On Condition | 4000 | 3600 | 5000 |
| Thrust (lbs) | 18250 | — | — | 3435 |
| No. of Engines | 2 | 2 | 2 | 2 |
| FADEC | — | Yes | Yes | Yes |
| Fuel Type | — | JetFuel | — | — |
| Horsepower | — | 1983 | 850 | — |
| Flat Rating | — | — | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 109.9 | 57.8 | 47.3 | 52.2 |
| Wingspan (ft) | 103 | — | 47.1 | 55.8 |
| Aisle Step (ft) | Flat Floor | — | — | Flat Floor |
| Cabin Width (ft) | 8.2 | — | 6.1 | 5.6 |
| Cabin Height (ft) | 6.25 | — | 5.8 | 5.1 |
| Cabin Length (ft) | 56.9 | — | 14.9 | 23 |
| Overall Height (ft) | 25.4 | 16.6 | 13.1 | 17.4 |
| Baggage Volume Int. (cu. ft) | 195 | — | 35.2 | 90 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | — |
| Cabin Width - Floor (ft) | — | — | 3.5 | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |