Gulfstream G700 vs Leonardo Aw189 vs Piaggio Avanti Evo
The Gulfstream G700 and Piaggio Avanti EVO are fixed‑wing business aircraft, while the Leonardo (Agusta) AW189 is a twin‑engine helicopter, so their strengths differ by mission. The G700 is an ultra‑long‑range business jet designed for intercontinental travel at high altitude and speed; it typically carries around 12–19 passengers depending on cabin configuration and has a range on the order of roughly 7,000+ nautical miles. The Piaggio Avanti EVO is a high‑speed turboprop optimized for efficient regional and mid‑range trips; it generally seats about 7–9 passengers and offers a range of roughly 1,500–1,800 nautical miles. The AW189 prioritizes vertical lift and access to remote or confined sites (offshore platforms, hoist/SAR, VIP shuttle); it commonly carries about 16–19 passengers in a high‑density layout (fewer in VIP/missionized roles) and has a range roughly in the 450–500 nautical mile class, varying with payload and reserves. In short, the G700 dominates for nonstop global reach, the Avanti EVO for efficient point‑to‑point regional flying, and the AW189 for places runways can’t reach.
| Spec | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 3 | 2 | 2 |
| Min Crew | 4 | 1 | 1 |
| Total Seats | 16 | 21 | 8 |
| Manufacturer | Gulfstream | Leonardo | Piaggio |
| Aircraft Name | G700 | AW189 | Avanti EVO |
| Certification | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7500 | 651 | 1530 |
| Max Cabin Seats | 19 | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Standard Cabin Seats | 12 | 19 | 6 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 516 | 155 | 400 |
| Base Aircraft Price (USD) | $78,000,000 | $2,413,000 | $ 7,695,000 |
| DOC / nm | — | $ 15.57 | — |
| Flight Rules | — | IFR | IFR |
| DOC / nm / Seat | — | $ 0.74 | — |
| Direct Operating Cost | — | $ 2,413 | — |
| Useful Load (lbs) | — | — | 3775 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 |
| Crew Rest | Optional | — | — |
| Jump Seat | Yes | — | — |
| Total Seats | 16 | 21 | 8 |
| Galley Location | FWD | — | — |
| Max Cabin Seats | 19 | 19 | 7 |
| Lavatory Location | FWD / AFT | — | — |
| Standard Cabin Seats | 12 | 19 | 6 |
| Lavatory | — | — | No |
| Cabin Pressure (psi) | — | — | 9 |
| Galley / Refreshment | — | — | No |
| SL Cabin Altitude (ft) | — | — | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| Model | Pearl 700 | CT7-2E1 | PT6A–66B |
| TBO (hrs) | On Condition | 4000 | 3600 |
| Thrust (lbs) | 18250 | — | — |
| No. of Engines | 2 | 2 | 2 |
| FADEC | — | Yes | Yes |
| Fuel Type | — | JetFuel | — |
| Horsepower | — | 1983 | 850 |
| Flat Rating | — | — | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 109.9 | 57.8 | 47.3 |
| Wingspan (ft) | 103 | — | 47.1 |
| Aisle Step (ft) | Flat Floor | — | — |
| Cabin Width (ft) | 8.2 | — | 6.1 |
| Cabin Height (ft) | 6.25 | — | 5.8 |
| Cabin Length (ft) | 56.9 | — | 14.9 |
| Overall Height (ft) | 25.4 | 16.6 | 13.1 |
| Baggage Volume Int. (cu. ft) | 195 | — | 35.2 |
| Rotor Diameter (ft) | — | 48 | — |
| Cabin Volume (cu. ft) | — | 395 | — |
| Baggage Volume Ext. (cu. ft) | — | 85 | — |
| Cabin Width - Floor (ft) | — | — | 3.5 |