Gulfstream G700 vs Leonardo Aw189 vs Piaggio Avanti Evo vs Piper M600 Sls
The Gulfstream G700 is a long‑range, large‑cabin business jet designed for intercontinental travel. It offers the greatest range of the four at roughly 7,500 nautical miles and typically accommodates about 13 to 19 passengers depending on cabin configuration. The Leonardo (Agusta) AW189 is a super‑medium twin‑engine helicopter optimized for offshore, SAR, and utility missions rather than high‑altitude cruise. Its range is far shorter than the jets and turboprops, generally on the order of roughly 450 to 500+ nautical miles with typical reserves, and it commonly carries around 16 to 19 passengers in a transport layout. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft positioned between light jets and larger turboprops. It typically carries about 6 to 9 passengers and offers mid‑range capability around roughly 1,500 to 1,800 nautical miles. The Piper M600 SLS is a single‑engine pressurized turboprop aimed at owner‑operators. It is the smallest here, usually seating 5 to 6 passengers, with a range around roughly 1,400 to 1,500 nautical miles.
| Spec | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 1 |
| Total Seats | 16 | 21 | 8 | 6 |
| Manufacturer | Gulfstream | Leonardo | Piaggio | Piper |
| Aircraft Name | G700 | AW189 | Avanti EVO | M600 |
| Certification | In Development | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7500 | 651 | 1530 | 1406 |
| Max Cabin Seats | 19 | 19 | 7 | — |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | VERIFIED |
| Standard Cabin Seats | 12 | 19 | 6 | 4 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 516 | 155 | 400 | 274 |
| Base Aircraft Price (USD) | $78,000,000 | $2,413,000 | $ 7,695,000 | $3,081,400 |
| DOC / nm | — | $ 15.57 | — | $ 2.19 |
| Flight Rules | — | IFR | IFR | IFR |
| DOC / nm / Seat | — | $ 0.74 | — | $ 0.55 |
| Direct Operating Cost | — | $ 2,413 | — | $ 603 |
| Useful Load (lbs) | — | — | 3775 | 2200 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 1 |
| Crew Rest | Optional | — | — | — |
| Jump Seat | Yes | — | — | — |
| Total Seats | 16 | 21 | 8 | 5 |
| Galley Location | FWD | — | — | MID |
| Max Cabin Seats | 19 | 19 | 7 | — |
| Lavatory Location | FWD / AFT | — | — | — |
| Standard Cabin Seats | 12 | 19 | 6 | 4 |
| Lavatory | — | — | No | No |
| Cabin Pressure (psi) | — | — | 9 | 5.6 |
| Galley / Refreshment | — | — | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| Model | Pearl 700 | CT7-2E1 | PT6A–66B | PT6A-42A |
| TBO (hrs) | On Condition | 4000 | 3600 | 3600 |
| Thrust (lbs) | 18250 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 1 |
| FADEC | — | Yes | Yes | No |
| Fuel Type | — | JetFuel | — | — |
| Horsepower | — | 1983 | 850 | 600 |
| Flat Rating | — | — | ISA + 28 | ISA + 55 |
| Fuel Burn (gph) | — | — | 100 | — |
| Fuel Capacity (gal) | — | — | — | 260 |
| Dimensions | ||||
| Length (ft) | 109.9 | 57.8 | 47.3 | 29.7 |
| Wingspan (ft) | 103 | — | 47.1 | 43.2 |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 8.2 | — | 6.1 | 4.1 |
| Cabin Height (ft) | 6.25 | — | 5.8 | 4 |
| Cabin Length (ft) | 56.9 | — | 14.9 | 12.3 |
| Overall Height (ft) | 25.4 | 16.6 | 13.1 | 11.3 |
| Baggage Volume Int. (cu. ft) | 195 | — | 35.2 | 20 |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | — | 165 |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | — |
| Cabin Width - Floor (ft) | — | — | 3.5 | — |