Gulfstream G700 vs Leonardo Aw189 vs Piper M600 Sls vs Sikorsky S 92
The Gulfstream G700 is a long-range, large-cabin business jet designed for intercontinental travel, offering roughly 7,000–7,500 nautical miles of range and typically seating about 12–19 passengers in executive configurations (with higher-density layouts possible). The Piper M600 SLS is a single‑engine turboprop aimed at owner-operators and short to mid-range missions, with about 1,400 nautical miles of range and seating for up to 6. The Leonardo (Agusta) AW189 is a super‑medium twin‑engine helicopter optimized for offshore, SAR, and utility roles; it typically carries about 16–19 passengers and has a practical range on the order of ~450–500 nautical miles depending on fit and reserves. The Sikorsky S‑92 is a larger heavy/medium-lift twin helicopter widely used for offshore transport and SAR; it commonly seats around 19 passengers and offers a broadly similar helicopter-class range, often ~500 nautical miles depending on configuration. In summary, the G700 dominates range and cabin comfort for point-to-point global travel, the M600 emphasizes efficiency and simplicity, and the AW189 and S‑92 trade speed and range for vertical lift and mission flexibility.
| Spec | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 2 |
| Total Seats | 16 | 21 | 6 | 21 |
| Manufacturer | Gulfstream | Leonardo | Piper | Sikorsky |
| Aircraft Name | G700 | AW189 | M600 | S-92 |
| Certification | In Development | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7500 | 651 | 1406 | 439 |
| Max Cabin Seats | 19 | 19 | — | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Standard Cabin Seats | 12 | 19 | 4 | 19 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | EFIS | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 516 | 155 | 274 | 155 |
| Base Aircraft Price (USD) | $78,000,000 | $2,413,000 | $3,081,400 | $30,650,000 |
| DOC / nm | — | $ 15.57 | $ 2.19 | $ 19.79 |
| Flight Rules | — | IFR | IFR | IFR |
| DOC / nm / Seat | — | $ 0.74 | $ 0.55 | $ 0.94 |
| Direct Operating Cost | — | $ 2,413 | $ 603 | $ 3,068 |
| Useful Load (lbs) | — | — | 2200 | 7417 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 2 |
| Crew Rest | Optional | — | — | — |
| Jump Seat | Yes | — | — | — |
| Total Seats | 16 | 21 | 5 | 21 |
| Galley Location | FWD | — | MID | — |
| Max Cabin Seats | 19 | 19 | — | 19 |
| Lavatory Location | FWD / AFT | — | — | — |
| Standard Cabin Seats | 12 | 19 | 4 | 19 |
| Lavatory | — | — | No | — |
| Cabin Pressure (psi) | — | — | 5.6 | — |
| Galley / Refreshment | — | — | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | — | 12600 | — |
| Max Cabin Altitude (ft) | — | — | 8644 | — |
| Engine | ||||
| Model | Pearl 700 | CT7-2E1 | PT6A-42A | CT7-8A |
| TBO (hrs) | On Condition | 4000 | 3600 | 4000 |
| Thrust (lbs) | 18250 | — | — | — |
| No. of Engines | 2 | 2 | 1 | 1 |
| FADEC | — | Yes | No | Yes |
| Fuel Type | — | JetFuel | — | JetFuel |
| Horsepower | — | 1983 | 600 | 2520 |
| Flat Rating | — | — | ISA + 55 | — |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Dimensions | ||||
| Length (ft) | 109.9 | 57.8 | 29.7 | — |
| Wingspan (ft) | 103 | — | 43.2 | — |
| Aisle Step (ft) | Flat Floor | — | — | — |
| Cabin Width (ft) | 8.2 | — | 4.1 | — |
| Cabin Height (ft) | 6.25 | — | 4 | — |
| Cabin Length (ft) | 56.9 | — | 12.3 | — |
| Overall Height (ft) | 25.4 | 16.6 | 11.3 | 17.8 |
| Baggage Volume Int. (cu. ft) | 195 | — | 20 | — |
| Rotor Diameter (ft) | — | 48 | — | — |
| Cabin Volume (cu. ft) | — | 395 | 165 | 775 |
| Baggage Volume Ext. (cu. ft) | — | 85 | — | 140 |