Gulfstream G700 vs Piaggio Avanti Evo vs Piper M600 Sls vs Sikorsky S 92
The Gulfstream G700 is a long-range, large-cabin business jet designed for intercontinental missions. It offers roughly 7,500–7,750 nautical miles of range (configuration dependent) and typically carries about 13–19 passengers in executive layouts, with a maximum certified capacity higher in high-density arrangements. The Piaggio Avanti EVO is a fast twin‑turboprop with a smaller cabin and shorter legs, generally around 1,700–1,900 nautical miles of range and seating typically 6–7 passengers (up to about 9). The Piper M600 SLS is a single‑engine turboprop positioned for owner‑operators and shorter regional travel, with about 1,400–1,600 nautical miles of range and typically 5–6 passenger seats plus the pilot (about 6 total seats). The Sikorsky S‑92 is a medium twin helicopter optimized for offshore, SAR, and utility roles rather than long-range cruise; it generally ranges about 500–600 nautical miles and commonly carries around 12–19 passengers depending on configuration. Overall, the G700 leads in range and cabin size, the Avanti EVO balances speed and efficiency for regional missions, the M600 SLS is a simpler personal turboprop, and the S‑92 prioritizes vertical lift and mission flexibility over range.
| Spec | Gulfstream G700 | Piaggio Avanti EVO | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 3 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 2 |
| Total Seats | 16 | 8 | 6 | 21 |
| Manufacturer | Gulfstream | Piaggio | Piper | Sikorsky |
| Aircraft Name | G700 | Avanti EVO | M600 | S-92 |
| Certification | In Development | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7500 | 1530 | 1406 | 439 |
| Max Cabin Seats | 19 | 7 | — | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Standard Cabin Seats | 12 | 6 | 4 | 19 |
| Flight Deck (Base Spec) | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 516 | 400 | 274 | 155 |
| Base Aircraft Price (USD) | $78,000,000 | $ 7,695,000 | $3,081,400 | $30,650,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Useful Load (lbs) | — | 3775 | 2200 | 7417 |
| DOC / nm | — | — | $ 2.19 | $ 19.79 |
| DOC / nm / Seat | — | — | $ 0.55 | $ 0.94 |
| Direct Operating Cost | — | — | $ 603 | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 4 | 1 | 1 | 2 |
| Crew Rest | Optional | — | — | — |
| Jump Seat | Yes | — | — | — |
| Total Seats | 16 | 8 | 5 | 21 |
| Galley Location | FWD | — | MID | — |
| Max Cabin Seats | 19 | 7 | — | 19 |
| Lavatory Location | FWD / AFT | — | — | — |
| Standard Cabin Seats | 12 | 6 | 4 | 19 |
| 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 | PT6A–66B | PT6A-42A | CT7-8A |
| TBO (hrs) | On Condition | 3600 | 3600 | 4000 |
| Thrust (lbs) | 18250 | — | — | — |
| No. of Engines | 2 | 2 | 1 | 1 |
| FADEC | — | Yes | No | Yes |
| Horsepower | — | 850 | 600 | 2520 |
| Flat Rating | — | ISA + 28 | ISA + 55 | — |
| Fuel Burn (gph) | — | 100 | — | — |
| Fuel Capacity (gal) | — | — | 260 | 760 |
| Fuel Type | — | — | — | JetFuel |
| Dimensions | ||||
| Length (ft) | 109.9 | 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 | 13.1 | 11.3 | 17.8 |
| Baggage Volume Int. (cu. ft) | 195 | 35.2 | 20 | — |
| Cabin Width - Floor (ft) | — | 3.5 | — | — |
| Cabin Volume (cu. ft) | — | — | 165 | 775 |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |