Airbus Helicopters H225 vs Gulfstream G700 vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy twin‑engine helicopters typically used for offshore transport, search and rescue, and government missions; their practical range is generally in the roughly 450–600 nautical mile class depending on payload and reserves, and they usually carry about 16–19 passengers in airline-style seating (with higher or lower counts depending on configuration). The Gulfstream G700 is an ultra‑long‑range business jet optimized for intercontinental travel; it offers the longest range by far at about 7,500 nautical miles and typically seats around 13–19 passengers in executive layouts, with high-density configurations possible but uncommon. The Piaggio Avanti EVO is a twin‑turboprop business aircraft positioned between helicopters and large jets in speed and mission; it is suited to regional trips with a range around 1,400–1,800 nautical miles and generally seats about 6–9 passengers. Overall, the G700 leads in range and long-haul comfort, the Avanti EVO targets efficient short-to-mid routes, and the H225 and S‑92 prioritize vertical-lift access with moderate point-to-point range and robust payload.
| Spec | AIRBUS H225 | Gulfstream G700 | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 20.87 | — | — | $ 19.79 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 16 | 8 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Gulfstream | Piaggio | Sikorsky |
| Aircraft Name | H225 | G700 | Avanti EVO | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 1530 | 439 |
| DOC / nm / Seat | $ 0.99 | — | — | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 7 | 19 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 3775 | 7417 |
| Standard Cabin Seats | 19 | 12 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | — | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $ 7,695,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 16 | 8 | 21 |
| Max Cabin Seats | 28 | 19 | 7 | 19 |
| Standard Cabin Seats | 19 | 12 | 6 | 19 |
| Crew Rest | — | Optional | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Lavatory | — | — | No | — |
| Cabin Pressure (psi) | — | — | 9 | — |
| Galley / Refreshment | — | — | No | — |
| SL Cabin Altitude (ft) | — | — | 24000 | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | — | Yes | Yes |
| Model | Makila 2A1 | Pearl 700 | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On Condition | 3600 | 4000 |
| Horsepower | 2100 | — | 850 | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Thrust (lbs) | — | 18250 | — | — |
| Flat Rating | — | — | ISA + 28 | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 109.9 | 47.3 | — |
| Overall Height (ft) | 16.3 | 25.4 | 13.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 775 |
| 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 | — |
| Baggage Volume Int. (cu. ft) | — | 195 | 35.2 | — |
| Cabin Width - Floor (ft) | — | — | 3.5 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |