Airbus Helicopters H225 vs Gulfstream G700 vs Piper M600 Sls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are twin‑engine heavy helicopters optimized for offshore transport and utility missions rather than long overland cruise. Typical range is roughly 500–600 nautical miles depending on payload and reserves, and they generally carry about 18–19 passengers in high‑density layouts, with more spacious executive or SAR configurations reducing seats. The Gulfstream G700 is a long‑range, large‑cabin business jet built for intercontinental travel. It offers an ultra‑long range on the order of about 7,000+ nautical miles and typically carries around 13–19 passengers in executive layouts, emphasizing comfort, speed, and nonstop city‑pair capability. The Piper M600 SLS is a single‑engine turboprop in the personal/light business category. Its range is roughly 1,000–1,500 nautical miles, and it usually seats up to six occupants, trading cabin size and payload for lower operating complexity and access to shorter runways than large jets. Overall, the helicopters prioritize vertical access and cabin utility at moderate range, the G700 maximizes range and cabin comfort, and the M600 SLS targets efficient regional travel with a small passenger load.
| Spec | AIRBUS H225 | Gulfstream G700 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 16 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Gulfstream | Piper | Sikorsky |
| Aircraft Name | H225 | G700 | M600 | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 1406 | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | — | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 2200 | 7417 |
| Standard Cabin Seats | 19 | 12 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 274 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $3,081,400 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 21 | 16 | 5 | 21 |
| Max Cabin Seats | 28 | 19 | — | 19 |
| Standard Cabin Seats | 19 | 12 | 4 | 19 |
| Crew Rest | — | Optional | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | MID | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Lavatory | — | — | No | — |
| Cabin Pressure (psi) | — | — | 5.6 | — |
| Galley / Refreshment | — | — | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | — | 12600 | — |
| Max Cabin Altitude (ft) | — | — | 8644 | — |
| Engine | ||||
| FADEC | Yes | — | No | Yes |
| Model | Makila 2A1 | Pearl 700 | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On Condition | 3600 | 4000 |
| Horsepower | 2100 | — | 600 | 2520 |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 | 760 |
| Thrust (lbs) | — | 18250 | — | — |
| Flat Rating | — | — | ISA + 55 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 109.9 | 29.7 | — |
| Overall Height (ft) | 16.3 | 25.4 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 | 775 |
| 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 | — |
| Baggage Volume Int. (cu. ft) | — | 195 | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |