Airbus Helicopters H225 vs Bombardier Global 7500 vs Piper M600 Sls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters built for offshore transport, search and rescue, and utility missions. They trade speed and range for vertical lift and hover capability, typically carrying around 18 to 19 passengers in high‑density seating (often fewer in executive or SAR layouts) and offering practical ranges on the order of a few hundred nautical miles, depending heavily on payload, reserves, and mission profile. The Bombardier Global 7500 is an ultra‑long‑range business jet optimized for intercontinental travel. It carries about 14 to 19 passengers in typical executive configurations (with higher maximum capacity depending on layout) and has a published range around 7,700 nautical miles, enabling nonstop city pairs across oceans. The Piper M600 SLS is a single‑engine turboprop, best viewed as a high‑performance personal or small business aircraft. It typically seats about 5 to 6 passengers and has a range roughly around 1,400 to 1,700 nautical miles, suited to regional point‑to‑point trips rather than long‑haul missions.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Piper | Sikorsky |
| Aircraft Name | H225 | Global 7500 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1406 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 2200 | 7417 |
| Standard Cabin Seats | 19 | 12 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 274 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $3,081,400 | $30,650,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 5 | 21 |
| Max Cabin Seats | 28 | 19 | — | 19 |
| Standard Cabin Seats | 19 | 12 | 4 | 19 |
| Lavatory | — | 2 Enclosed Flushing | No | — |
| Crew Rest | — | Yes | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | MID | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Galley / Refreshment | — | Galley | Refreshment Centre | — |
| Max Cabin Altitude (ft) | — | 4500 | 8644 | — |
| Cabin Pressure (psi) | — | — | 5.6 | — |
| SL Cabin Altitude (ft) | — | — | 12600 | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | Makila 2A1 | Passport | 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 |
| Flat Rating | — | ISA + 15 | ISA + 55 | — |
| Thrust (lbs) | — | 18920 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 29.7 | — |
| Overall Height (ft) | 16.3 | 27 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 | 775 |
| Wingspan (ft) | — | 104 | 43.2 | — |
| Cabin Width (ft) | — | 8 | 4.1 | — |
| Cabin Height (ft) | — | 6.2 | 4 | — |
| Cabin Length (ft) | — | 54.5 | 12.3 | — |
| Baggage Volume Int. (cu. ft) | — | — | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |