Airbus Helicopters H225 vs Bombardier Global 7500 vs Pilatus Pc 24 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large, twin‑engine helicopters designed for offshore, search‑and‑rescue, and utility transport; they trade speed and range for vertical lift and point‑to‑point access. Typical passenger loads are roughly 16–19 for an H225 and about 19 for an S‑92 in high‑density seating, with ranges commonly in the 450–550 nautical mile class depending on payload, reserves, and configuration. The Bombardier Global 7500 is an ultra‑long‑range business jet optimized for intercontinental travel, offering by far the longest range of the group at about 7,700 nautical miles and typically carrying around 8–19 passengers depending on cabin layout. The Pilatus PC‑24 is a light business jet positioned between the helicopters and the Global 7500 in both mission and capability, with a range around 2,000 nautical miles and typical seating for about 6–10 passengers (up to more in commuter-style layouts). Overall, the Global 7500 leads in range and cabin space, the PC‑24 balances versatility and runway flexibility, and the H225/S‑92 prioritize access to remote or confined sites.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 6 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Pilatus | Sikorsky |
| Aircraft Name | H225 | Global 7500 | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 2076 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 6680 | 7417 |
| Standard Cabin Seats | 19 | 12 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 440 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $11,800,000 | $30,650,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 14 | 6 | 21 |
| Max Cabin Seats | 28 | 19 | 10 | 19 |
| Standard Cabin Seats | 19 | 12 | 6 | 19 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Flushing | — |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | FWD | — |
| Galley / Refreshment | — | Galley | Optional Refreshment Center | — |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cargo Door | — | — | Yes | — |
| Cabin Pressure (psi) | — | — | 9.3 | — |
| SL Cabin Altitude (ft) | — | — | 23500 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 5000 | 4000 |
| Horsepower | 2100 | — | — | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 15 | ISA + 23 | — |
| Thrust (lbs) | — | 18920 | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 52.2 | — |
| Overall Height (ft) | 16.3 | 27 | 17.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 775 |
| Wingspan (ft) | — | 104 | 55.8 | — |
| Cabin Width (ft) | — | 8 | 5.6 | — |
| Cabin Height (ft) | — | 6.2 | 5.1 | — |
| Cabin Length (ft) | — | 54.5 | 23 | — |
| Aisle Step (ft) | — | — | Flat Floor | — |
| Cabin Width - Floor (ft) | — | — | 3.8 | — |
| Cabin Length - Seating (ft) | — | — | 17 | — |
| Baggage Volume Int. (cu. ft) | — | — | 90 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |