Airbus Helicopters H225 vs Bombardier Global 7500 vs Cessna Citation Xls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are twin‑engine heavy helicopters primarily used for offshore transport, search and rescue, and utility missions, while the Bombardier Global 7500 and Cessna Citation XLS+ are fixed‑wing business jets designed for point‑to‑point travel. In range terms, the Global 7500 is in a different class, offering ultra‑long‑range intercontinental capability around 7,700 nautical miles. The Citation XLS+ is a midsize business jet with a typical range around 2,100 nautical miles, suited to regional and transcontinental U.S. trips. Helicopter ranges are much shorter: the H225 is roughly in the 500–700 nautical mile class depending on configuration and reserves, and the S‑92 is similar, commonly around 500–600 nautical miles. Passenger capacity also reflects the mission: the Global 7500 typically seats about 14–19, the Citation XLS+ usually about 7–9, and both the H225 and S‑92 can carry larger cabin loads, often configured for roughly 16–19 passengers in offshore transport layouts.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Cessna Citation XLS+ | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 5.34 | $ 19.79 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 10 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Cessna Citation | Sikorsky |
| Aircraft Name | H225 | Global 7500 | XLS+ | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1906 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.67 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7540 | 7417 |
| Standard Cabin Seats | 19 | 12 | 8 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,303 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 430 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $15,500,000 | $30,650,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 10 | 21 |
| Max Cabin Seats | 28 | 19 | 9 | 19 |
| Standard Cabin Seats | 19 | 12 | 8 | 19 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | AFT | — |
| Galley / Refreshment | — | Galley | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 9.3 | — |
| SL Cabin Altitude (ft) | — | — | 25230 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW545C | 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 + 10 | — |
| Thrust (lbs) | — | 18920 | 4119 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 52.5 | — |
| Overall Height (ft) | 16.3 | 27 | 17.2 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 775 |
| Wingspan (ft) | — | 104 | 56.3 | — |
| Cabin Width (ft) | — | 8 | 5.5 | — |
| Cabin Height (ft) | — | 6.2 | 5.7 | — |
| Cabin Length (ft) | — | 54.5 | 18.5 | — |
| Aisle Step (ft) | — | — | 0.7 | — |
| Cabin Width - Floor (ft) | — | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 80 | 140 |
| Baggage Volume Int. (cu. ft) | — | — | 10 | — |