Airbus Helicopters H225 vs Cessna Citation Xls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters designed for offshore transport and search-and-rescue roles, while the Cessna Citation XLS+ is a super‑light/midsize business jet optimized for fast point‑to‑point travel between airports. In range, the Citation XLS+ typically offers the longest practical trip capability, commonly around 2,000 nautical miles depending on payload and conditions, whereas the H225 and S-92 are generally in the several-hundred‑nautical‑mile class, roughly about 500–550 nautical miles, with mission equipment, reserves, and payload affecting real-world figures. Passenger capacity tends to be higher in the helicopters for utility seating: the H225 is often configured around 16–19 passengers, and the S-92 commonly around 19, though layouts vary by operator and mission. The Citation XLS+ usually seats fewer, most often about 8–9 passengers in a typical executive configuration. Overall, the jet prioritizes speed and range, while the helicopters prioritize vertical access and higher cabin utility for short-to-medium sectors.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 19.79 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Sikorsky |
| Aircraft Name | H225 | XLS+ | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.94 |
| Max Cabin Seats | 28 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 7417 |
| Standard Cabin Seats | 19 | 8 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 21 |
| Max Cabin Seats | 28 | 9 | 19 |
| Standard Cabin Seats | 19 | 8 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 |
| Horsepower | 2100 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | — |
| Overall Height (ft) | 16.3 | 17.2 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| Wingspan (ft) | — | 56.3 | — |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | — |
| Cabin Height (ft) | — | 5.7 | — |
| Cabin Length (ft) | — | 18.5 | — |
| 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 | — |