Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna Citation Xls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters typically used for offshore oil and gas, search and rescue, and VIP transport. In general terms, both carry roughly 16–19 passengers in high‑density seating (or fewer in executive layouts) and offer practical ranges on the order of about 450–600 nautical miles depending on payload, reserves, and mission profile. The H225 is often cited with slightly longer nominal range in some configurations, while the S‑92 is widely regarded for robust offshore capability and cabin volume. The Beechcraft King Air 360ER is a twin‑turboprop fixed‑wing aircraft aimed at utility and corporate missions. It usually seats around 6–11 passengers and, with its extended‑range configuration, can reach roughly 1,500–1,800 nautical miles, significantly farther than the helicopters. The Cessna Citation XLS+ is a midsize business jet optimized for faster point‑to‑point travel. It typically seats about 7–9 passengers and has a range around 1,900–2,100 nautical miles, generally the longest of the four while also offering the highest cruise speeds.
| 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 | — |