Airbus Helicopters H225 vs Cessna Citation Xls vs Leonardo Aw189 vs Sikorsky S 92
The Airbus H225 and Leonardo AW189 are large twin‑engine helicopters primarily used for offshore transport and SAR, while the Sikorsky S‑92 is a heavy twin‑engine helicopter in the same mission set, typically positioned at the higher end of capacity and endurance. The Cessna Citation XLS+ is a midsize business jet, suited to point‑to‑point airport travel rather than vertical‑lift operations. In range terms, the Citation XLS+ generally offers the longest legs, typically around 2,000 nautical miles depending on payload and reserves. The helicopters are shorter‑range by comparison: the AW189 is commonly around the 450–500 nautical mile class, while the H225 and S‑92 are often in the roughly 500–600+ nautical mile class in typical offshore configurations, varying with tanks, payload, and weather. For passenger capacity, the Citation XLS+ is usually configured for about 8–9 passengers. The AW189 is commonly configured around 16–19 seats. The H225 and S‑92 typically carry more, often around 19 passengers in offshore seating, with the S‑92 frequently comparable or slightly higher depending on layout and certification.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 15.57 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 21 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Leonardo | Sikorsky |
| Aircraft Name | H225 | XLS+ | AW189 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 651 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.74 | $ 0.94 |
| Max Cabin Seats | 28 | 9 | 19 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | — | 7417 |
| Standard Cabin Seats | 19 | 8 | 19 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 2,413 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 155 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $2,413,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 21 | 21 |
| Max Cabin Seats | 28 | 9 | 19 | 19 |
| Standard Cabin Seats | 19 | 8 | 19 | 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 | Yes |
| Model | Makila 2A1 | PW545C | CT7-2E1 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 | 4000 |
| Horsepower | 2100 | — | 1983 | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 10 | — | — |
| Thrust (lbs) | — | 4119 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 57.8 | — |
| Overall Height (ft) | 16.3 | 17.2 | 16.6 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | 48 | — |
| Cabin Volume (cu. ft) | 547 | — | 395 | 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 | 85 | 140 |
| Baggage Volume Int. (cu. ft) | — | 10 | — | — |