Airbus Helicopters H225 vs Cessna Citation Xls vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are large twin‑engine helicopters optimized for offshore transport and search‑and‑rescue missions. Their range is broadly similar, typically around 500–600 nautical miles depending on payload and reserves, and each can carry roughly 18–19 passengers in a high‑density offshore layout (with fewer in VIP/SAR configurations). The Cessna Citation XLS+ is a midsize business jet focused on fast point‑to‑point travel; it offers substantially longer range than the helicopters, about 1,800–2,100 nautical miles, and commonly seats 7–9 passengers (up to around 12 with belted seats). The Piaggio Avanti EVO is a high‑performance twin‑turboprop business aircraft, generally positioned between the XLS+ and the helicopters: it has a range around 1,400–1,800 nautical miles and typically carries 6–9 passengers. In short, the helicopters prioritize vertical access and cabin capacity over distance and speed, while the XLS+ and Avanti EVO prioritize efficient regional to transcontinental travel with smaller passenger counts.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 8 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Piaggio | Sikorsky |
| Aircraft Name | H225 | XLS+ | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1530 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — | $ 0.94 |
| Max Cabin Seats | 28 | 9 | 7 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 3775 | 7417 |
| Standard Cabin Seats | 19 | 8 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 400 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 7,695,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 8 | 21 |
| Max Cabin Seats | 28 | 9 | 7 | 19 |
| Standard Cabin Seats | 19 | 8 | 6 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | — |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 9.3 | 9 | — |
| Galley / Refreshment | — | Galley | No | — |
| SL Cabin Altitude (ft) | — | 25230 | 24000 | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 3600 | 4000 |
| Horsepower | 2100 | — | 850 | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 10 | ISA + 28 | — |
| Thrust (lbs) | — | 4119 | — | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 47.3 | — |
| Overall Height (ft) | 16.3 | 17.2 | 13.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 775 |
| Wingspan (ft) | — | 56.3 | 47.1 | — |
| Aisle Step (ft) | — | 0.7 | — | — |
| Cabin Width (ft) | — | 5.5 | 6.1 | — |
| Cabin Height (ft) | — | 5.7 | 5.8 | — |
| Cabin Length (ft) | — | 18.5 | 14.9 | — |
| Cabin Width - Floor (ft) | — | 3.9 | 3.5 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | 140 |
| Baggage Volume Int. (cu. ft) | — | 10 | 35.2 | — |