Airbus Helicopters H225 vs Cessna Citation Xls vs Robinson R66 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy, twin‑engine helicopters typically used for offshore transport and SAR, offering large cabins and long helicopter-class range. The H225 generally seats around 16–19 passengers, while the S-92 is commonly configured for about 19 passengers; both can reach roughly 500–600 nautical miles depending on payload, reserves, and mission equipment. The Robinson R66 is a light, single‑engine helicopter aimed at private, utility, and training roles. It carries about 4 passengers plus a pilot (typically 5 seats total) and has a much shorter reach than the heavy twins, roughly in the 300–350 nautical mile class, with greater sensitivity to payload and conditions. The Cessna Citation XLS+ is a light/midsize business jet rather than a helicopter, optimized for fast point‑to‑point travel from runways. It typically carries about 7–9 passengers and has substantially longer range than the helicopters, around 2,000 nautical miles, making it best for regional to transcontinental trips where helicopter access is not required.
| 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 | — |