Airbus Helicopters H225 vs Cessna Citation Xls vs Pilatus Pc 24 vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy, twin‑engine helicopters designed for offshore, SAR, and utility work. They trade speed and range for vertical lift and hover capability. Typical passenger layouts are roughly in the high‑teens to around twenty seats depending on mission fit, with practical ranges commonly in the 400–600 nautical mile class, varying with payload and reserves. The Cessna Citation XLS+ and Pilatus PC‑24 are light business jets, optimized for fast point‑to‑point travel. The Citation XLS+ is a conventional paved‑runway executive jet, usually carrying about 7–9 passengers, with a range around 2,000 nautical miles. The Pilatus PC‑24 is a “super versatile” light jet built for short and semi‑prepared strips, typically seating about 6–10 passengers, with a range roughly around 2,000 nautical miles (often somewhat more depending on configuration). Overall, the jets offer far greater cruise speed and range, while the helicopters offer access to places with no runway at all.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Pilatus PC-24 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 3.71 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 6 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Pilatus | Sikorsky |
| Aircraft Name | H225 | XLS+ | PC-24 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 2076 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.62 | $ 0.94 |
| Max Cabin Seats | 28 | 9 | 10 | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 6680 | 7417 |
| Standard Cabin Seats | 19 | 8 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 1,619 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 440 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $11,800,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 6 | 21 |
| Max Cabin Seats | 28 | 9 | 10 | 19 |
| Standard Cabin Seats | 19 | 8 | 6 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | 1 Enclosed Flushing | — |
| Crew Rest | — | No | No | — |
| Jump Seat | — | No | No | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | AFT | FWD | — |
| Cabin Pressure (psi) | — | 9.3 | 9.3 | — |
| Galley / Refreshment | — | Galley | Optional Refreshment Center | — |
| SL Cabin Altitude (ft) | — | 25230 | 23500 | — |
| Cargo Door | — | — | Yes | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | FJ44-4A-QPM | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 5000 | 4000 |
| Horsepower | 2100 | — | — | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 10 | ISA + 23 | — |
| Thrust (lbs) | — | 4119 | 3435 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 52.2 | — |
| Overall Height (ft) | 16.3 | 17.2 | 17.4 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 775 |
| Wingspan (ft) | — | 56.3 | 55.8 | — |
| Aisle Step (ft) | — | 0.7 | Flat Floor | — |
| Cabin Width (ft) | — | 5.5 | 5.6 | — |
| Cabin Height (ft) | — | 5.7 | 5.1 | — |
| Cabin Length (ft) | — | 18.5 | 23 | — |
| Cabin Width - Floor (ft) | — | 3.9 | 3.8 | — |
| Cabin Length - Seating (ft) | — | 14.3 | 17 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | 140 |
| Baggage Volume Int. (cu. ft) | — | 10 | 90 | — |