Airbus Helicopters H225 vs Cessna Citation Xls vs Piper M600 Sls vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are large twin‑engine helicopters typically used for offshore transport, search and rescue, and utility missions. Both carry roughly 18–19 passengers in high‑density layouts (more in some utility configurations) and offer medium helicopter ranges on the order of about 500–600 nautical miles, depending heavily on payload, fuel reserves, and installed equipment. The Cessna Citation XLS+ is a light business jet optimized for short‑to‑medium regional trips at high speed, generally seating about 8–9 passengers in a typical executive configuration, with a range around 1,800–2,100 nautical miles depending on conditions and cabin fit. The Piper M600 SLS is a single‑engine turboprop (personal/business aircraft) in a smaller class, usually seating 5–6 occupants, with a range roughly around 1,400–1,600 nautical miles. Overall, the helicopters prioritize vertical lift and access to confined sites, while the fixed‑wing aircraft prioritize speed and longer point‑to‑point range from runways.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 6 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Piper | Sikorsky |
| Aircraft Name | H225 | XLS+ | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1406 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 28 | 9 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 2200 | 7417 |
| Standard Cabin Seats | 19 | 8 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 274 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $3,081,400 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 5 | 21 |
| Max Cabin Seats | 28 | 9 | — | 19 |
| Standard Cabin Seats | 19 | 8 | 4 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | — |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Galley Location | — | FWD | MID | — |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 9.3 | 5.6 | — |
| Galley / Refreshment | — | Galley | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | 25230 | 12600 | — |
| Max Cabin Altitude (ft) | — | — | 8644 | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | Makila 2A1 | PW545C | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 3600 | 4000 |
| Horsepower | 2100 | — | 600 | 2520 |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 | 760 |
| Flat Rating | — | ISA + 10 | ISA + 55 | — |
| Thrust (lbs) | — | 4119 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 29.7 | — |
| Overall Height (ft) | 16.3 | 17.2 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 | 775 |
| Wingspan (ft) | — | 56.3 | 43.2 | — |
| Aisle Step (ft) | — | 0.7 | — | — |
| Cabin Width (ft) | — | 5.5 | 4.1 | — |
| Cabin Height (ft) | — | 5.7 | 4 | — |
| Cabin Length (ft) | — | 18.5 | 12.3 | — |
| 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 | 20 | — |