Airbus Helicopters H225 vs Cessna Citation Xls vs Dassault Falcon 8x vs Pilatus Pc 24
The Airbus H225 is a twin‑engine helicopter in the heavy utility/offshore category, optimized for vertical access rather than speed. Its typical range is roughly 450–600 nautical miles depending on payload and reserves, and it commonly carries around 16–19 passengers in transport layouts (more in high‑density configurations). The Cessna Citation XLS+ is a super‑light/midsize business jet aimed at efficient short‑to‑medium missions. It typically flies about 2,000–2,100 nautical miles and is usually configured for 7–9 passengers. The Dassault Falcon 8X is an ultra‑long‑range, large‑cabin business jet designed for intercontinental flights. Its range is about 6,400 nautical miles, and it commonly seats 12–16 passengers depending on cabin layout. The Pilatus PC‑24 is a light business jet with “utility jet” traits, including strong short/rough‑field capability. Its range is about 2,000 nautical miles, and it typically carries 6–10 passengers.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Dassault Falcon 8X | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 7.66 | $ 3.71 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 17 | 6 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Dassault Falcon | Pilatus |
| Aircraft Name | H225 | XLS+ | 8X | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 6450 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.64 | $ 0.62 |
| Max Cabin Seats | 28 | 9 | 16 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 36900 | 6680 |
| Standard Cabin Seats | 19 | 8 | 14 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 3,805 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Honeywell Primus EASy II | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 430 | 516 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 62,500,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 17 | 6 |
| Max Cabin Seats | 28 | 9 | 16 | 10 |
| Standard Cabin Seats | 19 | 8 | 14 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | 2 Enclosed Flushing | 1 Enclosed Flushing |
| Crew Rest | — | No | No | No |
| Jump Seat | — | No | Yes | No |
| Galley Location | — | FWD | FWD | FWD |
| Lavatory Location | — | AFT | FWD / AFT | FWD |
| Cabin Pressure (psi) | — | 9.3 | 10.2 | 9.3 |
| Galley / Refreshment | — | Galley | Galley | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 25230 | 29200 | 23500 |
| Max Cabin Altitude (ft) | — | — | 3900 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | PW307D | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | On-Condition | 5000 |
| Horsepower | 2100 | — | — | — |
| No. of Engines | 2 | 2 | 3 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | ISA + 17 | ISA + 23 |
| Thrust (lbs) | — | 4119 | 6722 | 3435 |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 80.2 | 52.2 |
| Overall Height (ft) | 16.3 | 17.2 | 26.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 1695 | — |
| Wingspan (ft) | — | 56.3 | 86.3 | 55.8 |
| Aisle Step (ft) | — | 0.7 | — | Flat Floor |
| Cabin Width (ft) | — | 5.5 | 7.7 | 5.6 |
| Cabin Height (ft) | — | 5.7 | 6.2 | 5.1 |
| Cabin Length (ft) | — | 18.5 | 42.7 | 23 |
| Cabin Width - Floor (ft) | — | 3.9 | 6.3 | 3.8 |
| Cabin Length - Seating (ft) | — | 14.3 | 29.2 | 17 |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 140 | 90 |