| Summary |
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 10 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Cessna Citation |
| Aircraft Name | H225 | XLS+ |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 |
| Max Cabin Seats | 28 | 9 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 |
| Standard Cabin Seats | 19 | 8 |
| Direct Operating Cost | $ 2,963 | $ 2,303 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 430 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 |
| Cabin |
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 10 |
| Max Cabin Seats | 28 | 9 |
| Standard Cabin Seats | 19 | 8 |
| 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 |
| Model | Makila 2A1 | PW545C |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 5000 |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 10 |
| Thrust (lbs) | — | 4119 |
| Dimensions |
| Length (ft) | 63.4 | 52.5 |
| Overall Height (ft) | 16.3 | 17.2 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| 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 |
| Baggage Volume Int. (cu. ft) | — | 10 |
