Airbus Helicopters H225 vs Cessna Citation Xls vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Pilatus Pc 24
The Airbus H225 is a large twin‑engine helicopter designed for offshore, rescue, and utility missions. It typically carries about 19 passengers (depending on layout) and offers a practical range on the order of roughly 450–500 nautical miles, trading speed and altitude for vertical‑lift flexibility. The MD Helicopters (McDonnell Douglas) 902 Explorer is a lighter twin‑engine helicopter, generally seating around 8–10 passengers, with a shorter typical range of roughly 300–350 nautical miles, optimized for law enforcement, EMS, and corporate shuttle roles. The Cessna Citation XLS+ is a midsize business jet, usually configured for about 8–9 passengers, with a range around 1,800–2,100 nautical miles, suited to efficient point‑to‑point regional travel. The Pilatus PC‑24 is a light business jet with “super versatile” operations, commonly seating 6–10 passengers, and offering roughly 1,900–2,000 nautical miles of range; it stands out for its ability to use shorter or rougher runways compared with many jets in its class.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 3.71 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Pilatus |
| Aircraft Name | H225 | XLS+ | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.62 |
| Max Cabin Seats | 28 | 9 | 10 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 6680 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 430 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 6 |
| Max Cabin Seats | 28 | 9 | 10 |
| Standard Cabin Seats | 19 | 8 | 6 |
| 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 |
| Model | Makila 2A1 | PW545C | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | 5000 |
| Horsepower | 2100 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| 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 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| 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 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 90 |