Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna Citation Xls vs Pilatus Pc 24
The Airbus H225 is a large twin‑engine helicopter (rotorcraft) optimized for offshore, SAR, and utility missions rather than point‑to‑point speed. It typically carries around 16–19 passengers depending on cabin fit, with practical range commonly in the ~500–650 nm class, extendable with auxiliary tanks. The Beechcraft King Air 360ER is a pressurized twin‑turboprop business aircraft aimed at efficient regional travel. It generally seats about 8–9 passengers, with an extended range around ~1,500–1,800 nm depending on payload and reserves. The Cessna Citation XLS+ is a midsize business jet focused on faster city‑pair capability. Typical seating is about 8–9 passengers (up to 12 in some configurations), with range roughly ~2,000–2,100 nm. The Pilatus PC‑24 is a light jet with a notably flexible cabin and rough/short‑field capability for its class. It typically carries 6–8 passengers (up to around 10), with range commonly ~1,800–2,000 nm depending on mission profile.
| 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 |