Airbus Helicopters H225 vs Cessna Citation Xls vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 is a heavy twin‑engine helicopter, typically used for offshore and utility missions rather than point‑to‑point business travel. Its practical range is roughly 400–500 nautical miles, and it can carry a large cabin load, commonly around 16–19 passengers depending on configuration. The Cessna Citation XLS+ is a midsize business jet optimized for short‑to‑medium trips. It typically offers about 1,800–2,100 nautical miles of range and is usually arranged for about 8–9 passengers. The Piaggio Avanti EVO is a high‑speed twin‑turboprop business aircraft that competes with light jets on speed while retaining turboprop efficiency. Range is generally around 1,500–1,800 nautical miles with a typical seating of about 6–8 passengers. The Pilatus PC‑24 is a light jet designed for versatility, including operations from shorter or semi‑prepared runways. It commonly offers about 1,800–2,000 nautical miles of range and seats roughly 6–10 passengers, with a comparatively flexible cabin and cargo capability.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — | $ 3.71 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 8 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Piaggio | Pilatus |
| Aircraft Name | H225 | XLS+ | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — | $ 0.62 |
| Max Cabin Seats | 28 | 9 | 7 | 10 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 3775 | 6680 |
| Standard Cabin Seats | 19 | 8 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 430 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 7,695,000 | $11,800,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 8 | 6 |
| Max Cabin Seats | 28 | 9 | 7 | 10 |
| Standard Cabin Seats | 19 | 8 | 6 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | 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 | 9.3 |
| Galley / Refreshment | — | Galley | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 25230 | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | 3600 | 5000 |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | ISA + 28 | ISA + 23 |
| Thrust (lbs) | — | 4119 | — | 3435 |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 17.2 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 56.3 | 47.1 | 55.8 |
| Aisle Step (ft) | — | 0.7 | — | Flat Floor |
| Cabin Width (ft) | — | 5.5 | 6.1 | 5.6 |
| Cabin Height (ft) | — | 5.7 | 5.8 | 5.1 |
| Cabin Length (ft) | — | 18.5 | 14.9 | 23 |
| Cabin Width - Floor (ft) | — | 3.9 | 3.5 | 3.8 |
| Cabin Length - Seating (ft) | — | 14.3 | — | 17 |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 35.2 | 90 |