Airbus Helicopters H225 vs Cessna Citation Xls vs Embraer Legacy 650 E vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter rather than a fixed‑wing business jet. Its typical practical range is on the order of a few hundred nautical miles (roughly 400–500 nm depending on load and reserves), and it commonly carries about 16–19 passengers in an offshore or utility configuration, with flexibility for fewer passengers plus cargo or mission equipment. The Cessna Citation XLS+ is a midsize business jet designed for short‑to‑medium trips, with a range around 1,900–2,100 nm and a typical cabin layout for about 8–9 passengers (maximum seating generally higher in dense configurations). The Embraer Legacy 650E is a large‑cabin long‑range business jet, offering roughly 3,800–3,900 nm of range and usually seating 13 passengers (often 13–14 depending on layout), emphasizing comfort and baggage volume for longer missions. The Piaggio Avanti EVO is a twin‑engine turboprop in the high‑end executive category, with a range around 1,700–1,800 nm and a typical passenger capacity of about 7–9, combining jet‑like cabin comfort with turboprop operating economics.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Piaggio |
| Aircraft Name | H225 | XLS+ | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — |
| Max Cabin Seats | 28 | 9 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 3775 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 430 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 8 |
| Max Cabin Seats | 28 | 9 | 7 |
| Standard Cabin Seats | 19 | 8 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | 9 |
| Galley / Refreshment | — | Galley | No |
| SL Cabin Altitude (ft) | — | 25230 | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | 3600 |
| Horsepower | 2100 | — | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 28 |
| Thrust (lbs) | — | 4119 | — |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 47.3 |
| Overall Height (ft) | 16.3 | 17.2 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 56.3 | 47.1 |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | 6.1 |
| Cabin Height (ft) | — | 5.7 | 5.8 |
| Cabin Length (ft) | — | 18.5 | 14.9 |
| Cabin Width - Floor (ft) | — | 3.9 | 3.5 |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 35.2 |