Airbus Helicopters H225 vs Cessna Citation Xls vs Embraer Legacy 650 E
The Airbus H225 is a long‑range twin‑engine helicopter built for vertical lift missions such as offshore transport and search and rescue. Compared with the two jets, its range is shorter, typically around 450–550 nautical miles depending on payload and reserves, but it can carry a relatively large cabin load for a helicopter, commonly about 16–19 passengers in transport layouts. The Cessna Citation XLS+ is a super‑light business jet optimized for short to medium trips and frequent airport access. It offers a typical range of about 1,800–2,100 nautical miles and usually seats 7–9 passengers in executive configuration, trading cabin size for efficiency and runway flexibility. The Embraer Legacy 650E is a large‑cabin, long‑range business jet aimed at transcontinental missions. It generally reaches about 3,800–4,000 nautical miles and typically accommodates 10–13 passengers, offering more space and endurance than the XLS+ and far longer range than the H225, though without helicopter VTOL capability.
| Spec | AIRBUS H225 | Cessna Citation XLS+ |
|---|---|---|
| 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 |