Airbus Helicopters H225 vs Cessna Citation Xls vs Piaggio Avanti Evo vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Cessna Citation XLS+ and Piaggio Avanti EVO are fixed‑wing business aircraft. In category, the H225 is a large, twin‑engine heavy helicopter designed for offshore transport, SAR, and utility missions; the R66 is a light, single‑engine turbine helicopter typically used for short corporate hops, training, and local utility work. The Citation XLS+ is a super‑light/midsize‑class business jet optimized for fast point‑to‑point travel, whereas the Avanti EVO is a high‑speed turboprop business aircraft known for jet‑like cruise speeds with turboprop efficiency. In range, the Citation XLS+ generally offers the longest reach for nonstop trips among these four, with the Avanti EVO typically close behind; both substantially exceed the practical trip lengths of the helicopters. The H225 can cover meaningful medium distances for a helicopter, but it is still well below typical business‑jet ranges, while the R66 is best suited to shorter legs. For passenger capacity, the H225 carries the most, commonly configured for well over a dozen passengers. The Citation XLS+ and Avanti EVO usually seat around 7–9 passengers. The R66 is the smallest, typically carrying about 4 passengers plus a pilot.
| 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 |