Airbus Helicopters H225 vs Cessna Citation Xls vs Piaggio Avanti Evo vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter optimized for offshore and utility missions rather than point‑to‑point airliner‑style travel. Its practical range is roughly in the 450–650 nm class depending on payload and reserves, and it typically carries around 16–19 passengers in transport seating (more in high‑density layouts). The Cessna Citation XLS+ is a midsize business jet built for fast regional trips. It offers about 1,800–2,100 nm range and usually seats 7–9 passengers in a club configuration, with optional belted capacity higher. The Piaggio Avanti EVO is a twin‑turboprop business aircraft positioned between light jets and turboprops: jet‑like cruise speeds with turboprop economics. It generally provides around 1,500–1,800 nm range and seats about 7–9 passengers. The Piper M600 SLS is a single‑engine turboprop aimed at owner‑pilots and short‑to‑medium missions. It typically delivers about 1,200–1,500 nm range and carries 4–6 passengers plus a pilot, depending on cabin layout and payload.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Piaggio Avanti EVO | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — | $ 2.19 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 8 | 6 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Piaggio | Piper |
| Aircraft Name | H225 | XLS+ | Avanti EVO | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1530 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — | $ 0.55 |
| Max Cabin Seats | 28 | 9 | 7 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 3775 | 2200 |
| Standard Cabin Seats | 19 | 8 | 6 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 430 | 400 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $ 7,695,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 8 | 5 |
| Max Cabin Seats | 28 | 9 | 7 | — |
| Standard Cabin Seats | 19 | 8 | 6 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | No |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Galley Location | — | FWD | — | MID |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 9.3 | 9 | 5.6 |
| Galley / Refreshment | — | Galley | No | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 25230 | 24000 | 12600 |
| Max Cabin Altitude (ft) | — | — | 6600 | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | Makila 2A1 | PW545C | PT6A–66B | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | 3600 | 3600 |
| Horsepower | 2100 | — | 850 | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 10 | ISA + 28 | ISA + 55 |
| Thrust (lbs) | — | 4119 | — | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 47.3 | 29.7 |
| Overall Height (ft) | 16.3 | 17.2 | 13.1 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Wingspan (ft) | — | 56.3 | 47.1 | 43.2 |
| Aisle Step (ft) | — | 0.7 | — | — |
| Cabin Width (ft) | — | 5.5 | 6.1 | 4.1 |
| Cabin Height (ft) | — | 5.7 | 5.8 | 4 |
| Cabin Length (ft) | — | 18.5 | 14.9 | 12.3 |
| 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 | 20 |