Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Cessna Citation Xls vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore or utility missions where vertical lift matters more than speed. Its range is typically around 450–650 nautical miles depending on payload and reserves, and it commonly carries about 16–19 passengers in high‑density seating (or fewer in VIP/offshore layouts). The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for short, rugged strips and lower operating cost. It generally offers about 800–900 nautical miles of range and seats up to 14 passengers (often 9–12 in commuter configurations). The Cessna Citation XLS+ is a midsize business jet focused on faster point‑to‑point travel. Typical range is about 2,000–2,100 nautical miles, with seating commonly 8–9 passengers (up to about 12 in higher‑density arrangements). The Piaggio Avanti EVO is a high‑speed twin‑turboprop that bridges turboprops and light jets, offering jet‑like cruise speeds with turboprop efficiency. Range is typically around 1,400–1,800 nautical miles, and it usually seats 7–9 passengers.
| 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 |