Airbus Helicopters H225 vs Bombardier Global 7500 vs Cessna Citation Xls vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore transport, search and rescue, and utility missions where vertical lift matters more than speed. Its practical range is roughly 500–700 nautical miles depending on payload and reserves, and it typically carries about 16–19 passengers in transport seating (with higher-density configurations possible). The Bombardier Global 7500 is an ultra‑long‑range business jet optimized for intercontinental flying. It offers about 7,700 nautical miles of range and is usually configured for 10–19 passengers, emphasizing comfort, multiple cabin zones, and long endurance. The Cessna Citation XLS+ is a super‑midsize business jet aimed at efficient regional to transcontinental missions. It delivers roughly 2,100 nautical miles of range and commonly seats 7–9 passengers in a club cabin layout, with a maximum certified capacity around 12. The Piaggio Avanti EVO is a high‑speed turboprop business aircraft, positioned between light jets and midsize jets on cost and performance. Range is about 1,500–1,800 nautical miles, and typical seating is 6–8 passengers.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Cessna Citation XLS+ | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 5.34 | — |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 10 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Cessna Citation | Piaggio |
| Aircraft Name | H225 | Global 7500 | XLS+ | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 1906 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.67 | — |
| Max Cabin Seats | 28 | 19 | 9 | 7 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7540 | 3775 |
| Standard Cabin Seats | 19 | 12 | 8 | 6 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 2,303 | — |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 430 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $15,500,000 | $ 7,695,000 |
| Aircraft Type | — | Business Jet | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 21 | 14 | 10 | 8 |
| Max Cabin Seats | 28 | 19 | 9 | 7 |
| Standard Cabin Seats | 19 | 12 | 8 | 6 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | AFT | — |
| Galley / Refreshment | — | Galley | Galley | No |
| Max Cabin Altitude (ft) | — | 4500 | — | 6600 |
| Cabin Pressure (psi) | — | — | 9.3 | 9 |
| SL Cabin Altitude (ft) | — | — | 25230 | 24000 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | PW545C | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | 5000 | 3600 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 28 |
| Thrust (lbs) | — | 18920 | 4119 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 111 | 52.5 | 47.3 |
| Overall Height (ft) | 16.3 | 27 | 17.2 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 104 | 56.3 | 47.1 |
| Cabin Width (ft) | — | 8 | 5.5 | 6.1 |
| Cabin Height (ft) | — | 6.2 | 5.7 | 5.8 |
| Cabin Length (ft) | — | 54.5 | 18.5 | 14.9 |
| Aisle Step (ft) | — | — | 0.7 | — |
| 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 |