Airbus Helicopters H225 vs Cessna Citation Xls vs Gulfstream G700 vs Piaggio Avanti Evo
The Airbus H225 is a large twin‑engine helicopter suited to offshore, search‑and‑rescue, and utility missions rather than point‑to‑point jet travel. It typically carries around 16–19 passengers (depending on fit) and has a practical range on the order of roughly 500–600 nautical miles. The Cessna Citation XLS+ is a midsize business jet optimized for short‑to‑medium trips, often seating 7–9 passengers in a typical executive layout. Its range is roughly about 2,000 nautical miles, making it well suited to regional and many transcontinental missions with a stop. The Gulfstream G700 is an ultra‑long‑range, large‑cabin business jet designed for intercontinental flying, commonly configured for about 12–19 passengers. Its range is roughly 7,500 nautical miles, enabling many nonstop city pairs across oceans. The Piaggio Avanti EVO is a high‑speed, pressurized twin‑turboprop with a business‑aviation cabin, typically seating about 6–9 passengers. Its range is generally around 1,500–1,800 nautical miles, bridging the gap between light jets and larger midsize jets.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — | — |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 8 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Gulfstream | Piaggio |
| Aircraft Name | H225 | XLS+ | G700 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — | — |
| Max Cabin Seats | 28 | 9 | 19 | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | — | 3775 |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 430 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $78,000,000 | $ 7,695,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 8 |
| Max Cabin Seats | 28 | 9 | 19 | 7 |
| Standard Cabin Seats | 19 | 8 | 12 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | — | No |
| Crew Rest | — | No | Optional | — |
| Jump Seat | — | No | Yes | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | AFT | FWD / 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 | Pearl 700 | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | On Condition | 3600 |
| Horsepower | 2100 | — | — | 850 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | — | ISA + 28 |
| Thrust (lbs) | — | 4119 | 18250 | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 109.9 | 47.3 |
| Overall Height (ft) | 16.3 | 17.2 | 25.4 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | — |
| Wingspan (ft) | — | 56.3 | 103 | 47.1 |
| Aisle Step (ft) | — | 0.7 | Flat Floor | — |
| Cabin Width (ft) | — | 5.5 | 8.2 | 6.1 |
| Cabin Height (ft) | — | 5.7 | 6.25 | 5.8 |
| Cabin Length (ft) | — | 18.5 | 56.9 | 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 | 195 | 35.2 |