Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Gulfstream G700 vs Piaggio Avanti Evo
The Airbus H225 is a long‑range twin‑engine helicopter suited to offshore and SAR-style missions. It typically carries around 16–19 passengers (higher in high‑density layouts) and offers a practical range on the order of roughly 400–500 nautical miles, trading speed for vertical lift and access to unimproved sites. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for short, rugged strips and cargo/passenger flexibility. It commonly seats 9–14 passengers, with a typical range around 900–1,100 nautical miles depending on payload and reserves. The Gulfstream G700 is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel. It generally accommodates about 13–19 passengers in executive configurations (with higher maximums possible) and can reach roughly 7,500 nautical miles, emphasizing high speed, altitude, and cabin comfort. The Piaggio Avanti EVO is a twin‑turboprop business aircraft positioned between utility turboprops and business jets, usually seating about 6–9 passengers. Its typical range is around 1,500–1,800 nautical miles, offering efficient cruise and a relatively fast turboprop profile.
| Spec | AIRBUS H225 | Gulfstream G700 | Piaggio Avanti EVO |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | — | — |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 8 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Gulfstream | Piaggio |
| Aircraft Name | H225 | G700 | Avanti EVO |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 1530 |
| DOC / nm / Seat | $ 0.99 | — | — |
| Max Cabin Seats | 28 | 19 | 7 |
| OEM Verification | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — | 3775 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Direct Operating Cost | $ 2,963 | — | — |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 516 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $ 7,695,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 8 |
| Max Cabin Seats | 28 | 19 | 7 |
| Standard Cabin Seats | 19 | 12 | 6 |
| Crew Rest | — | Optional | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Lavatory | — | — | No |
| Cabin Pressure (psi) | — | — | 9 |
| Galley / Refreshment | — | — | No |
| SL Cabin Altitude (ft) | — | — | 24000 |
| Max Cabin Altitude (ft) | — | — | 6600 |
| Engine | |||
| FADEC | Yes | — | Yes |
| Model | Makila 2A1 | Pearl 700 | PT6A–66B |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On Condition | 3600 |
| Horsepower | 2100 | — | 850 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Thrust (lbs) | — | 18250 | — |
| Flat Rating | — | — | ISA + 28 |
| Fuel Burn (gph) | — | — | 100 |
| Dimensions | |||
| Length (ft) | 63.4 | 109.9 | 47.3 |
| Overall Height (ft) | 16.3 | 25.4 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 103 | 47.1 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 8.2 | 6.1 |
| Cabin Height (ft) | — | 6.25 | 5.8 |
| Cabin Length (ft) | — | 56.9 | 14.9 |
| Baggage Volume Int. (cu. ft) | — | 195 | 35.2 |
| Cabin Width - Floor (ft) | — | — | 3.5 |