Airbus Helicopters H225 vs Enstrom 480b vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo
The Airbus H225 is a heavy twin‑engine helicopter optimized for offshore transport and utility missions; it offers the greatest passenger capacity of the group (typically around 19 plus crew) and solid mission radius for a rotorcraft, commonly in the few‑hundred‑nautical‑mile range depending on payload and reserves. The Enstrom 480B is a light single‑engine piston helicopter aimed at training and light utility; it carries about 4–5 occupants and has the shortest practical range here, generally a couple hundred nautical miles. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter with the NOTAR system; it usually seats about 8–10 occupants and provides mid‑tier helicopter range, often a few hundred nautical miles. The Piaggio Avanti EVO is a twin‑turboprop fixed‑wing aircraft in the light business category; it carries typically 6–9 passengers and, unlike the helicopters, delivers the longest range by a wide margin, commonly well over 1,000 nautical miles, making it best for fast point‑to‑point travel rather than vertical‑lift missions.
| Spec | AIRBUS H225 | Piaggio Avanti EVO |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 8 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio |
| Aircraft Name | H225 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 7 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 |
| Standard Cabin Seats | 19 | 6 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 1 |
| Total Seats | 21 | 8 |
| Max Cabin Seats | 28 | 7 |
| Standard Cabin Seats | 19 | 6 |
| 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 | PT6A–66B |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 3600 |
| Horsepower | 2100 | 850 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 28 |
| Fuel Burn (gph) | — | 100 |
| Dimensions | ||
| Length (ft) | 63.4 | 47.3 |
| Overall Height (ft) | 16.3 | 13.1 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| Wingspan (ft) | — | 47.1 |
| Cabin Width (ft) | — | 6.1 |
| Cabin Height (ft) | — | 5.8 |
| Cabin Length (ft) | — | 14.9 |
| Cabin Width - Floor (ft) | — | 3.5 |
| Baggage Volume Int. (cu. ft) | — | 35.2 |