Airbus Helicopters H225 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Piaggio Avanti Evo vs Pilatus Pc 24
The Airbus H225 and the MD Helicopters 902 Explorer are helicopters, optimized for vertical lift and access to confined or unimproved sites, while the Piaggio Avanti EVO and Pilatus PC-24 are fixed‑wing business aircraft designed for faster point‑to‑point travel. In category terms, the H225 is a heavy, long‑range twin‑engine helicopter, typically used for offshore transport, SAR, and utility roles; the 902 Explorer is a light twin‑engine helicopter aimed at corporate, law‑enforcement, and EMS missions. For range, the H225 generally offers longer helicopter legs (roughly in the 450–700 nm class depending on fit and reserves) than the 902 (often around 300–400 nm). Passenger capacity also favors the H225, which can seat around 16–19 in typical layouts, versus roughly 7–8 for the 902. The Avanti EVO is a pressurized twin‑turboprop business aircraft with a typical range around 1,500–1,800 nm and seating commonly 6–9. The Pilatus PC‑24 is a light business jet with roughly 1,800–2,000+ nm range and usually 6–10 passengers, trading higher cruise speed and altitude for runway requirements.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 3.71 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Piaggio | Pilatus |
| Aircraft Name | H225 | Avanti EVO | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 2076 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.62 |
| Max Cabin Seats | 28 | 7 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 3775 | 6680 |
| Standard Cabin Seats | 19 | 6 | 6 |
| Direct Operating Cost | $ 2,963 | — | $ 1,619 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 142 | 400 | 440 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $11,800,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 |
| Total Seats | 21 | 8 | 6 |
| Max Cabin Seats | 28 | 7 | 10 |
| Standard Cabin Seats | 19 | 6 | 6 |
| Lavatory | — | No | 1 Enclosed Flushing |
| Cabin Pressure (psi) | — | 9 | 9.3 |
| Galley / Refreshment | — | No | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | 24000 | 23500 |
| Max Cabin Altitude (ft) | — | 6600 | — |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PT6A–66B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 3600 | 5000 |
| Horsepower | 2100 | 850 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 28 | ISA + 23 |
| Fuel Burn (gph) | — | 100 | — |
| Thrust (lbs) | — | — | 3435 |
| Dimensions | |||
| Length (ft) | 63.4 | 47.3 | 52.2 |
| Overall Height (ft) | 16.3 | 13.1 | 17.4 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Wingspan (ft) | — | 47.1 | 55.8 |
| Cabin Width (ft) | — | 6.1 | 5.6 |
| Cabin Height (ft) | — | 5.8 | 5.1 |
| Cabin Length (ft) | — | 14.9 | 23 |
| Cabin Width - Floor (ft) | — | 3.5 | 3.8 |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 90 |
| Aisle Step (ft) | — | — | Flat Floor |
| Cabin Length - Seating (ft) | — | — | 17 |