Airbus Helicopters H225 vs Dassault Falcon 8x vs Piaggio Avanti Evo vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are twin‑engine heavy helicopters, typically chosen for offshore transport, search and rescue, and utility missions where vertical lift and point-to-point access matter more than speed. Their effective range is generally in the few‑hundred‑nautical‑mile class (often roughly 400–600 nm depending on payload and reserves), and they commonly carry around 16–19 passengers in transport layouts, with higher maximum seating possible in denser configurations. The Dassault Falcon 8X is a long‑range, three‑engine business jet optimized for intercontinental travel. It offers the longest range of the group at about 6,450 nm and usually seats about 8–14 passengers in executive cabin configurations. The Piaggio Avanti EVO is a twin‑turboprop business aircraft positioned between the helicopters and the Falcon 8X. It is used for regional to medium‑range trips, with a typical range around 1,500–1,800 nm and seating commonly 6–9 passengers, emphasizing efficiency and speed for its class rather than maximum cabin size.
| Spec | AIRBUS H225 | Dassault Falcon 8X | Piaggio Avanti EVO | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 | — | $ 19.79 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 8 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Dassault Falcon | Piaggio | Sikorsky |
| Aircraft Name | H225 | 8X | Avanti EVO | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 | 1530 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 | — | $ 0.94 |
| Max Cabin Seats | 28 | 16 | 7 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 36900 | 3775 | 7417 |
| Standard Cabin Seats | 19 | 14 | 6 | 19 |
| Direct Operating Cost | $ 2,963 | $ 3,805 | — | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 400 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 | $ 7,695,000 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 17 | 8 | 21 |
| Max Cabin Seats | 28 | 16 | 7 | 19 |
| Standard Cabin Seats | 19 | 14 | 6 | 19 |
| Lavatory | — | 2 Enclosed Flushing | No | — |
| Crew Rest | — | No | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Cabin Pressure (psi) | — | 10.2 | 9 | — |
| Galley / Refreshment | — | Galley | No | — |
| SL Cabin Altitude (ft) | — | 29200 | 24000 | — |
| Max Cabin Altitude (ft) | — | 3900 | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW307D | PT6A–66B | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 3600 | 4000 |
| Horsepower | 2100 | — | 850 | 2520 |
| No. of Engines | 2 | 3 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 760 |
| Flat Rating | — | ISA + 17 | ISA + 28 | — |
| Thrust (lbs) | — | 6722 | — | — |
| Fuel Burn (gph) | — | — | 100 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 80.2 | 47.3 | — |
| Overall Height (ft) | 16.3 | 26.1 | 13.1 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | 1695 | — | 775 |
| Wingspan (ft) | — | 86.3 | 47.1 | — |
| Cabin Width (ft) | — | 7.7 | 6.1 | — |
| Cabin Height (ft) | — | 6.2 | 5.8 | — |
| Cabin Length (ft) | — | 42.7 | 14.9 | — |
| Cabin Width - Floor (ft) | — | 6.3 | 3.5 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — | — |
| Baggage Volume Int. (cu. ft) | — | 140 | 35.2 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |