Airbus Helicopters H225 vs Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Robinson R66
The Airbus H225 is a large twin‑engine helicopter built for offshore transport, SAR, and utility work. It typically carries around 19 passengers (high‑density configurations can be higher) and offers roughly 450–550 nautical miles of range depending on tanks, payload, and reserves. The Dassault Falcon 8X is a long‑range tri‑jet business aircraft focused on fast point‑to‑point travel; it usually seats about 12–16 passengers in executive layouts and can fly about 6,450 nautical miles, far exceeding the others. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter (often used for law enforcement, EMS, and corporate shuttle) with typical seating for 6–8 passengers and a range around 250–350 nautical miles. The Robinson R66 is a light single‑engine helicopter aimed at private and utility missions; it generally carries 4 passengers plus a pilot (5 total) and has about 300–350 nautical miles of range. Overall, the Falcon 8X dominates range and cruise efficiency, while the helicopters trade speed and distance for vertical access and hover capability.
| Spec | AIRBUS H225 | Dassault Falcon 8X |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 7.66 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Dassault Falcon |
| Aircraft Name | H225 | 8X |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.64 |
| Max Cabin Seats | 28 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 36900 |
| Standard Cabin Seats | 19 | 14 |
| Direct Operating Cost | $ 2,963 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 62,500,000 |
| Cabin | ||
| Cockpit | 2 | 3 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 17 |
| Max Cabin Seats | 28 | 16 |
| Standard Cabin Seats | 19 | 14 |
| Lavatory | — | 2 Enclosed Flushing |
| Crew Rest | — | No |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD / AFT |
| Cabin Pressure (psi) | — | 10.2 |
| Galley / Refreshment | — | Galley |
| SL Cabin Altitude (ft) | — | 29200 |
| Max Cabin Altitude (ft) | — | 3900 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Makila 2A1 | PW307D |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | On-Condition |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 3 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 17 |
| Thrust (lbs) | — | 6722 |
| Dimensions | ||
| Length (ft) | 63.4 | 80.2 |
| Overall Height (ft) | 16.3 | 26.1 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | 1695 |
| Wingspan (ft) | — | 86.3 |
| Cabin Width (ft) | — | 7.7 |
| Cabin Height (ft) | — | 6.2 |
| Cabin Length (ft) | — | 42.7 |
| Cabin Width - Floor (ft) | — | 6.3 |
| Cabin Length - Seating (ft) | — | 29.2 |
| Baggage Volume Int. (cu. ft) | — | 140 |