Airbus Helicopters H135 vs Bell 407gxi
The Airbus Helicopters H135 and Bell 407GXi occupy different niches within the light helicopter category. The H135 is a light twin‑engine helicopter typically positioned for roles that prioritize redundancy and multi‑mission capability, such as EMS, law enforcement, and offshore support. The Bell 407GXi is a light single‑engine helicopter more often associated with utility, corporate, and sightseeing missions where simplicity and lower operating complexity are valued. In range, the 407GXi commonly offers a longer typical range in standard configurations, while the H135’s range varies notably with equipment fit and mission load, and is often optimized around multi‑role operations rather than maximum endurance. For passenger capacity, both can be configured for similar headcounts in passenger transport, but the H135’s cabin design often emphasizes flexible layouts (including medical interiors) and can accommodate a pilot plus several passengers depending on configuration. The 407GXi generally carries a pilot plus a comparable number of passengers, with strong emphasis on cabin comfort and useful load for single‑engine operations.
| Spec | AIRBUS H135 | Bell 407GXi |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 6.33 | $ 4.43 |
| Min Crew | 1 | 1 |
| Total Seats | 9 | 6 |
| Flight Rules | IFR | VFR |
| Manufacturer | Airbus Helicopters | Bell |
| Aircraft Name | H135 | 407GXi |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 342 | 337 |
| DOC / nm / Seat | $ 0.79 | $ 0.74 |
| Max Cabin Seats | 7 | 5 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3124 | 2300 |
| Standard Cabin Seats | 7 | 5 |
| Direct Operating Cost | $ 861 | $ 589 |
| Flight Deck (Base Spec) | Helionix | Garmin G1000H NXI |
| Max Cruise Speed (ktas) | 136 | 133 |
| Base Aircraft Price (USD) | $6,150,000 | $3,225,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 1 | 1 |
| Total Seats | 9 | 6 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 7 | 5 |
| Standard Cabin Seats | 7 | 5 |
| Engine | ||
| FADEC | Yes | Yes |
| Model | Arrius 2B2+ | M250-C47E/4 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 4000 | 3500 |
| Horsepower | 660 | 862 |
| No. of Engines | 2 | 1 |
| Fuel Burn (gph) | — | 46 |
| Fuel Capacity (gal) | — | 127.8 |
| Dimensions | ||
| Length (ft) | 33.5 | 41.4 |
| Overall Height (ft) | 12.6 | 10.2 |
| Rotor Diameter (ft) | 34 | 35 |
| Cabin Volume (cu. ft) | 173 | 125 |
| Width (ft) | — | 25.4 |
| Cabin Width (ft) | — | 5 |
| Cabin Height (ft) | — | 3.9 |
| Baggage Volume Ext. (cu. ft) | — | 16 |