Airbus Helicopters H130 vs Bell 407gxi vs Airbus Helicopters H135
The Airbus H130, Bell 407GXi, and Airbus H135 sit in different light-helicopter niches. In category, the H130 and 407GXi are single‑engine light helicopters, typically favored for lower operating complexity and strong utility or tour performance, while the H135 is a twin‑engine light helicopter aimed more at missions where redundancy and higher IFR/EMS-style capability are priorities. On range, all three are broadly comparable in typical cruise planning, with the H135 often offering the longest practical range in many configurations, while the H130 and 407GXi are generally in a similar mid‑range band that varies notably with fuel fit, payload, and reserves. On passenger capacity, the H130 is commonly configured for the most passengers in its class, typically accommodating a pilot plus up to seven passengers in high‑density layouts. The Bell 407GXi is usually configured for a pilot plus five or six passengers depending on interior. The H135 commonly carries a pilot plus five or six passengers, though cabin layouts vary widely by mission.
| Spec | AIRBUS H130 | AIRBUS H135 | Bell 407GXi |
|---|---|---|---|
| Summary | |||
| Cockpit | 3 | 2 | 2 |
| DOC / nm | $ 5.00 | $ 6.33 | $ 4.43 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 7 | 9 | 6 |
| Flight Rules | VFR | IFR | VFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | Bell |
| Aircraft Name | H130 | H135 | 407GXi |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 333 | 342 | 337 |
| DOC / nm / Seat | $ 0.71 | $ 0.79 | $ 0.74 |
| Max Cabin Seats | 5 | 7 | 5 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 2299 | 3124 | 2300 |
| Standard Cabin Seats | 4 | 7 | 5 |
| Direct Operating Cost | $ 640 | $ 861 | $ 589 |
| Flight Deck (Base Spec) | Garmin G500H | Helionix | Garmin G1000H NXI |
| Max Cruise Speed (ktas) | 128 | 136 | 133 |
| Base Aircraft Price (USD) | $3,450,000 | $6,150,000 | $3,225,000 |
| Cabin | |||
| Cockpit | 3 | 2 | 2 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 7 | 9 | 6 |
| Max Cabin Seats | 5 | 7 | 5 |
| Standard Cabin Seats | 4 | 7 | 5 |
| Configuration | — | Green Interior | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Arriel 2D | Arrius 2B2+ | M250-C47E/4 |
| Fuel Type | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 4000 | 3500 |
| Horsepower | 952 | 660 | 862 |
| No. of Engines | 1 | 2 | 1 |
| Fuel Capacity (gal) | 143 | — | 127.8 |
| Fuel Burn (gph) | — | — | 46 |
| Dimensions | |||
| Length (ft) | 41.5 | 33.5 | 41.4 |
| Overall Height (ft) | 11.1 | 12.6 | 10.2 |
| Rotor Diameter (ft) | 35.1 | 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 |