Airbus Helicopters H125 vs Bell 407gxi vs Bell 505 Jetranger X vs Md Helicopters Md 500e
All four are light, single‑engine helicopters, but they sit in slightly different sub‑classes. The Airbus Helicopters H125 is a higher‑performance light single (often used for utility and high‑hot work) with a typical range around 340–350 nm and seating commonly for 5–6 passengers plus a pilot (depending on configuration). The Bell 407GXi is also a light single, positioned as a fast, versatile utility/passenger platform, with typical range roughly 330–360 nm and usually up to 6 passengers plus a pilot. The Bell 505 JetRanger X is a lighter, more cost‑focused light single, with a shorter typical range around 300–320 nm and generally up to 4 passengers plus a pilot. The MD Helicopters MD 500E is a light single in the “light utility”/“hot‑rod” family known for agility and compact size; typical range is about 230–260 nm, and it usually seats about 4 passengers plus a pilot (often fewer depending on mission fit).
| Spec | AIRBUS H125 | Bell 407GXi | Bell 505 JetRanger X | MD Helicopters MD 500E |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.43 | $ 3.53 | $ 2.95 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 5 | 4 |
| Flight Rules | VFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Bell | MD Helicotpers |
| Aircraft Name | H125 | 407GXi | 505 JetRanger X | MD 500E |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 337 | 306 | 258 |
| DOC / nm / Seat | $ 0.77 | $ 0.74 | $ 0.71 | $ 0.74 |
| Max Cabin Seats | 5 | 5 | — | 3 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 2189 | 2300 | 1500 | 1483 |
| Standard Cabin Seats | 4 | 5 | 3 | 2 |
| Direct Operating Cost | $ 627 | $ 589 | $ 441 | $ 398 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H NXI | Garmin G1000H | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 133 | 125 | 135 |
| Base Aircraft Price (USD) | $3,200,000 | $3,225,000 | $1,445,000 | $ 2,750,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 5 | 4 |
| Max Cabin Seats | 5 | 5 | — | 3 |
| Standard Cabin Seats | 4 | 5 | 3 | 2 |
| Engine | ||||
| FADEC | Yes | Yes | Dual-Channel | No |
| Model | Arriel 2D | M250-C47E/4 | Arrius 2R | 250-C20B |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 3500 | 4000 | 3500 |
| Horsepower | 847 | 862 | 505 | 420 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 127.8 | 84.85 | 64 |
| Fuel Burn (gph) | — | 46 | 32.3 | 35 |
| Dimensions | ||||
| Length (ft) | 42.5 | 41.4 | 42.48 | 30.9 |
| Overall Height (ft) | 10 | 10.2 | 10.65 | 8.7 |
| Rotor Diameter (ft) | 36.1 | 35 | 37 | 26.4 |
| Width (ft) | — | 25.4 | 6.51 | — |
| Cabin Width (ft) | — | 5 | 4.66 | — |
| Cabin Height (ft) | — | 3.9 | 2.75 | — |
| Cabin Volume (cu. ft) | — | 125 | 137 | — |
| Baggage Volume Ext. (cu. ft) | — | 16 | 18 | — |
| Cabin Length (ft) | — | — | 7.17 | — |