Airbus Helicopters H125 vs Bell 407gxi vs Leonardo Aw119kx vs Leonardo Aw169 vs Leonardo Sh09 vs Md Helicopters Md 500e
Airbus Helicopters’ H125 and MD Helicopters’ MD 500E sit in the light single‑engine utility class: the H125 is the more “workhorse” option with generally longer range and higher useful load, typically carrying a pilot plus about five to six passengers, while the MD 500E is smaller, faster-feeling in handling, and commonly configured for a pilot plus four passengers with a shorter practical range. Bell’s 407GXi and Leonardo’s AW119Kx are also single‑engine light utility helicopters; both usually seat a pilot plus five to six passengers, with broadly comparable range, with the 407GXi often favored for smoothness and cruise efficiency and the AW119Kx noted for cabin volume in its class. Leonardo’s AW169 moves up to the light‑intermediate twin‑engine category, offering higher speed, more redundancy, and a larger cabin, typically carrying around eight to ten passengers with longer range options. Leonardo’s SH09, as a modern light single‑engine design, is aimed at the H125/407/AW119Kx space, typically around five passengers plus pilot, with range expected to be in the same general bracket depending on final configuration.
| Spec | AIRBUS H125 | Bell 407GXi | AGUSTA / LEONARDO AW119Kx | AGUSTA / LEONARDO AW169 | AGUSTA / LEONARDO SH09 | MD Helicopters MD 500E |
|---|---|---|---|---|---|---|
| Summary | ||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 4.43 | $ 6.76 | $ 11.84 | $4.48 | $ 2.95 |
| Min Crew | 1 | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 12 | 8 | 4 |
| Flight Rules | VFR | VFR | VFR | IFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Bell | Leonardo | Leonardo | Leonardo | MD Helicotpers |
| Aircraft Name | H125 | 407GXi | AW119Kx | AW169 | SH09 | MD 500E |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | In-Development | FAA / EASA |
| Max Range (nm) | 341 | 337 | 515 | 440 | 430 | 258 |
| DOC / nm / Seat | $ 0.77 | $ 0.74 | $ 0.84 | $ 0.99 | $0.56 | $ 0.74 |
| Max Cabin Seats | 5 | 5 | 6 | 10 | 6 | 3 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2300 | — | — | — | 1483 |
| Standard Cabin Seats | 4 | 5 | 6 | 10 | 6 | 2 |
| Direct Operating Cost | $ 627 | $ 589 | $ 885 | $ 1,658 | $627 | $ 398 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G1000H NXI | Garmin G1000H | EFIS | EFIS | Gyro / Analog |
| Max Cruise Speed (ktas) | 136 | 133 | 131 | 140 | 140 | 135 |
| Base Aircraft Price (USD) | $3,200,000 | $3,225,000 | $3,850,000 | $9,450,000 | $3,500,000 | $ 2,750,000 |
| Max Passengers | — | — | — | — | 7 | — |
| Cabin | ||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 6 | 8 | 12 | 8 | 4 |
| Max Cabin Seats | 5 | 5 | 6 | 10 | — | 3 |
| Standard Cabin Seats | 4 | 5 | 6 | 10 | 6 | 2 |
| Engine | ||||||
| FADEC | Yes | Yes | Yes | Yes | Yes | No |
| Model | Arriel 2D | M250-C47E/4 | PT6B-37A | PW210A | HTS 900 | 250-C20B |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 3500 | 4500 | 4000 | 5500 | 3500 |
| Horsepower | 847 | 862 | 917 | 1000 | 1020 | 420 |
| No. of Engines | 1 | 1 | 1 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 127.8 | 160 | — | — | 64 |
| Fuel Burn (gph) | — | 46 | — | — | — | 35 |
| Dimensions | ||||||
| Length (ft) | 42.5 | 41.4 | 42.5 | 48.1 | — | 30.9 |
| Overall Height (ft) | 10 | 10.2 | 11.9 | 14.8 | — | 8.7 |
| Rotor Diameter (ft) | 36.1 | 35 | 35.5 | — | — | 26.4 |
| Width (ft) | — | 25.4 | — | — | — | — |
| Cabin Width (ft) | — | 5 | — | — | — | — |
| Cabin Height (ft) | — | 3.9 | — | — | — | — |
| Cabin Volume (cu. ft) | — | 125 | — | 222.5 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 16 | — | 49.5 | — | — |