Airbus Helicopters H125 vs Airbus Helicopters H130 vs Md Helicopters Md 500e vs Md Helicopters Md 530f
The Airbus Helicopters H125 and H130 are light single‑engine utility helicopters, while the MD Helicopters MD 500E and MD 530F are light single‑engine helicopters in the MD 500 “NOTAR/500” family, typically optimized for agile utility and mission work. In category terms, the H130 is best described as a light single focused on passenger comfort and tourism/VIP-style operations, whereas the H125 is a more rugged light utility/“hot and high” workhorse often chosen for lift and external-load roles. The MD 500E is a lighter, highly maneuverable light utility platform, and the MD 530F is the higher‑performance variant geared toward better hot‑and‑high capability and demanding missions. For range, all four generally sit in the same broad light‑single bracket, but typical configurations place the H125 and H130 around the mid‑300 nautical mile class, with the MD 500E and MD 530F commonly somewhat shorter unless equipped with auxiliary fuel. For passenger capacity, the H130 usually carries the most (typically 1 pilot plus up to 6 passengers), the H125 commonly follows (often 1 plus up to 5), while the MD 500E and MD 530F are typically configured for smaller loads (often 1 plus 4).
| Spec | AIRBUS H125 | AIRBUS H130 | MD Helicopters MD 500E | MD Helicopters MD 530F |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| DOC / nm | $ 4.61 | $ 5.00 | $ 2.95 | $ 3.59 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 7 | 4 | 4 |
| Flight Rules | VFR | VFR | VFR | VFR |
| Manufacturer | Airbus Helicopters | Airbus Helicopters | MD Helicotpers | MD Helicotpers |
| Aircraft Name | H125 | H130 | MD 500E | MD 530F |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 341 | 333 | 258 | 216 |
| DOC / nm / Seat | $ 0.77 | $ 0.71 | $ 0.74 | $ 0.90 |
| Max Cabin Seats | 5 | 5 | 3 | 3 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 2189 | 2299 | 1483 | 1509 |
| Standard Cabin Seats | 4 | 4 | 2 | 2 |
| Direct Operating Cost | $ 627 | $ 640 | $ 398 | $ 480 |
| Flight Deck (Base Spec) | Garmin G500H | Garmin G500H | Gyro / Analog | Garmin G500H |
| Max Cruise Speed (ktas) | 136 | 128 | 135 | 134 |
| Base Aircraft Price (USD) | $3,200,000 | $3,450,000 | $ 2,750,000 | $ 3,400,000 |
| Cabin | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 6 | 7 | 4 | 4 |
| Max Cabin Seats | 5 | 5 | 3 | 3 |
| Standard Cabin Seats | 4 | 4 | 2 | 2 |
| Engine | ||||
| FADEC | Yes | Yes | No | No |
| Model | Arriel 2D | Arriel 2D | 250-C20B | 250-C30 |
| Fuel Type | JetFuel | JetFuel | JetFuel | JetFuel |
| TBO (hrs) | 5000 | 5000 | 3500 | 2000 |
| Horsepower | 847 | 952 | 420 | 650 |
| No. of Engines | 1 | 1 | 1 | 1 |
| Fuel Capacity (gal) | 143 | 143 | 64 | 64 |
| Fuel Burn (gph) | — | — | 35 | 35 |
| Dimensions | ||||
| Length (ft) | 42.5 | 41.5 | 30.9 | 32.2 |
| Overall Height (ft) | 10 | 11.1 | 8.7 | 8.7 |
| Rotor Diameter (ft) | 36.1 | 35.1 | 26.4 | 27.5 |