Airbus Acj320 vs Md Helicopters Md 530f
The Airbus ACJ330neo and the MD Helicopters MD 530F sit in entirely different aircraft categories. The ACJ330neo is a long‑range, widebody VIP airliner derivative designed for intercontinental travel with airline-level comfort and extensive cabin customization, while the MD 530F is a light, single‑engine utility helicopter optimized for short-range missions such as patrol, training, light transport, and operations from confined or unimproved sites. In range, the ACJ330neo is built for long nonstop legs measured in thousands of nautical miles, enabling true global routing with few stops depending on configuration. The MD 530F’s range is comparatively short, typically a few hundred nautical miles, and it is more sensitive to payload, reserve requirements, and hover/mission profiles. Passenger capacity also differs dramatically. The ACJ330neo can be configured to carry a small number of VIPs in very spacious layouts or a much larger group in higher-density arrangements, whereas the MD 530F generally carries a pilot plus a small number of passengers, with practical seating usually limited to a handful.
| Spec | Airbus ACJ330 Neo | MD Helicopters MD 530F |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 16.95 | $ 3.59 |
| Min Crew | 4 | 1 |
| Total Seats | 12 | 4 |
| Manufacturer | Airbus | MD Helicotpers |
| Aircraft Name | ACJ330 Neo | MD 530F |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 6000 | 216 |
| DOC / nm / Seat | $ 2.12 | $ 0.90 |
| Max Cabin Seats | 35 | 3 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 28800 | 1509 |
| Standard Cabin Seats | 8 | 2 |
| Direct Operating Cost | $ 7,965 | $ 480 |
| Flight Deck (Base Spec) | Thales | Garmin G500H |
| Max Cruise Speed (ktas) | 470 | 134 |
| Base Aircraft Price (USD) | $101,500,000 | $ 3,400,000 |
| Flight Rules | — | VFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 4 | 1 |
| Total Seats | 10 | 4 |
| Configuration | Green Interior | — |
| Max Cabin Seats | 35 | 3 |
| Standard Cabin Seats | 8 | 2 |
| Engine | ||
| FADEC | Yes | No |
| Model | CFM LEAP-1A27 | 250-C30 |
| TBO (hrs) | On-Condition | 2000 |
| Thrust (lbs) | 29000 | — |
| No. of Engines | 2 | 1 |
| Fuel Type | — | JetFuel |
| Horsepower | — | 650 |
| Fuel Burn (gph) | — | 35 |
| Fuel Capacity (gal) | — | 64 |
| Dimensions | ||
| Length (ft) | 123.3 | 32.2 |
| Wingspan (ft) | 117.5 | — |
| Cabin Width (ft) | 12.1 | — |
| Cabin Height (ft) | 7.4 | — |
| Cabin Length (ft) | 91 | — |
| Overall Height (ft) | 38.58 | 8.7 |
| Cabin Volume (cu. ft) | 7700 | — |
| Baggage Volume Ext. (cu. ft) | 1324 | — |
| Rotor Diameter (ft) | — | 27.5 |