Airbus Acj350 vs Airbus Helicopters H175
The Airbus ACJ350 is a long-range, large-cabin VIP airliner designed for intercontinental travel, while the Airbus Helicopters H175 is a medium-class helicopter optimized for regional missions and point-to-point access where runways are unavailable. In category terms, the ACJ350 sits in the ultra-long-range business jet/VIP transport segment based on a widebody airliner platform, emphasizing spacious living areas, high cruise speed, and global connectivity; the H175 is a twin-engine helicopter aimed at executive transport, offshore energy support, and search-and-rescue-style utility with vertical takeoff and landing flexibility. For range, an ACJ350 typically covers roughly 10,000–11,000 nautical miles depending on configuration, enabling nonstop flights such as Europe to Australia or North America to Asia, whereas the H175 is generally around 600–700 nautical miles with reserves, suited to shorter legs and frequent hops. Passenger capacity also differs sharply: an ACJ350 can be outfitted for a few dozen VIP passengers, often around 20–50 depending on layout, while the H175 usually carries about 12–16 passengers in a typical transport configuration.
| Spec | Airbus ACJ350 | AIRBUS H175 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| Min Crew | 4 | 2 |
| Total Seats | 12 | 18 |
| Manufacturer | Airbus | Airbus Helicopters |
| Aircraft Name | ACJ350 | H175 |
| Certification | FAA / EASA | FAA / EASA |
| Max Cabin Seats | 35 | 18 |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 32500 | 6797 |
| Flight Deck (Base Spec) | Thales | EFIS |
| Max Cruise Speed (ktas) | 470 | 149 |
| Base Aircraft Price (USD) | $366,000,000 | $17,900,000 |
| DOC / nm | — | $ 13.53 |
| Flight Rules | — | IFR |
| Max Range (nm) | — | 573 |
| DOC / nm / Seat | — | $ 0.75 |
| Standard Cabin Seats | — | 16 |
| Direct Operating Cost | — | $ 2,016 |
| Cabin | ||
| Cockpit | — | 2 |
| Min Crew | — | 2 |
| Total Seats | — | 18 |
| Max Cabin Seats | — | 18 |
| Standard Cabin Seats | — | 16 |
| Engine | ||
| Model | Trent XWB 84 | PT6A-67E |
| Fuel Capacity (gal) | 43985 | — |
| FADEC | — | Yes |
| Fuel Type | — | JetFuel |
| TBO (hrs) | — | 3500 |
| Horsepower | — | 1775 |
| No. of Engines | — | 2 |
| Dimensions | ||
| Length (ft) | 219 ft 2 in | 59.2 |
| Wingspan (ft) | 212 ft 5 in | — |
| Cabin Width (ft) | 167 ft 5 in | — |
| Cabin Length (ft) | 167 ft 5 in | — |
| Overall Height (ft) | 55 ft 11 in | 17.5 |
| Cabin Volume (cu. ft) | 30,162 cu ft | 423.8 |
| Cabin Width - Floor (ft) | 2,905 sq ft | — |
| Rotor Diameter (ft) | — | 48.5 |
| Baggage Volume Ext. (cu. ft) | — | 81.9 |