Airbus Helicopters H225 vs Cessna Citation Xls vs Daher Tbm 960 vs Dassault Falcon 8x
The Airbus H225 is a large twin‑engine helicopter rather than a fixed‑wing airplane, optimized for offshore and utility missions with a typical range around 450–600 nautical miles and seating commonly configured for roughly 16–19 passengers (higher in dense layouts). The Cessna Citation XLS+ is a midsize business jet aimed at short‑to‑medium trips, offering about 1,900–2,100 nautical miles of range and typically seating 7–9 passengers. The Daher TBM 960 is a high‑performance single‑engine turboprop, best for efficient owner‑flown travel, with roughly 1,400–1,700 nautical miles of range (mission dependent) and usually 4–6 passengers plus a pilot. The Dassault Falcon 8X is an ultra‑long‑range heavy business jet designed for intercontinental missions, with about 6,400–6,450 nautical miles of range and typical seating for 12–16 passengers (with wider cabin flexibility). Overall, the H225 prioritizes vertical access, the TBM 960 efficiency, the XLS+ regional jet convenience, and the Falcon 8X global reach and cabin space.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Daher TBM 960 | Dassault Falcon 8X |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 2.25 | $ 7.66 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 6 | 17 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Airbus Helicopters | Cessna Citation | Daher TBM | Dassault Falcon |
| Aircraft Name | H225 | XLS+ | TBM 960 | 8X |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1730 | 6450 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.56 | $ 0.64 |
| Max Cabin Seats | 28 | 9 | — | 16 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | 2908 | 36900 |
| Standard Cabin Seats | 19 | 8 | 4 | 14 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 744 | $ 3,805 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 | Honeywell Primus EASy II |
| Max Cruise Speed (ktas) | 142 | 430 | 330 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $4,450,000 | $ 62,500,000 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 3 |
| Min Crew | 2 | 2 | 1 | 2 |
| Total Seats | 21 | 10 | 6 | 17 |
| Max Cabin Seats | 28 | 9 | — | 16 |
| Standard Cabin Seats | 19 | 8 | 4 | 14 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | 2 Enclosed Flushing |
| Crew Rest | — | No | — | No |
| Jump Seat | — | No | — | Yes |
| Galley Location | — | FWD | MID | FWD |
| Lavatory Location | — | AFT | — | FWD / AFT |
| Cabin Pressure (psi) | — | 9.3 | 6.2 | 10.2 |
| Galley / Refreshment | — | Galley | — | Galley |
| SL Cabin Altitude (ft) | — | 25230 | 14390 | 29200 |
| Max Cabin Altitude (ft) | — | — | — | 3900 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | TBM 960 | PW307D |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | 3500 | On-Condition |
| Horsepower | 2100 | — | 850 | — |
| No. of Engines | 2 | 2 | — | 3 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | ISA + 49 | ISA + 17 |
| Thrust (lbs) | — | 4119 | — | 6722 |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 35.3 | 80.2 |
| Overall Height (ft) | 16.3 | 17.2 | — | 26.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | 1695 |
| Wingspan (ft) | — | 56.3 | 42.1 | 86.3 |
| Aisle Step (ft) | — | 0.7 | — | — |
| Cabin Width (ft) | — | 5.5 | 4 | 7.7 |
| Cabin Height (ft) | — | 5.7 | 4.1 | 6.2 |
| Cabin Length (ft) | — | 18.5 | 13.4 | 42.7 |
| Cabin Width - Floor (ft) | — | 3.9 | — | 6.3 |
| Cabin Length - Seating (ft) | — | 14.3 | — | 29.2 |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | — | 140 |