Airbus Helicopters H225 vs Cessna Citation Xls vs Daher Tbm 960 vs Embraer Legacy 650 E
The Airbus H225 is a large twin‑engine helicopter, best categorized as a long‑range utility/transport rotorcraft. It typically carries around 16–19 passengers in an airline-style layout (more in high-density) and offers roughly 400–500 nautical miles of range depending on configuration and reserves, trading speed for vertical lift and access to confined sites. The Cessna Citation XLS+ is a midsize business jet aimed at short‑to‑medium missions. It generally seats 8–9 passengers and delivers about 2,000 nautical miles of range, balancing cabin comfort with the ability to use relatively shorter runways. The Daher TBM 960 is a single‑engine turboprop in the high‑performance personal/business category. It usually carries 4–6 passengers and can reach roughly 1,400–1,700 nautical miles, prioritizing efficiency and access to smaller airports over cabin size. The Embraer Legacy 650E is a large‑cabin long‑range business jet. It commonly seats 12–14 (up to about 16) and offers around 3,900 nautical miles of range, emphasizing intercontinental capability and a spacious cabin.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Daher TBM 960 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 2.25 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Daher TBM |
| Aircraft Name | H225 | XLS+ | TBM 960 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1730 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.56 |
| Max Cabin Seats | 28 | 9 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 2908 |
| Standard Cabin Seats | 19 | 8 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 744 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 430 | 330 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $4,450,000 |
| Aircraft Type | — | — | Turbo Prop |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 6 |
| Max Cabin Seats | 28 | 9 | — |
| Standard Cabin Seats | 19 | 8 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | No |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | 6.2 |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | 14390 |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | TBM 960 |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | 5000 | 3500 |
| Horsepower | 2100 | — | 850 |
| No. of Engines | 2 | 2 | — |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | ISA + 49 |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 35.3 |
| Overall Height (ft) | 16.3 | 17.2 | — |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 |
| Wingspan (ft) | — | 56.3 | 42.1 |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | 4 |
| Cabin Height (ft) | — | 5.7 | 4.1 |
| Cabin Length (ft) | — | 18.5 | 13.4 |
| Cabin Width - Floor (ft) | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — |
| Baggage Volume Int. (cu. ft) | — | 10 | — |