Airbus Helicopters H225 vs Cessna Citation Xls vs Daher Tbm 960 vs Robinson R66
The Airbus H225 is a large, twin‑engine helicopter aimed at offshore transport and utility missions; it carries the most people (typically around 16–19 passengers in transport layouts) and offers long helicopter range on the order of roughly 450–600 nautical miles depending on configuration and reserves. The Robinson R66 is a light single‑engine helicopter for personal, training, and light utility use; it carries about 4 passengers plus a pilot (or up to 5 seats total) and has a much shorter range, roughly 300–350 nautical miles. The Cessna Citation XLS+ is a midsize business jet designed for fast, comfortable point‑to‑point travel; it typically seats about 7–9 passengers and has a range around 1,800–2,100 nautical miles. The Daher TBM 960 is a high‑performance single‑engine turboprop positioned between piston aircraft and jets; it generally carries 4–6 passengers (up to 6 seats plus pilot depending on interior) and delivers long range for its class, commonly around 1,400–1,700 nautical miles.
| 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 | — |