Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Cessna Citation Xls vs Daher Tbm 960
The Airbus H225 is a heavy twin‑engine helicopter, best suited to offshore and utility missions where vertical lift matters more than speed. Its typical range is roughly 450–700 nautical miles (mission‑dependent), and it commonly carries about 16–19 passengers (with configurations that can vary widely). The Beechcraft King Air 360ER is a twin‑turboprop airplane aimed at efficient regional travel and special missions. It offers long endurance with an approximate range around 1,500–1,800 nautical miles, and typical seating is about 6–9 passengers (higher in commuter layouts). The Cessna Citation XLS+ is a midsize business jet optimized for faster point‑to‑point trips. Its range is about 1,900–2,100 nautical miles, and it generally seats 8–9 passengers in executive configurations. The Daher TBM 960 is a high‑performance single‑engine turboprop focused on owner‑pilot efficiency and speed. Its range is typically around 1,400–1,700 nautical miles, with seating for about 4–6 passengers (up to 6).
| 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 | — |