Airbus Helicopters H225 vs Cessna Citation Xls vs Daher Tbm 960 vs Piaggio Avanti Evo
The Airbus H225 is a large twin‑engine helicopter rather than a fixed‑wing airplane, optimized for vertical lift, offshore and utility missions. It typically carries a larger group (often around 16–19 passengers depending on configuration) but has a shorter point‑to‑point range than the airplanes, generally in the few‑hundred‑nautical‑mile class and roughly up to about 500–600 nm with reserves depending on fit and payload. The Cessna Citation XLS+ is a light business jet designed for fast, comfortable regional travel. It commonly seats about 8–9 passengers in a corporate layout and offers an IFR range on the order of roughly 1,800–2,100 nm. The Daher TBM 960 is a single‑engine turboprop, typically configured for 4–6 passengers plus pilot, trading jet speed for efficiency and access to shorter runways. Its range is broadly comparable to light jets in many missions, around roughly 1,400–1,700 nm. The Piaggio Avanti EVO is a twin‑turboprop business aircraft, usually seating about 6–8 passengers, with jet‑like cruise for a turboprop and an approximate range around 1,500–1,800 nm.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Daher TBM 960 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 2.25 | — |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 6 | 8 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Daher TBM | Piaggio |
| Aircraft Name | H225 | XLS+ | TBM 960 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 1730 | 1530 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.56 | — |
| Max Cabin Seats | 28 | 9 | — | 7 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 2908 | 3775 |
| Standard Cabin Seats | 19 | 8 | 4 | 6 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 744 | — |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 430 | 330 | 400 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $4,450,000 | $ 7,695,000 |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 | 1 |
| Total Seats | 21 | 10 | 6 | 8 |
| Max Cabin Seats | 28 | 9 | — | 7 |
| Standard Cabin Seats | 19 | 8 | 4 | 6 |
| Lavatory | — | 1 Enclosed Belted Flushing | No | No |
| Crew Rest | — | No | — | — |
| Jump Seat | — | No | — | — |
| Galley Location | — | FWD | MID | — |
| Lavatory Location | — | AFT | — | — |
| Cabin Pressure (psi) | — | 9.3 | 6.2 | 9 |
| Galley / Refreshment | — | Galley | — | No |
| SL Cabin Altitude (ft) | — | 25230 | 14390 | 24000 |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | TBM 960 | PT6A–66B |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | 3500 | 3600 |
| Horsepower | 2100 | — | 850 | 850 |
| No. of Engines | 2 | 2 | — | 2 |
| Fuel Capacity (gal) | 684 | — | — | — |
| Flat Rating | — | ISA + 10 | ISA + 49 | ISA + 28 |
| Thrust (lbs) | — | 4119 | — | — |
| Fuel Burn (gph) | — | — | — | 100 |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 35.3 | 47.3 |
| Overall Height (ft) | 16.3 | 17.2 | — | 13.1 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 123 | — |
| Wingspan (ft) | — | 56.3 | 42.1 | 47.1 |
| Aisle Step (ft) | — | 0.7 | — | — |
| Cabin Width (ft) | — | 5.5 | 4 | 6.1 |
| Cabin Height (ft) | — | 5.7 | 4.1 | 5.8 |
| Cabin Length (ft) | — | 18.5 | 13.4 | 14.9 |
| Cabin Width - Floor (ft) | — | 3.9 | — | 3.5 |
| Cabin Length - Seating (ft) | — | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | — | 35.2 |