Airbus Helicopters H225 vs Cessna Citation Xls vs Enstrom 480b vs Leonardo Aw189
The Airbus H225 and Leonardo AW189 are large, twin‑engine helicopters aimed at offshore, SAR, and utility work, while the Enstrom 480B is a much smaller, single‑engine light helicopter typically used for training, patrol, and personal/utility missions. The Cessna Citation XLS+ is a fixed‑wing light business jet optimized for fast point‑to‑point travel. On range, the Citation XLS+ generally offers the longest point‑to‑point capability (roughly about 2,000+ nautical miles depending on payload and conditions). The H225 and AW189 provide substantial helicopter ranges suited to offshore legs (commonly in the few‑hundred‑nautical‑mile class, varying with tanks, payload, and reserves). The Enstrom 480B typically has the shortest range, generally a few hundred nautical miles at most. On passenger capacity, the H225 is usually highest, often configured around 16–19 passengers in typical transport layouts. The AW189 is close behind, commonly around 16–18. The Citation XLS+ typically seats about 8–9 passengers in executive configuration. The Enstrom 480B is the smallest, typically seating about 4–5 people including the pilot.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 15.57 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Leonardo |
| Aircraft Name | H225 | XLS+ | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 651 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.74 |
| Max Cabin Seats | 28 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | — |
| Standard Cabin Seats | 19 | 8 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 2,413 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 142 | 430 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $2,413,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 21 | 10 | 21 |
| Max Cabin Seats | 28 | 9 | 19 |
| Standard Cabin Seats | 19 | 8 | 19 |
| Lavatory | — | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | No | — |
| Jump Seat | — | No | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | AFT | — |
| Cabin Pressure (psi) | — | 9.3 | — |
| Galley / Refreshment | — | Galley | — |
| SL Cabin Altitude (ft) | — | 25230 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Makila 2A1 | PW545C | CT7-2E1 |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 |
| Horsepower | 2100 | — | 1983 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | — | — |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | 57.8 |
| Overall Height (ft) | 16.3 | 17.2 | 16.6 |
| Rotor Diameter (ft) | 53.2 | — | 48 |
| Cabin Volume (cu. ft) | 547 | — | 395 |
| Wingspan (ft) | — | 56.3 | — |
| Aisle Step (ft) | — | 0.7 | — |
| Cabin Width (ft) | — | 5.5 | — |
| Cabin Height (ft) | — | 5.7 | — |
| Cabin Length (ft) | — | 18.5 | — |
| Cabin Width - Floor (ft) | — | 3.9 | — |
| Cabin Length - Seating (ft) | — | 14.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | 85 |
| Baggage Volume Int. (cu. ft) | — | 10 | — |