Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Cessna Citation Xls vs Embraer Legacy 650 E
The Airbus H225 is a large twin‑engine helicopter suited to offshore, SAR, and utility work; it typically carries around 16–19 passengers in passenger layouts, with practical range roughly 400–600 nautical miles depending on payload and reserves. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft optimized for short, unimproved strips and regional hops; it commonly seats 9–14 passengers, with range typically about 900–1,000 nautical miles. The Cessna Citation XLS+ is a super‑light business jet aimed at fast point‑to‑point travel; it generally accommodates 7–9 passengers, with range around 1,900–2,100 nautical miles. The Embraer Legacy 650E is a large‑cabin long‑range business jet designed for transcontinental missions and higher comfort; it usually seats about 10–13 passengers, with range roughly 3,700–3,900 nautical miles. Overall, capacity and range rise from helicopter and utility turboprop to super‑light jet, and peak with the large‑cabin Legacy 650E.
| Spec | AIRBUS H225 | Cessna Citation XLS+ |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 10 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Cessna Citation |
| Aircraft Name | H225 | XLS+ |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 |
| Max Cabin Seats | 28 | 9 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 |
| Standard Cabin Seats | 19 | 8 |
| Direct Operating Cost | $ 2,963 | $ 2,303 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 430 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 10 |
| Max Cabin Seats | 28 | 9 |
| Standard Cabin Seats | 19 | 8 |
| 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 |
| Model | Makila 2A1 | PW545C |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | 5000 |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Flat Rating | — | ISA + 10 |
| Thrust (lbs) | — | 4119 |
| Dimensions | ||
| Length (ft) | 63.4 | 52.5 |
| Overall Height (ft) | 16.3 | 17.2 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| 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 |
| Baggage Volume Int. (cu. ft) | — | 10 |