Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Cessna Citation Xls vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are twin‑engine heavy helicopters designed for offshore transport, search and rescue, and utility missions. Both typically carry around 18–19 passengers in high‑density layouts (often fewer in VIP/mission configurations) and offer medium helicopter ranges on the order of roughly 450–550 nautical miles depending on payload, reserves, and conditions; the S‑92 is often cited slightly higher in typical range, while the H225 is broadly comparable. The Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing aircraft aimed at rugged regional, cargo, and short/remote‑strip operations. It usually seats about 9–14 passengers (common commuter layouts around 9–12) and provides longer point‑to‑point range than the helicopters, roughly 900–1,200 nautical miles depending on load and configuration. The Cessna Citation XLS+ is a twin‑engine light/midsize business jet focused on fast business travel. It generally carries about 7–9 passengers (up to about 12 in some layouts) and has the longest range of the group, roughly 1,800–2,100 nautical miles, with substantially higher cruise speed than the Caravan or the helicopters.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | $ 19.79 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 10 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Sikorsky |
| Aircraft Name | H225 | XLS+ | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | $ 0.94 |
| Max Cabin Seats | 28 | 9 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 7540 | 7417 |
| Standard Cabin Seats | 19 | 8 | 19 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | $ 3,068 |
| 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 | $30,650,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| 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 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | 5000 | 4000 |
| Horsepower | 2100 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 52.5 | — |
| Overall Height (ft) | 16.3 | 17.2 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| 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 | 140 |
| Baggage Volume Int. (cu. ft) | — | 10 | — |