Airbus Helicopters H225 vs Bell 525 Relentless vs Cessna 208b Grand Caravan Ex vs Cessna Citation Xls
The Airbus H225 and Bell 525 Relentless are long-range, twin‑engine helicopters aimed at offshore, SAR, and VIP missions. Both typically carry around 16–19 passengers in high-density layouts (fewer in VIP). In range, each generally sits in the roughly 500–600 nautical mile class depending on configuration and reserves, with the H225 often optimized for heavy offshore payloads and the 525 positioned as a newer-generation, high-speed executive/offshore rotorcraft. The Cessna 208B Grand Caravan EX is a single‑engine turboprop utility aircraft, best for short-to-medium regional legs. It commonly seats about 9–14 passengers (often 9 in commuter/charter configurations) and offers a range typically around 900–1,000 nautical miles, varying with payload and fuel. The Cessna Citation XLS+ is a midsize business jet focused on speed and comfort rather than rugged utility. It generally seats 7–9 passengers in standard executive layouts and has a typical range around 1,800–2,100 nautical miles, making it the longest-range option here and the best suited to point‑to‑point business travel.
| Spec | AIRBUS H225 | Bell 525 Relentless | Cessna Citation XLS+ |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 5.34 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 18 | 10 |
| Flight Rules | IFR | IFR | — |
| Manufacturer | Airbus Helicopters | Bell | Cessna Citation |
| Aircraft Name | H225 | 525 Relentless | XLS+ |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 | 1906 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.67 |
| Max Cabin Seats | 28 | 16 | 9 |
| OEM Verification | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 | 7540 |
| Standard Cabin Seats | 19 | 16 | 8 |
| Direct Operating Cost | $ 2,963 | — | $ 2,303 |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 142 | 160 | 430 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 | $15,500,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 18 | 10 |
| Max Cabin Seats | 28 | 16 | 9 |
| Standard Cabin Seats | 19 | 16 | 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 | Dual-Channel | Yes |
| Model | Makila 2A1 | CT7-2F1 | PW545C |
| Fuel Type | JetFuel | JetFuel | — |
| TBO (hrs) | 3500 | 4000 | 5000 |
| Horsepower | 2100 | 1800 | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 684 | 641 | — |
| Flat Rating | — | — | ISA + 10 |
| Thrust (lbs) | — | — | 4119 |
| Dimensions | |||
| Length (ft) | 63.4 | 61.58 | 52.5 |
| Overall Height (ft) | 16.3 | 18.18 | 17.2 |
| Rotor Diameter (ft) | 53.2 | 54.5 | — |
| Cabin Volume (cu. ft) | 547 | — | — |
| Width (ft) | — | 25.77 | — |
| Cabin Width (ft) | — | 7.58 | 5.5 |
| Cabin Height (ft) | — | 4.5 | 5.7 |
| Cabin Length (ft) | — | 15.5 | 18.5 |
| Baggage Volume Ext. (cu. ft) | — | 128 | 80 |
| Wingspan (ft) | — | — | 56.3 |
| Aisle Step (ft) | — | — | 0.7 |
| Cabin Width - Floor (ft) | — | — | 3.9 |
| Cabin Length - Seating (ft) | — | — | 14.3 |
| Baggage Volume Int. (cu. ft) | — | — | 10 |