Airbus Helicopters H225 vs Bell 525 Relentless vs Cessna 208b Grand Caravan Ex
The Airbus H225 and Bell 525 Relentless are large, long-range twin‑engine helicopters aimed at offshore transport, SAR, and high‑end utility missions, while the Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing aircraft optimized for rugged regional hauling. In category terms, the H225 is a proven heavy/“super‑medium” class rotorcraft with strong lift and established offshore credentials; the Bell 525 is a newer super‑medium design emphasizing speed, modern avionics, and efficient long legs. The Grand Caravan EX sits in a different niche: simpler, lower operating complexity, and best where runways (even short or unimproved) are available rather than vertical lift. On range, both helicopters generally deliver long offshore-style reach, with the H225 typically around the mid‑400 nautical mile class and the Bell 525 targeting roughly the 500–600+ nautical mile class depending on fit and reserves, whereas the Caravan EX commonly reaches roughly 900–1,000+ nautical miles with reserves, benefiting from fixed‑wing efficiency. For passenger capacity, the H225 is commonly configured around 16–19 passengers, the Bell 525 about 16–20, and the 208B typically up to 9 passengers.
| Spec | AIRBUS H225 | Bell 525 Relentless |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 18 |
| Flight Rules | IFR | IFR |
| Manufacturer | Airbus Helicopters | Bell |
| Aircraft Name | H225 | 525 Relentless |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 580 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 16 |
| OEM Verification | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 6675 |
| Standard Cabin Seats | 19 | 16 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Garmin G5000H |
| Max Cruise Speed (ktas) | 142 | 160 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 2 |
| Total Seats | 21 | 18 |
| Max Cabin Seats | 28 | 16 |
| Standard Cabin Seats | 19 | 16 |
| Engine | ||
| FADEC | Yes | Dual-Channel |
| Model | Makila 2A1 | CT7-2F1 |
| Fuel Type | JetFuel | JetFuel |
| TBO (hrs) | 3500 | 4000 |
| Horsepower | 2100 | 1800 |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | 641 |
| Dimensions | ||
| Length (ft) | 63.4 | 61.58 |
| Overall Height (ft) | 16.3 | 18.18 |
| Rotor Diameter (ft) | 53.2 | 54.5 |
| Cabin Volume (cu. ft) | 547 | — |
| Width (ft) | — | 25.77 |
| Cabin Width (ft) | — | 7.58 |
| Cabin Height (ft) | — | 4.5 |
| Cabin Length (ft) | — | 15.5 |
| Baggage Volume Ext. (cu. ft) | — | 128 |