Airbus Helicopters H225 vs Bell 525 Relentless vs Cessna Citation Xls vs Enstrom 480b
The Airbus H225 and Bell 525 Relentless are large, long-range helicopters aimed at offshore, search-and-rescue, and high-end transport. The H225 is a heavy helicopter with typically around 19 passengers in a high-density layout and a practical range on the order of roughly 450–500 nautical miles depending on mission fit. The Bell 525 is a “super-medium” helicopter, generally configured for about 16–20 passengers, with a similar offshore-oriented range commonly quoted around the 500-nautical-mile class. The Cessna Citation XLS+ is a light-to-midsize business jet rather than a helicopter, optimized for fast point-to-point travel. It typically carries about 7–9 passengers and offers significantly longer range than the helicopters, roughly around 1,900–2,100 nautical miles, depending on payload and conditions. The Enstrom 480B is a much smaller single-engine helicopter used for utility, patrol, and training roles. It carries about 4–5 occupants and has a far shorter range, commonly in the ~200–300 nautical mile range, varying with reserves and configuration.
| 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 |