Bell 525 Relentless vs Cessna Citation Xls vs Embraer Legacy 650 E vs Leonardo Aw189
The Bell 525 Relentless and Leonardo AW189 are twin‑engine helicopters aimed at offshore, VIP, and utility roles, while the Cessna Citation XLS+ and Embraer Legacy 650E are fixed‑wing business jets optimized for faster point‑to‑point travel. In category terms, the 525 is a “super‑medium” class helicopter and the AW189 is a “super‑medium”/medium‑heavy helicopter, typically offering more cabin volume per mile than jets but at much lower cruise speeds. The Citation XLS+ is a midsize jet suited to efficient regional and transcontinental missions, whereas the Legacy 650E is a large‑cabin long‑range jet designed for higher endurance and comfort on longer routes. For range, the helicopters generally cover a few hundred nautical miles in typical configurations, often under about 500 nm depending on payload and reserves, while the Citation XLS+ is roughly in the ~2,000 nm class and the Legacy 650E about ~3,900–4,000 nm, making the Embraer the clear leader for nonstop distance. For passenger capacity, the AW189 can seat the most in high‑density layouts (often up to around 16–19), the Bell 525 commonly seats around 12–16, the Citation XLS+ typically 8–9, and the Legacy 650E usually 13–14 in executive layouts.
| Spec | Bell 525 Relentless | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Cessna Citation | Leonardo |
| Aircraft Name | 525 Relentless | XLS+ | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 1906 | 651 |
| Max Cabin Seats | 16 | 9 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 7540 | — |
| Standard Cabin Seats | 16 | 8 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 160 | 430 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $15,500,000 | $2,413,000 |
| DOC / nm | — | $ 5.34 | $ 15.57 |
| DOC / nm / Seat | — | $ 0.67 | $ 0.74 |
| Direct Operating Cost | — | $ 2,303 | $ 2,413 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 1 |
| Total Seats | 18 | 10 | 21 |
| Max Cabin Seats | 16 | 9 | 19 |
| Standard Cabin Seats | 16 | 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 | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | PW545C | CT7-2E1 |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 5000 | 4000 |
| Horsepower | 1800 | — | 1983 |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 10 | — |
| Thrust (lbs) | — | 4119 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 52.5 | 57.8 |
| Cabin Width (ft) | 7.58 | 5.5 | — |
| Cabin Height (ft) | 4.5 | 5.7 | — |
| Cabin Length (ft) | 15.5 | 18.5 | — |
| Overall Height (ft) | 18.18 | 17.2 | 16.6 |
| Rotor Diameter (ft) | 54.5 | — | 48 |
| Baggage Volume Ext. (cu. ft) | 128 | 80 | 85 |
| 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 | — |
| Cabin Volume (cu. ft) | — | — | 395 |