Bell 525 Relentless vs Bombardier Global 7500 vs Cessna Citation Xls vs Leonardo Aw189
The Bell 525 Relentless and Leonardo AW189 are super‑medium helicopters, optimized for point‑to‑point flexibility, vertical access, and shorter stage lengths than jets. The Bell 525 typically offers roughly 500–600 nautical miles of range with IFR reserves (mission‑dependent) and is commonly configured for about 12–16 passengers. The AW189 is in a similar role, generally around 450–500 nautical miles (mission‑dependent) and often configured for about 12–16 passengers, with layouts varying widely between offshore and VIP use. The Cessna Citation XLS+ is a midsize business jet, faster and higher‑flying than the helicopters, suited to regional-to-continental trips. It typically carries about 7–9 passengers in executive seating and has an approximate range near 2,000 nautical miles. The Bombardier Global 7500 is an ultra‑long‑range business jet designed for intercontinental missions. It typically seats about 14–19 passengers in executive configurations (with higher maximums possible) and offers roughly 7,700 nautical miles of range, enabling nonstop city pairs that are out of reach for midsize jets and any helicopter.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Cessna Citation XLS+ | AGUSTA / LEONARDO AW189 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 10 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Bell | Bombardier | Cessna Citation | Leonardo |
| Aircraft Name | 525 Relentless | Global 7500 | XLS+ | AW189 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 1906 | 651 |
| Max Cabin Seats | 16 | 19 | 9 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | — | 7540 | — |
| Standard Cabin Seats | 16 | 12 | 8 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | EFIS |
| Max Cruise Speed (ktas) | 160 | 516 | 430 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $15,500,000 | $2,413,000 |
| DOC / nm | — | $ 9.50 | $ 5.34 | $ 15.57 |
| Aircraft Type | — | Business Jet | — | — |
| DOC / nm / Seat | — | $ 0.79 | $ 0.67 | $ 0.74 |
| Direct Operating Cost | — | $ 4,900 | $ 2,303 | $ 2,413 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 10 | 21 |
| Max Cabin Seats | 16 | 19 | 9 | 19 |
| Standard Cabin Seats | 16 | 12 | 8 | 19 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | — |
| Crew Rest | — | Yes | No | — |
| Jump Seat | — | Yes | No | — |
| Galley Location | — | FWD | FWD | — |
| Lavatory Location | — | FWD / AFT | AFT | — |
| Galley / Refreshment | — | Galley | Galley | — |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 9.3 | — |
| SL Cabin Altitude (ft) | — | — | 25230 | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | Passport | PW545C | CT7-2E1 |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 4000 | On-Condition | 5000 | 4000 |
| Horsepower | 1800 | — | — | 1983 |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | — |
| Thrust (lbs) | — | 18920 | 4119 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 111 | 52.5 | 57.8 |
| Cabin Width (ft) | 7.58 | 8 | 5.5 | — |
| Cabin Height (ft) | 4.5 | 6.2 | 5.7 | — |
| Cabin Length (ft) | 15.5 | 54.5 | 18.5 | — |
| Overall Height (ft) | 18.18 | 27 | 17.2 | 16.6 |
| Rotor Diameter (ft) | 54.5 | — | — | 48 |
| Baggage Volume Ext. (cu. ft) | 128 | — | 80 | 85 |
| Wingspan (ft) | — | 104 | 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 |