Bell 525 Relentless vs Bombardier Global 7500 vs Cessna Citation Xls vs Pilatus Pc 24
The Bell 525 Relentless is a fly-by-wire super‑medium helicopter aimed at point-to-point access and offshore/remote missions. It typically carries around 16 passengers in a high-density layout (fewer in executive interiors) and offers roughly a 500–560 nautical mile range depending on reserves and configuration. The Bombardier Global 7500 is an ultra‑long‑range large‑cabin business jet designed for intercontinental travel. It generally seats about 14–19 passengers (with higher certified maximums depending on layout) and delivers about 7,700 nautical miles of range, enabling nonstop city pairs such as New York–Hong Kong under favorable conditions. The Cessna Citation XLS+ is a midsize business jet optimized for efficient regional flying and short/medium sectors. It commonly seats 7–9 passengers in executive configuration and has an approximate 2,100 nautical mile range. The Pilatus PC‑24 is a light jet with “rugged” capabilities, notable for operating from shorter and semi‑prepared runways. It typically seats 6–10 passengers and offers about a 2,000 nautical mile range, depending on payload and conditions.
| Spec | Bell 525 Relentless | Bombardier Global 7500 | Cessna Citation XLS+ | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 10 | 6 |
| Flight Rules | IFR | — | — | — |
| Manufacturer | Bell | Bombardier | Cessna Citation | Pilatus |
| Aircraft Name | 525 Relentless | Global 7500 | XLS+ | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7700 | 1906 | 2076 |
| Max Cabin Seats | 16 | 19 | 9 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | — | 7540 | 6680 |
| Standard Cabin Seats | 16 | 12 | 8 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Bombardier Vision (Pro Line Fusion) | Rockwell Collins Pro Line 21 | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 516 | 430 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $75,000,000 | $15,500,000 | $11,800,000 |
| DOC / nm | — | $ 9.50 | $ 5.34 | $ 3.71 |
| Aircraft Type | — | Business Jet | — | — |
| DOC / nm / Seat | — | $ 0.79 | $ 0.67 | $ 0.62 |
| Direct Operating Cost | — | $ 4,900 | $ 2,303 | $ 1,619 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 | 1 |
| Total Seats | 18 | 14 | 10 | 6 |
| Max Cabin Seats | 16 | 19 | 9 | 10 |
| Standard Cabin Seats | 16 | 12 | 8 | 6 |
| Lavatory | — | 2 Enclosed Flushing | 1 Enclosed Belted Flushing | 1 Enclosed Flushing |
| Crew Rest | — | Yes | No | No |
| Jump Seat | — | Yes | No | No |
| Galley Location | — | FWD | FWD | FWD |
| Lavatory Location | — | FWD / AFT | AFT | FWD |
| Galley / Refreshment | — | Galley | Galley | Optional Refreshment Center |
| Max Cabin Altitude (ft) | — | 4500 | — | — |
| Cabin Pressure (psi) | — | — | 9.3 | 9.3 |
| SL Cabin Altitude (ft) | — | — | 25230 | 23500 |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | Passport | PW545C | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 4000 | On-Condition | 5000 | 5000 |
| Horsepower | 1800 | — | — | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Flat Rating | — | ISA + 15 | ISA + 10 | ISA + 23 |
| Thrust (lbs) | — | 18920 | 4119 | 3435 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 111 | 52.5 | 52.2 |
| Cabin Width (ft) | 7.58 | 8 | 5.5 | 5.6 |
| Cabin Height (ft) | 4.5 | 6.2 | 5.7 | 5.1 |
| Cabin Length (ft) | 15.5 | 54.5 | 18.5 | 23 |
| Overall Height (ft) | 18.18 | 27 | 17.2 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 80 | — |
| Wingspan (ft) | — | 104 | 56.3 | 55.8 |
| Aisle Step (ft) | — | — | 0.7 | Flat Floor |
| Cabin Width - Floor (ft) | — | — | 3.9 | 3.8 |
| Cabin Length - Seating (ft) | — | — | 14.3 | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 10 | 90 |