Bell 525 Relentless vs Gulfstream G700 vs Leonardo Aw189 vs Pilatus Pc 24
The Bell 525 Relentless and Leonardo AW189 are twin‑engine helicopters, while the Gulfstream G700 and Pilatus PC‑24 are fixed‑wing business jets. The Bell 525 sits in the “super‑medium” helicopter class, typically carrying about 12–16 passengers in an executive layout, with roughly 500–600 nautical miles of range depending on configuration and reserves. The AW189 is a larger “super‑medium” helicopter, commonly set up for about 12–16 passengers in VIP use (higher in offshore transport), with a similar ballpark range around 450–550 nautical miles. The Pilatus PC‑24 is a light jet designed for versatile operations, usually seating about 6–10 passengers, with range roughly around 2,000 nautical miles. The Gulfstream G700 is an ultra‑long‑range, large‑cabin jet aimed at intercontinental missions, typically accommodating around 13–19 passengers (higher density possible) and offering about 7,000+ nautical miles of range, enabling nonstop city pairs far beyond the reach of the helicopters and the PC‑24.
| Spec | Bell 525 Relentless | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 18 | 16 | 21 | 6 |
| Flight Rules | IFR | — | IFR | — |
| Manufacturer | Bell | Gulfstream | Leonardo | Pilatus |
| Aircraft Name | 525 Relentless | G700 | AW189 | PC-24 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7500 | 651 | 2076 |
| Max Cabin Seats | 16 | 19 | 19 | 10 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | — | — | 6680 |
| Standard Cabin Seats | 16 | 12 | 19 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Gulfstream Symmetry Flight Deck | EFIS | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 516 | 155 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $78,000,000 | $2,413,000 | $11,800,000 |
| DOC / nm | — | — | $ 15.57 | $ 3.71 |
| DOC / nm / Seat | — | — | $ 0.74 | $ 0.62 |
| Direct Operating Cost | — | — | $ 2,413 | $ 1,619 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 1 |
| Total Seats | 18 | 16 | 21 | 6 |
| Max Cabin Seats | 16 | 19 | 19 | 10 |
| Standard Cabin Seats | 16 | 12 | 19 | 6 |
| Crew Rest | — | Optional | — | No |
| Jump Seat | — | Yes | — | No |
| Galley Location | — | FWD | — | FWD |
| Lavatory Location | — | FWD / AFT | — | FWD |
| Lavatory | — | — | — | 1 Enclosed Flushing |
| Cargo Door | — | — | — | Yes |
| Cabin Pressure (psi) | — | — | — | 9.3 |
| Galley / Refreshment | — | — | — | Optional Refreshment Center |
| SL Cabin Altitude (ft) | — | — | — | 23500 |
| Engine | ||||
| FADEC | Dual-Channel | — | Yes | Yes |
| Model | CT7-2F1 | Pearl 700 | CT7-2E1 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | JetFuel | — |
| TBO (hrs) | 4000 | On Condition | 4000 | 5000 |
| Horsepower | 1800 | — | 1983 | — |
| No. of Engines | 2 | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — | — |
| Thrust (lbs) | — | 18250 | — | 3435 |
| Flat Rating | — | — | — | ISA + 23 |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 109.9 | 57.8 | 52.2 |
| Cabin Width (ft) | 7.58 | 8.2 | — | 5.6 |
| Cabin Height (ft) | 4.5 | 6.25 | — | 5.1 |
| Cabin Length (ft) | 15.5 | 56.9 | — | 23 |
| Overall Height (ft) | 18.18 | 25.4 | 16.6 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 85 | — |
| Wingspan (ft) | — | 103 | — | 55.8 |
| Aisle Step (ft) | — | Flat Floor | — | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | 195 | — | 90 |
| Cabin Volume (cu. ft) | — | — | 395 | — |
| Cabin Width - Floor (ft) | — | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | — | 17 |