Bell 525 Relentless vs Gulfstream G700 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Pilatus Pc 24
The Bell 525 Relentless and the MD Helicopters (McDonnell Douglas) 902 Explorer are helicopters, while the Gulfstream G700 and Pilatus PC-24 are fixed‑wing business jets. In category and mission, the 525 is a super‑medium helicopter aimed at offshore and corporate transport, whereas the 902 Explorer is a light utility/turbine helicopter commonly used for EMS, law enforcement, and short corporate hops. The G700 is an ultra‑long‑range, large‑cabin business jet designed for intercontinental travel, while the PC-24 is a light/“super versatile” business jet optimized for shorter runways and mixed passenger/cargo use. On range, the G700 is far ahead at roughly 7,500+ nautical miles, enabling nonstop long-haul city pairs. The PC-24 is midrange for a jet at about 2,000 nautical miles. Helicopters are much shorter-range by comparison: the Bell 525 is roughly in the 500–600 nautical mile class, and the 902 Explorer is typically around 300 nautical miles. For passenger capacity, the G700 generally seats about 13–19, the PC-24 typically 6–10, the Bell 525 around 16–20 depending on layout, and the 902 Explorer usually about 6–8.
| Spec | Bell 525 Relentless | Gulfstream G700 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 18 | 16 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Bell | Gulfstream | Pilatus |
| Aircraft Name | 525 Relentless | G700 | PC-24 |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 580 | 7500 | 2076 |
| Max Cabin Seats | 16 | 19 | 10 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 6675 | — | 6680 |
| Standard Cabin Seats | 16 | 12 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Gulfstream Symmetry Flight Deck | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 516 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $78,000,000 | $11,800,000 |
| DOC / nm | — | — | $ 3.71 |
| DOC / nm / Seat | — | — | $ 0.62 |
| Direct Operating Cost | — | — | $ 1,619 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 18 | 16 | 6 |
| Max Cabin Seats | 16 | 19 | 10 |
| Standard Cabin Seats | 16 | 12 | 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 |
| Model | CT7-2F1 | Pearl 700 | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | On Condition | 5000 |
| Horsepower | 1800 | — | — |
| No. of Engines | 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 | 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 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | — |
| Wingspan (ft) | — | 103 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | Flat Floor |
| Baggage Volume Int. (cu. ft) | — | 195 | 90 |
| Cabin Width - Floor (ft) | — | — | 3.8 |
| Cabin Length - Seating (ft) | — | — | 17 |