Bell 525 Relentless vs Boeing Bbj Max 9 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Pilatus Pc 24
The Bell 525 Relentless is a long-range, fly-by-wire commercial helicopter aimed at executive and offshore missions, typically carrying about 16–19 passengers in standard seating. Its practical range is roughly in the 500–600 nautical mile class, trading speed and cabin volume for vertical-lift flexibility and point-to-point access. The Boeing BBJ MAX 9 is a large VIP airliner derived from the 737 MAX 9, positioned for head-of-state or corporate transport. It offers by far the greatest range—about 3,300–3,500 nautical miles depending on configuration—and the largest capacity, commonly outfitted for roughly 25–50 passengers in VIP layouts (though airline-style seating can be much higher). The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin-engine helicopter for utility, EMS, law enforcement, and corporate shuttle roles. It generally seats around 8–10 passengers including crew, with range typically around 300–350 nautical miles. The Pilatus PC-24 is a light business jet optimized for short and unimproved runways, bridging turboprop-like access with jet speed. It usually carries about 6–10 passengers, with range around 1,800–2,000 nautical miles.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Pilatus PC-24 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 18 | 12 | 6 |
| Flight Rules | IFR | — | — |
| Manufacturer | Bell | Boeing | Pilatus |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | PC-24 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6376 | 2076 |
| Max Cabin Seats | 16 | 35 | 10 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED |
| Useful Load (lbs) | 6675 | 77120 | 6680 |
| Standard Cabin Seats | 16 | 8 | 6 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 160 | 470 | 440 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $11,800,000 |
| DOC / nm | — | $ 15.74 | $ 3.71 |
| DOC / nm / Seat | — | $ 1.97 | $ 0.62 |
| Direct Operating Cost | — | $ 7,396 | $ 1,619 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 18 | 10 | 6 |
| Max Cabin Seats | 16 | 35 | 10 |
| Standard Cabin Seats | 16 | 8 | 6 |
| Configuration | — | Green Interior | — |
| Cabin Pressure (psi) | — | 9 | 9.3 |
| SL Cabin Altitude (ft) | — | 24000 | 23500 |
| Lavatory | — | — | 1 Enclosed Flushing |
| Crew Rest | — | — | No |
| Jump Seat | — | — | No |
| Cargo Door | — | — | Yes |
| Galley Location | — | — | FWD |
| Lavatory Location | — | — | FWD |
| Galley / Refreshment | — | — | Optional Refreshment Center |
| Engine | |||
| FADEC | Dual-Channel | Yes | Yes |
| Model | CT7-2F1 | LEAP-1B | FJ44-4A-QPM |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 4000 | On-Condition | 5000 |
| Horsepower | 1800 | — | — |
| No. of Engines | 2 | 2 | 2 |
| Fuel Capacity (gal) | 641 | — | — |
| Flat Rating | — | ISA + 15 | ISA + 23 |
| Thrust (lbs) | — | 28000 | 3435 |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 138.4 | 52.2 |
| Cabin Width (ft) | 7.58 | 11.6 | 5.6 |
| Cabin Height (ft) | 4.5 | 7.1 | 5.1 |
| Cabin Length (ft) | 15.5 | 107.2 | 23 |
| Overall Height (ft) | 18.18 | 40.3 | 17.4 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | — |
| Wingspan (ft) | — | 117.9 | 55.8 |
| Aisle Step (ft) | — | Flat Floor | Flat Floor |
| Cabin Width - Floor (ft) | — | 10.7 | 3.8 |
| Cabin Length - Seating (ft) | — | 100.6 | 17 |
| Baggage Volume Int. (cu. ft) | — | — | 90 |