Bell 525 Relentless vs Boeing Bbj Max 9 vs Gulfstream G700 vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are helicopters, best suited to point-to-point access into tight or unimproved landing areas, while the Boeing BBJ MAX 9 and Gulfstream G700 are long-range business jets optimized for fast intercity and intercontinental travel between airports. In typical configurations, the Bell 525 carries roughly up to the mid-teens of passengers and offers a practical range on the order of about 500–600 nautical miles, making it strong for regional corporate or offshore-style missions. The Sikorsky S-92 is a larger, heavy helicopter, commonly configured for about 19 passengers, with a broadly similar regional range around 500+ nautical miles depending on payload. The Gulfstream G700 is an ultra-long-range business jet, typically carrying around 13–19 passengers in executive layouts, with intercontinental range around 7,500+ nautical miles. The Boeing BBJ MAX 9 is a VIP airliner based on the 737 MAX 9; it can be configured for a few dozen passengers in luxury layouts and has long range roughly around 6,000+ nautical miles, trading some range and airport flexibility versus the G700 for a much larger cabin.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Gulfstream G700 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 4 | 2 |
| Total Seats | 18 | 12 | 16 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Bell | Boeing | Gulfstream | Sikorsky |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | G700 | S-92 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 580 | 6376 | 7500 | 439 |
| Max Cabin Seats | 16 | 35 | 19 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | 77120 | — | 7417 |
| Standard Cabin Seats | 16 | 8 | 12 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 160 | 470 | 516 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $78,000,000 | $30,650,000 |
| DOC / nm | — | $ 15.74 | — | $ 19.79 |
| DOC / nm / Seat | — | $ 1.97 | — | $ 0.94 |
| Direct Operating Cost | — | $ 7,396 | — | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 4 | 2 |
| Total Seats | 18 | 10 | 16 | 21 |
| Max Cabin Seats | 16 | 35 | 19 | 19 |
| Standard Cabin Seats | 16 | 8 | 12 | 19 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | — | — |
| SL Cabin Altitude (ft) | — | 24000 | — | — |
| Crew Rest | — | — | Optional | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | — | Yes |
| Model | CT7-2F1 | LEAP-1B | Pearl 700 | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 4000 | On-Condition | On Condition | 4000 |
| Horsepower | 1800 | — | — | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | — | 760 |
| Flat Rating | — | ISA + 15 | — | — |
| Thrust (lbs) | — | 28000 | 18250 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 109.9 | — |
| Cabin Width (ft) | 7.58 | 11.6 | 8.2 | — |
| Cabin Height (ft) | 4.5 | 7.1 | 6.25 | — |
| Cabin Length (ft) | 15.5 | 107.2 | 56.9 | — |
| Overall Height (ft) | 18.18 | 40.3 | 25.4 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | — | 140 |
| Wingspan (ft) | — | 117.9 | 103 | — |
| Aisle Step (ft) | — | Flat Floor | Flat Floor | — |
| Cabin Width - Floor (ft) | — | 10.7 | — | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | 195 | — |
| Cabin Volume (cu. ft) | — | — | — | 775 |