Bell 525 Relentless vs Boeing Bbj Max 9 vs Bombardier Global 7500 vs Sikorsky S 92
The Bell 525 Relentless and Sikorsky S-92 are civil helicopters suited to point-to-point missions where vertical lift matters more than cruise efficiency. The Bell 525 is a super‑medium helicopter with roughly 500–600 nautical miles of range and typically carries about 12–16 passengers depending on layout. The Sikorsky S‑92 is a larger medium helicopter, commonly configured for about 16–19 passengers, with a similar order of range (around 500 nautical miles) but optimized for offshore and utility reliability. The Bombardier Global 7500 is an ultra‑long‑range business jet designed for fast intercontinental travel. It offers about 7,700 nautical miles of range and generally carries 8–19 passengers in executive layouts. The Boeing BBJ MAX 9 is a VIP airliner based on a narrow‑body transport, prioritizing space and endurance for government or head‑of‑state missions. It has intercontinental range on the order of roughly 6,000–6,600 nautical miles (configuration dependent) and, while the airframe can seat far more, VIP interiors typically accommodate around 25–50 passengers (sometimes more) with lounges, offices, and bedrooms.
| Spec | Bell 525 Relentless | Boeing BBJ MAX 9 | Bombardier Global 7500 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 18 | 12 | 14 | 21 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Bell | Boeing | Bombardier | Sikorsky |
| Aircraft Name | 525 Relentless | BBJ MAX 9 | Global 7500 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 6376 | 7700 | 439 |
| Max Cabin Seats | 16 | 35 | 19 | 19 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | Un-Verified |
| Useful Load (lbs) | 6675 | 77120 | — | 7417 |
| Standard Cabin Seats | 16 | 8 | 12 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Honeywell | Bombardier Vision (Pro Line Fusion) | EFIS |
| Max Cruise Speed (ktas) | 160 | 470 | 516 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $107,700,000 | $75,000,000 | $30,650,000 |
| DOC / nm | — | $ 15.74 | $ 9.50 | $ 19.79 |
| DOC / nm / Seat | — | $ 1.97 | $ 0.79 | $ 0.94 |
| Direct Operating Cost | — | $ 7,396 | $ 4,900 | $ 3,068 |
| Aircraft Type | — | — | Business Jet | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 | 2 |
| Total Seats | 18 | 10 | 14 | 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 | — | — |
| Lavatory | — | — | 2 Enclosed Flushing | — |
| Crew Rest | — | — | Yes | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | — |
| Lavatory Location | — | — | FWD / AFT | — |
| Galley / Refreshment | — | — | Galley | — |
| Max Cabin Altitude (ft) | — | — | 4500 | — |
| Engine | ||||
| FADEC | Dual-Channel | Yes | Yes | Yes |
| Model | CT7-2F1 | LEAP-1B | Passport | 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 | ISA + 15 | — |
| Thrust (lbs) | — | 28000 | 18920 | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 138.4 | 111 | — |
| Cabin Width (ft) | 7.58 | 11.6 | 8 | — |
| Cabin Height (ft) | 4.5 | 7.1 | 6.2 | — |
| Cabin Length (ft) | 15.5 | 107.2 | 54.5 | — |
| Overall Height (ft) | 18.18 | 40.3 | 27 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | 1485 | — | 140 |
| Wingspan (ft) | — | 117.9 | 104 | — |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Cabin Width - Floor (ft) | — | 10.7 | — | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Cabin Volume (cu. ft) | — | — | — | 775 |