Bell 525 Relentless vs Gulfstream G700 vs Leonardo Aw189 vs Sikorsky S 92
The Gulfstream G700 is a long‑range business jet, designed for intercontinental travel. It offers by far the greatest range (roughly 7,000+ nautical miles, depending on configuration) and typically carries around 10–19 passengers in high‑end executive layouts, trading vertical-lift capability for speed, altitude, and nonstop global reach. The Bell 525 Relentless is a super‑medium helicopter aimed at offshore, corporate, and mission roles. Its range is on the order of the high hundreds of nautical miles (commonly cited around ~500 nm class), with passenger capacity typically up to about 16–20 depending on interior. The Leonardo (Agusta) AW189 is a larger super‑medium helicopter optimized for offshore and SAR. Its range is broadly similar (high hundreds of nautical miles, mission‑dependent), and it commonly seats around 16–19 passengers in transport layouts. The Sikorsky S‑92 is a heavy helicopter used extensively offshore and for head‑of‑state/VIP missions. It generally offers comparable or slightly greater mission radius than super‑mediums depending on tanks, and typically carries about 19 passengers in offshore configurations, emphasizing payload, robustness, and cabin volume over jet-like range.
| Spec | Bell 525 Relentless | Gulfstream G700 | AGUSTA / LEONARDO AW189 | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 3 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 18 | 16 | 21 | 21 |
| Flight Rules | IFR | — | IFR | IFR |
| Manufacturer | Bell | Gulfstream | Leonardo | Sikorsky |
| Aircraft Name | 525 Relentless | G700 | AW189 | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA | FAA / EASA |
| Max Range (nm) | 580 | 7500 | 651 | 439 |
| Max Cabin Seats | 16 | 19 | 19 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | — | — | 7417 |
| Standard Cabin Seats | 16 | 12 | 19 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Gulfstream Symmetry Flight Deck | EFIS | EFIS |
| Max Cruise Speed (ktas) | 160 | 516 | 155 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $78,000,000 | $2,413,000 | $30,650,000 |
| DOC / nm | — | — | $ 15.57 | $ 19.79 |
| DOC / nm / Seat | — | — | $ 0.74 | $ 0.94 |
| Direct Operating Cost | — | — | $ 2,413 | $ 3,068 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 | 2 |
| Total Seats | 18 | 16 | 21 | 21 |
| Max Cabin Seats | 16 | 19 | 19 | 19 |
| Standard Cabin Seats | 16 | 12 | 19 | 19 |
| Crew Rest | — | Optional | — | — |
| Jump Seat | — | Yes | — | — |
| Galley Location | — | FWD | — | — |
| Lavatory Location | — | FWD / AFT | — | — |
| Engine | ||||
| FADEC | Dual-Channel | — | Yes | Yes |
| Model | CT7-2F1 | Pearl 700 | CT7-2E1 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel | JetFuel |
| TBO (hrs) | 4000 | On Condition | 4000 | 4000 |
| Horsepower | 1800 | — | 1983 | 2520 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | — | 760 |
| Thrust (lbs) | — | 18250 | — | — |
| Dimensions | ||||
| Width (ft) | 25.77 | — | — | — |
| Length (ft) | 61.58 | 109.9 | 57.8 | — |
| Cabin Width (ft) | 7.58 | 8.2 | — | — |
| Cabin Height (ft) | 4.5 | 6.25 | — | — |
| Cabin Length (ft) | 15.5 | 56.9 | — | — |
| Overall Height (ft) | 18.18 | 25.4 | 16.6 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | 48 | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 85 | 140 |
| Wingspan (ft) | — | 103 | — | — |
| Aisle Step (ft) | — | Flat Floor | — | — |
| Baggage Volume Int. (cu. ft) | — | 195 | — | — |
| Cabin Volume (cu. ft) | — | — | 395 | 775 |