Bell 525 Relentless vs Gulfstream G700 vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Sikorsky S 92
The Gulfstream G700 is a long‑range business jet, optimized for intercontinental travel. It offers roughly 7,500 nautical miles of range and typically carries about 10–19 passengers in a luxury cabin, making it the clear choice when speed and nonstop distance are priorities. The Bell 525 Relentless is a super‑medium helicopter aimed at corporate and offshore missions; it has a range on the order of about 550–600 nautical miles and commonly seats around 16 passengers (with layouts varying by mission). The Sikorsky S‑92 is a larger, heavy helicopter widely used for offshore transport and SAR; it generally provides about 540–600 nautical miles of range and is often configured for roughly 19 passengers. The MD Helicopters (McDonnell Douglas) MD 902 Explorer is a light twin helicopter suited to law enforcement, EMS, and utility roles; its range is typically around 300–350 nautical miles and it usually carries about 6–8 passengers. Overall, the G700 dominates on range and cruise efficiency, while the S‑92 and 525 carry more people than the 902 and excel at vertical-lift missions.
| Spec | Bell 525 Relentless | Gulfstream G700 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| Min Crew | 2 | 4 | 2 |
| Total Seats | 18 | 16 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Bell | Gulfstream | Sikorsky |
| Aircraft Name | 525 Relentless | G700 | S-92 |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 580 | 7500 | 439 |
| Max Cabin Seats | 16 | 19 | 19 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified |
| Useful Load (lbs) | 6675 | — | 7417 |
| Standard Cabin Seats | 16 | 12 | 19 |
| Flight Deck (Base Spec) | Garmin G5000H | Gulfstream Symmetry Flight Deck | EFIS |
| Max Cruise Speed (ktas) | 160 | 516 | 155 |
| Base Aircraft Price (USD) | $15,000,000 | $78,000,000 | $30,650,000 |
| DOC / nm | — | — | $ 19.79 |
| DOC / nm / Seat | — | — | $ 0.94 |
| Direct Operating Cost | — | — | $ 3,068 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 2 |
| Total Seats | 18 | 16 | 21 |
| Max Cabin Seats | 16 | 19 | 19 |
| Standard Cabin Seats | 16 | 12 | 19 |
| Crew Rest | — | Optional | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | — |
| Lavatory Location | — | FWD / AFT | — |
| Engine | |||
| FADEC | Dual-Channel | — | Yes |
| Model | CT7-2F1 | Pearl 700 | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | On Condition | 4000 |
| Horsepower | 1800 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 641 | — | 760 |
| Thrust (lbs) | — | 18250 | — |
| Dimensions | |||
| Width (ft) | 25.77 | — | — |
| Length (ft) | 61.58 | 109.9 | — |
| 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 | 17.8 |
| Rotor Diameter (ft) | 54.5 | — | — |
| Baggage Volume Ext. (cu. ft) | 128 | — | 140 |
| Wingspan (ft) | — | 103 | — |
| Aisle Step (ft) | — | Flat Floor | — |
| Baggage Volume Int. (cu. ft) | — | 195 | — |
| Cabin Volume (cu. ft) | — | — | 775 |