Bombardier Global 7500 vs Dassault Falcon 8x vs Md Helicopters (mcdonnell Douglas) 902 Explorer vs Sikorsky S 92
The Bombardier Global 7500 and Dassault Falcon 8X are long‑range business jets, while the MD Helicopters 902 Explorer and Sikorsky S‑92 are twin‑engine helicopters, with the S‑92 aimed more at offshore/VIP and transport missions than the lighter 902. In range, the Global 7500 leads the group with roughly 7,700 nautical miles, enabling ultra‑long intercontinental trips. The Falcon 8X is also ultra‑long‑range at about 6,450 nautical miles, slightly shorter but still capable of major nonstop city pairs. Helicopter range is far lower: the MD 902 Explorer is typically in the few‑hundred‑nautical‑mile class (often around 300–400 nm depending on configuration), and the larger S‑92 generally offers a similar or somewhat higher practical range (commonly around 500 nm, mission‑dependent). Passenger capacity also separates them. The Global 7500 typically carries about 14–19 passengers in executive layouts, while the Falcon 8X commonly seats about 12–16. The MD 902 Explorer usually carries the pilot plus roughly 7–8 passengers. The Sikorsky S‑92 is the capacity leader among the helicopters, frequently configured for about 12–19 passengers depending on mission and interior.
| Spec | Bombardier Global 7500 | Dassault Falcon 8X | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 9.50 | $ 7.66 | $ 19.79 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 14 | 17 | 21 |
| Manufacturer | Bombardier | Dassault Falcon | Sikorsky |
| Aircraft Name | Global 7500 | 8X | S-92 |
| Aircraft Type | Business Jet | — | — |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 7700 | 6450 | 439 |
| DOC / nm / Seat | $ 0.79 | $ 0.64 | $ 0.94 |
| Max Cabin Seats | 19 | 16 | 19 |
| OEM Verification | VERIFIED | VERIFIED | Un-Verified |
| Standard Cabin Seats | 12 | 14 | 19 |
| Direct Operating Cost | $ 4,900 | $ 3,805 | $ 3,068 |
| Flight Deck (Base Spec) | Bombardier Vision (Pro Line Fusion) | Honeywell Primus EASy II | EFIS |
| Max Cruise Speed (ktas) | 516 | 516 | 155 |
| Base Aircraft Price (USD) | $75,000,000 | $ 62,500,000 | $30,650,000 |
| Useful Load (lbs) | — | 36900 | 7417 |
| Flight Rules | — | — | IFR |
| Cabin | |||
| Cockpit | 2 | 3 | 2 |
| Lavatory | 2 Enclosed Flushing | 2 Enclosed Flushing | — |
| Min Crew | 2 | 2 | 2 |
| Crew Rest | Yes | No | — |
| Jump Seat | Yes | Yes | — |
| Total Seats | 14 | 17 | 21 |
| Galley Location | FWD | FWD | — |
| Max Cabin Seats | 19 | 16 | 19 |
| Lavatory Location | FWD / AFT | FWD / AFT | — |
| Galley / Refreshment | Galley | Galley | — |
| Standard Cabin Seats | 12 | 14 | 19 |
| Max Cabin Altitude (ft) | 4500 | 3900 | — |
| Cabin Pressure (psi) | — | 10.2 | — |
| SL Cabin Altitude (ft) | — | 29200 | — |
| Engine | |||
| FADEC | Yes | Yes | Yes |
| Model | Passport | PW307D | CT7-8A |
| TBO (hrs) | On-Condition | On-Condition | 4000 |
| Flat Rating | ISA + 15 | ISA + 17 | — |
| Thrust (lbs) | 18920 | 6722 | — |
| No. of Engines | 2 | 3 | 1 |
| Fuel Type | — | — | JetFuel |
| Horsepower | — | — | 2520 |
| Fuel Capacity (gal) | — | — | 760 |
| Dimensions | |||
| Length (ft) | 111 | 80.2 | — |
| Wingspan (ft) | 104 | 86.3 | — |
| Cabin Width (ft) | 8 | 7.7 | — |
| Cabin Height (ft) | 6.2 | 6.2 | — |
| Cabin Length (ft) | 54.5 | 42.7 | — |
| Overall Height (ft) | 27 | 26.1 | 17.8 |
| Cabin Volume (cu. ft) | — | 1695 | 775 |
| Cabin Width - Floor (ft) | — | 6.3 | — |
| Cabin Length - Seating (ft) | — | 29.2 | — |
| Baggage Volume Int. (cu. ft) | — | 140 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |