Airbus Helicopters H225 vs Bombardier Global 7500 vs Enstrom 480b vs Sikorsky S 92
The Airbus H225 and Sikorsky S-92 are heavy, twin‑engine helicopters optimized for offshore transport and utility missions. Both typically carry around 16–19 passengers in common transport layouts, with ranges roughly in the 450–550 nautical mile class depending on fuel, payload, and reserves; the H225 is often cited around 500–600 nm, while the S‑92 is commonly around 500 nm. The Enstrom 480B is a light, single‑engine piston helicopter aimed at training, patrol, and personal/utility flying. It carries up to 5 people (including the pilot) and has a much shorter range, generally around 200–300 nautical miles. The Bombardier Global 7500 is a long‑range business jet in an entirely different category: intercontinental point‑to‑point travel at high speed and altitude. It typically seats 8–19 passengers depending on configuration and offers approximately 7,700 nautical miles of range, far exceeding the helicopters and the Enstrom.
| Spec | AIRBUS H225 | Bombardier Global 7500 | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | $ 9.50 | $ 19.79 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 21 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Bombardier | Sikorsky |
| Aircraft Name | H225 | Global 7500 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 7700 | 439 |
| DOC / nm / Seat | $ 0.99 | $ 0.79 | $ 0.94 |
| Max Cabin Seats | 28 | 19 | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | — | 7417 |
| Standard Cabin Seats | 19 | 12 | 19 |
| Direct Operating Cost | $ 2,963 | $ 4,900 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Bombardier Vision (Pro Line Fusion) | EFIS |
| Max Cruise Speed (ktas) | 142 | 516 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $75,000,000 | $30,650,000 |
| Aircraft Type | — | Business Jet | — |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 2 |
| Total Seats | 21 | 14 | 21 |
| Max Cabin Seats | 28 | 19 | 19 |
| Standard Cabin Seats | 19 | 12 | 19 |
| 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 | Yes | Yes | Yes |
| Model | Makila 2A1 | Passport | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 3500 | On-Condition | 4000 |
| Horsepower | 2100 | — | 2520 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 760 |
| Flat Rating | — | ISA + 15 | — |
| Thrust (lbs) | — | 18920 | — |
| Dimensions | |||
| Length (ft) | 63.4 | 111 | — |
| Overall Height (ft) | 16.3 | 27 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 775 |
| Wingspan (ft) | — | 104 | — |
| Cabin Width (ft) | — | 8 | — |
| Cabin Height (ft) | — | 6.2 | — |
| Cabin Length (ft) | — | 54.5 | — |
| Baggage Volume Ext. (cu. ft) | — | — | 140 |