Airbus Helicopters H225 vs Beechcraft King Air 360 Er vs Gulfstream G700 vs Md Helicopters (mcdonnell Douglas) 902 Explorer
The Airbus H225 is a heavy twin‑engine helicopter optimized for offshore and SAR missions; it typically carries about 19 passengers and has a practical range around 450–600 nautical miles depending on fit and reserves. The MD Helicopters (McDonnell Douglas) 902 Explorer is a light twin helicopter aimed at EMS, law enforcement, and utility work; it generally seats 6–8 and flies roughly 300–400 nautical miles. The Beechcraft King Air 360ER is a twin‑turboprop fixed‑wing aircraft designed for long‑endurance special missions and efficient regional travel; passenger seating varies by interior, but it’s commonly configured for about 6–9, with range on the order of ~1,500–2,000+ nautical miles depending on payload and mission equipment. The Gulfstream G700 is an ultra‑long‑range business jet focused on high‑speed intercontinental travel and cabin comfort; it typically accommodates about 13–19 passengers and offers roughly 7,000–7,500 nautical miles of range. Overall, the helicopters trade speed and range for vertical access and hover capability, while the King Air bridges regional efficiency and versatility, and the G700 dominates on speed, altitude, and global reach.
| Spec | AIRBUS H225 | Gulfstream G700 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 3 |
| DOC / nm | $ 20.87 | — |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 16 |
| Flight Rules | IFR | — |
| Manufacturer | Airbus Helicopters | Gulfstream |
| Aircraft Name | H225 | G700 |
| Certification | FAA / EASA | In Development |
| Max Range (nm) | 454 | 7500 |
| DOC / nm / Seat | $ 0.99 | — |
| Max Cabin Seats | 28 | 19 |
| OEM Verification | Un-Verified | Un-Verified |
| Useful Load (lbs) | 11929 | — |
| Standard Cabin Seats | 19 | 12 |
| Direct Operating Cost | $ 2,963 | — |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck |
| Max Cruise Speed (ktas) | 142 | 516 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 |
| Cabin | ||
| Cockpit | 2 | 2 |
| Min Crew | 2 | 4 |
| Total Seats | 21 | 16 |
| Max Cabin Seats | 28 | 19 |
| Standard Cabin Seats | 19 | 12 |
| Crew Rest | — | Optional |
| Jump Seat | — | Yes |
| Galley Location | — | FWD |
| Lavatory Location | — | FWD / AFT |
| Engine | ||
| FADEC | Yes | — |
| Model | Makila 2A1 | Pearl 700 |
| Fuel Type | JetFuel | — |
| TBO (hrs) | 3500 | On Condition |
| Horsepower | 2100 | — |
| No. of Engines | 2 | 2 |
| Fuel Capacity (gal) | 684 | — |
| Thrust (lbs) | — | 18250 |
| Dimensions | ||
| Length (ft) | 63.4 | 109.9 |
| Overall Height (ft) | 16.3 | 25.4 |
| Rotor Diameter (ft) | 53.2 | — |
| Cabin Volume (cu. ft) | 547 | — |
| Wingspan (ft) | — | 103 |
| Aisle Step (ft) | — | Flat Floor |
| Cabin Width (ft) | — | 8.2 |
| Cabin Height (ft) | — | 6.25 |
| Cabin Length (ft) | — | 56.9 |
| Baggage Volume Int. (cu. ft) | — | 195 |