Airbus Helicopters H225 vs Cessna 208b Grand Caravan Ex vs Gulfstream G700 vs Piper M600 Sls
The Airbus H225 is a large twin‑engine helicopter optimized for vertical lift missions rather than point‑to‑point cruise; it typically carries around 19 passengers, but its practical range is generally a few hundred nautical miles depending heavily on payload, reserves, and mission profile. The Cessna 208B Grand Caravan EX is a rugged single‑engine turboprop utility aircraft, commonly configured for about 9–14 passengers, with a typical range in the roughly 900–1,200 nautical mile class. The Gulfstream G700 is an ultra‑long‑range business jet designed for high‑speed intercontinental travel; it usually seats about 10–19 passengers in luxury (with higher maximums possible by configuration) and offers a range around 7,500 nautical miles. The Piper M600 SLS is a single‑engine turboprop personal/business aircraft, typically seating 5–6 passengers, with range on the order of about 1,400 nautical miles. In short, the H225 prioritizes access and lift, the Caravan emphasizes utility and short‑field flexibility, the G700 dominates long‑range speed and comfort, and the M600 SLS targets efficient owner‑flown travel.
| Spec | AIRBUS H225 | Gulfstream G700 | Piper M600 SLS |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | — | $ 2.19 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 6 |
| Flight Rules | IFR | — | IFR |
| Manufacturer | Airbus Helicopters | Gulfstream | Piper |
| Aircraft Name | H225 | G700 | M600 |
| Certification | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 7500 | 1406 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.55 |
| Max Cabin Seats | 28 | 19 | — |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | — | 2200 |
| Standard Cabin Seats | 19 | 12 | 4 |
| Direct Operating Cost | $ 2,963 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Gulfstream Symmetry Flight Deck | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $78,000,000 | $3,081,400 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 1 |
| Total Seats | 21 | 16 | 5 |
| Max Cabin Seats | 28 | 19 | — |
| Standard Cabin Seats | 19 | 12 | 4 |
| Crew Rest | — | Optional | — |
| Jump Seat | — | Yes | — |
| Galley Location | — | FWD | MID |
| Lavatory Location | — | FWD / AFT | — |
| Lavatory | — | — | No |
| Cabin Pressure (psi) | — | — | 5.6 |
| Galley / Refreshment | — | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | — | 12600 |
| Max Cabin Altitude (ft) | — | — | 8644 |
| Engine | |||
| FADEC | Yes | — | No |
| Model | Makila 2A1 | Pearl 700 | PT6A-42A |
| Fuel Type | JetFuel | — | — |
| TBO (hrs) | 3500 | On Condition | 3600 |
| Horsepower | 2100 | — | 600 |
| No. of Engines | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 |
| Thrust (lbs) | — | 18250 | — |
| Flat Rating | — | — | ISA + 55 |
| Dimensions | |||
| Length (ft) | 63.4 | 109.9 | 29.7 |
| Overall Height (ft) | 16.3 | 25.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 |
| Wingspan (ft) | — | 103 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | — |
| Cabin Width (ft) | — | 8.2 | 4.1 |
| Cabin Height (ft) | — | 6.25 | 4 |
| Cabin Length (ft) | — | 56.9 | 12.3 |
| Baggage Volume Int. (cu. ft) | — | 195 | 20 |