Airbus Helicopters H225 vs Embraer Legacy 650 E vs Gulfstream G700 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter (rotary‑wing) optimized for offshore, SAR, and utility missions rather than fast point‑to‑point travel. Typical range is on the order of a few hundred nautical miles depending on payload and reserves, and it generally carries roughly 16–19 passengers in high‑density configurations (often fewer in VIP or missionized layouts). The Embraer Legacy 650E is a large‑cabin business jet designed for long‑range regional/international trips, offering roughly 3,900 nautical miles of range and typically seating about 13 passengers in a standard executive cabin. The Gulfstream G700 is an ultra‑long‑range, large‑cabin flagship business jet focused on nonstop intercontinental missions, with about 7,500 nautical miles of range and typically configured for around 13–19 passengers depending on layout. The Piper M600 SLS is a single‑engine turboprop (fixed‑wing) aimed at owner‑operators, with roughly 1,500 nautical miles of range and seating for up to 6 occupants including the pilot (typically 5 passengers).
| 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 |