Airbus Helicopters H225 vs Gulfstream G700 vs Piper M600 Sls vs Robinson R66
The Airbus H225 and Robinson R66 are helicopters, while the Gulfstream G700 and Piper M600 SLS are fixed‑wing business aircraft, so their range and capacity reflect very different missions. The Airbus H225 is a heavy, long‑range twin‑engine helicopter used for offshore transport, search and rescue, and utility roles, typically carrying around 16–19 passengers in high‑density seating (or fewer in VIP/SAR layouts) with roughly 450–650 nautical miles of range depending on configuration and reserves. The Robinson R66 is a light single‑engine helicopter aimed at private and training use, usually carrying 4 passengers plus a pilot (5 total) with about 300–350 nautical miles of range. Among the jets and turboprops, the Gulfstream G700 is an ultra‑long‑range business jet designed for intercontinental travel, typically seating 10–19 passengers (up to the low‑20s in some layouts) with about 7,500 nautical miles of range. The Piper M600 SLS is a single‑engine turboprop for owner‑pilots, seating up to 5–6 with roughly 1,000–1,400 nautical miles of range depending on cruise and reserves.
| 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 |