Airbus Helicopters H225 vs Enstrom 480b vs Gulfstream G700 vs Piper M600 Sls
The Airbus H225 and Enstrom 480B are helicopters, while the Gulfstream G700 and Piper M600 SLS are fixed‑wing business aircraft. The H225 is a large, long‑range twin‑engine helicopter typically used for offshore, search and rescue, and utility transport; it can carry a relatively high number of passengers for a helicopter (often around the high‑teens to low‑20s depending on configuration) and offers a several‑hundred‑nautical‑mile range. The Enstrom 480B is a much smaller piston helicopter aimed at training and personal/utility flying, usually seating five with a comparatively short range of only a few hundred nautical miles. The Gulfstream G700 is an ultra‑long‑range business jet built for intercontinental missions, generally accommodating about a dozen to nearly twenty passengers depending on cabin layout, with a range on the order of 7,000+ nautical miles. The Piper M600 SLS is a single‑engine turboprop positioned below large jets, typically seating up to six, with a range around 1,500 nautical miles, making it suited to regional and some transcontinental trips with fewer 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 |