Airbus Helicopters H225 vs Boeing Bbj Max 9 vs Gulfstream G700 vs Piper M600 Sls
The Airbus H225 is a long‑range, twin‑engine helicopter suited to offshore transport and utility roles rather than point‑to‑point jet travel. Its practical range is roughly in the 500–700 nautical mile class depending on payload and reserves, and it typically carries around 16–19 passengers in transport seating (higher with denser, mission‑specific layouts). The Boeing BBJ MAX 9 is a large‑cabin, airline‑derived VIP airliner. It offers intercontinental range on the order of about 6,000–6,500 nautical miles with auxiliary tanks, and capacity is highly configuration‑dependent: it can be fitted for roughly a few dozen VIP passengers, while the underlying airframe can seat well over 150 in airline layout. The Gulfstream G700 is an ultra‑long‑range business jet optimized for high‑speed, high‑altitude private travel, typically rated around 7,500 nautical miles and commonly configured for about 10–19 passengers. The Piper M600 SLS is a single‑engine turboprop in the personal/light business category, with range around 1,000–1,400 nautical miles and seating typically for 1 pilot plus up to 5 passengers.
| Spec | AIRBUS H225 | Boeing BBJ MAX 9 | Gulfstream G700 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 15.74 | — | $ 2.19 |
| Min Crew | 2 | 4 | 4 | 1 |
| Total Seats | 21 | 12 | 16 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Boeing | Gulfstream | Piper |
| Aircraft Name | H225 | BBJ MAX 9 | G700 | M600 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 6376 | 7500 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 1.97 | — | $ 0.55 |
| Max Cabin Seats | 28 | 35 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 77120 | — | 2200 |
| Standard Cabin Seats | 19 | 8 | 12 | 4 |
| Direct Operating Cost | $ 2,963 | $ 7,396 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Honeywell | Gulfstream Symmetry Flight Deck | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 470 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $107,700,000 | $78,000,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 4 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 5 |
| Max Cabin Seats | 28 | 35 | 19 | — |
| Standard Cabin Seats | 19 | 8 | 12 | 4 |
| Configuration | — | Green Interior | — | — |
| Cabin Pressure (psi) | — | 9 | — | 5.6 |
| SL Cabin Altitude (ft) | — | 24000 | — | 12600 |
| Crew Rest | — | — | Optional | — |
| Jump Seat | — | — | Yes | — |
| Galley Location | — | — | FWD | MID |
| Lavatory Location | — | — | FWD / AFT | — |
| Lavatory | — | — | — | No |
| Galley / Refreshment | — | — | — | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | — | No |
| Model | Makila 2A1 | LEAP-1B | Pearl 700 | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | On-Condition | On Condition | 3600 |
| Horsepower | 2100 | — | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 15 | — | ISA + 55 |
| Thrust (lbs) | — | 28000 | 18250 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 138.4 | 109.9 | 29.7 |
| Overall Height (ft) | 16.3 | 40.3 | 25.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Wingspan (ft) | — | 117.9 | 103 | 43.2 |
| Aisle Step (ft) | — | Flat Floor | Flat Floor | — |
| Cabin Width (ft) | — | 11.6 | 8.2 | 4.1 |
| Cabin Height (ft) | — | 7.1 | 6.25 | 4 |
| Cabin Length (ft) | — | 107.2 | 56.9 | 12.3 |
| Cabin Width - Floor (ft) | — | 10.7 | — | — |
| Cabin Length - Seating (ft) | — | 100.6 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 1485 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | 195 | 20 |