Airbus Helicopters H225 vs Cessna Citation Xls vs Gulfstream G700 vs Piper M600 Sls
The Airbus H225 is a heavy twin‑engine helicopter optimized for offshore, SAR, and utility missions; it trades speed and altitude for vertical lift and typically carries around 19 passengers in high‑density seating, with practical range on the order of a few hundred nautical miles (often roughly 400–500 nm depending on fit and reserves). The Cessna Citation XLS+ is a super‑light/midsize business jet designed for short‑to‑medium trips, usually seating 7–9 passengers, and offers about 2,000 nm of range. The Gulfstream G700 is an ultra‑long‑range large‑cabin jet aimed at intercontinental travel, commonly configured for roughly 10–19 passengers, with range around 7,500 nm. The Piper M600 SLS is a single‑engine turboprop in the personal/business category, typically seating 5–6 passengers, with range around 1,500 nm. In short, H225 emphasizes access and lift, M600 SLS emphasizes efficient regional flexibility, XLS+ targets practical point‑to‑point business travel, and G700 dominates for long‑haul, high‑comfort missions.
| Spec | AIRBUS H225 | Cessna Citation XLS+ | Gulfstream G700 | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 3 | 2 |
| DOC / nm | $ 20.87 | $ 5.34 | — | $ 2.19 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 6 |
| Flight Rules | IFR | — | — | IFR |
| Manufacturer | Airbus Helicopters | Cessna Citation | Gulfstream | Piper |
| Aircraft Name | H225 | XLS+ | G700 | M600 |
| Certification | FAA / EASA | FAA / EASA | In Development | FAA / EASA |
| Max Range (nm) | 454 | 1906 | 7500 | 1406 |
| DOC / nm / Seat | $ 0.99 | $ 0.67 | — | $ 0.55 |
| Max Cabin Seats | 28 | 9 | 19 | — |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 11929 | 7540 | — | 2200 |
| Standard Cabin Seats | 19 | 8 | 12 | 4 |
| Direct Operating Cost | $ 2,963 | $ 2,303 | — | $ 603 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Gulfstream Symmetry Flight Deck | Garmin G3000 |
| Max Cruise Speed (ktas) | 142 | 430 | 516 | 274 |
| Base Aircraft Price (USD) | $ 29,500,000 | $15,500,000 | $78,000,000 | $3,081,400 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 2 | 4 | 1 |
| Total Seats | 21 | 10 | 16 | 5 |
| Max Cabin Seats | 28 | 9 | 19 | — |
| Standard Cabin Seats | 19 | 8 | 12 | 4 |
| Lavatory | — | 1 Enclosed Belted Flushing | — | No |
| Crew Rest | — | No | Optional | — |
| Jump Seat | — | No | Yes | — |
| Galley Location | — | FWD | FWD | MID |
| Lavatory Location | — | AFT | FWD / AFT | — |
| Cabin Pressure (psi) | — | 9.3 | — | 5.6 |
| Galley / Refreshment | — | Galley | — | Refreshment Centre |
| SL Cabin Altitude (ft) | — | 25230 | — | 12600 |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | Yes | Yes | — | No |
| Model | Makila 2A1 | PW545C | Pearl 700 | PT6A-42A |
| Fuel Type | JetFuel | — | — | — |
| TBO (hrs) | 3500 | 5000 | On Condition | 3600 |
| Horsepower | 2100 | — | — | 600 |
| No. of Engines | 2 | 2 | 2 | 1 |
| Fuel Capacity (gal) | 684 | — | — | 260 |
| Flat Rating | — | ISA + 10 | — | ISA + 55 |
| Thrust (lbs) | — | 4119 | 18250 | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 52.5 | 109.9 | 29.7 |
| Overall Height (ft) | 16.3 | 17.2 | 25.4 | 11.3 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | — | 165 |
| Wingspan (ft) | — | 56.3 | 103 | 43.2 |
| Aisle Step (ft) | — | 0.7 | Flat Floor | — |
| Cabin Width (ft) | — | 5.5 | 8.2 | 4.1 |
| Cabin Height (ft) | — | 5.7 | 6.25 | 4 |
| Cabin Length (ft) | — | 18.5 | 56.9 | 12.3 |
| Cabin Width - Floor (ft) | — | 3.9 | — | — |
| Cabin Length - Seating (ft) | — | 14.3 | — | — |
| Baggage Volume Ext. (cu. ft) | — | 80 | — | — |
| Baggage Volume Int. (cu. ft) | — | 10 | 195 | 20 |