Airbus Helicopters H225 vs Piaggio Avanti Evo vs Piper M600 Sls vs Sikorsky S 92
The Airbus H225 and Sikorsky S‑92 are heavy, twin‑engine helicopters primarily used for offshore transport, SAR, and government missions; both prioritize lifting capability and cabin volume over speed and range. In passenger terms, each typically carries around 16–19 passengers in offshore-style seating (with higher-density layouts possible for other roles). Their practical range is generally in the mid‑hundreds of nautical miles, often roughly 400–600 nm depending on payload, reserves, and mission equipment. The Piaggio Avanti EVO and Piper M600 SLS are pressurized fixed‑wing turboprops aimed at fast business and personal travel. The Avanti EVO is a twin‑turboprop executive aircraft, commonly configured for about 6–9 passengers, with a range typically around 1,500–1,800 nm. The Piper M600 SLS is a single‑engine turboprop optimized for owner‑pilots, usually seating 5–6 passengers, with a range commonly around 1,200–1,500 nm. Overall, the fixed‑wing turboprops offer substantially longer range and higher cruise speed, while the helicopters offer vertical access and better short‑area utility.
| Spec | AIRBUS H225 | Piaggio Avanti EVO | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 20.87 | — | $ 2.19 | $ 19.79 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 8 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR | IFR |
| Manufacturer | Airbus Helicopters | Piaggio | Piper | Sikorsky |
| Aircraft Name | H225 | Avanti EVO | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 454 | 1530 | 1406 | 439 |
| DOC / nm / Seat | $ 0.99 | — | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 28 | 7 | — | 19 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | Un-Verified |
| Useful Load (lbs) | 11929 | 3775 | 2200 | 7417 |
| Standard Cabin Seats | 19 | 6 | 4 | 19 |
| Direct Operating Cost | $ 2,963 | — | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Rockwell Collins Pro Line 21 | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 142 | 400 | 274 | 155 |
| Base Aircraft Price (USD) | $ 29,500,000 | $ 7,695,000 | $3,081,400 | $30,650,000 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Min Crew | 2 | 1 | 1 | 2 |
| Total Seats | 21 | 8 | 5 | 21 |
| Max Cabin Seats | 28 | 7 | — | 19 |
| Standard Cabin Seats | 19 | 6 | 4 | 19 |
| Lavatory | — | No | No | — |
| Cabin Pressure (psi) | — | 9 | 5.6 | — |
| Galley / Refreshment | — | No | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | 24000 | 12600 | — |
| Max Cabin Altitude (ft) | — | 6600 | 8644 | — |
| Galley Location | — | — | MID | — |
| Engine | ||||
| FADEC | Yes | Yes | No | Yes |
| Model | Makila 2A1 | PT6A–66B | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | — | JetFuel |
| TBO (hrs) | 3500 | 3600 | 3600 | 4000 |
| Horsepower | 2100 | 850 | 600 | 2520 |
| No. of Engines | 2 | 2 | 1 | 1 |
| Fuel Capacity (gal) | 684 | — | 260 | 760 |
| Flat Rating | — | ISA + 28 | ISA + 55 | — |
| Fuel Burn (gph) | — | 100 | — | — |
| Dimensions | ||||
| Length (ft) | 63.4 | 47.3 | 29.7 | — |
| Overall Height (ft) | 16.3 | 13.1 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 53.2 | — | — | — |
| Cabin Volume (cu. ft) | 547 | — | 165 | 775 |
| Wingspan (ft) | — | 47.1 | 43.2 | — |
| Cabin Width (ft) | — | 6.1 | 4.1 | — |
| Cabin Height (ft) | — | 5.8 | 4 | — |
| Cabin Length (ft) | — | 14.9 | 12.3 | — |
| Cabin Width - Floor (ft) | — | 3.5 | — | — |
| Baggage Volume Int. (cu. ft) | — | 35.2 | 20 | — |
| Baggage Volume Ext. (cu. ft) | — | — | — | 140 |