Cessna 208b Grand Caravan Ex vs Leonardo Aw189 vs Piper M600 Sls vs Sikorsky S 92
The Cessna 208B Grand Caravan EX is a single‑engine turboprop fixed‑wing utility aircraft, typically used for short‑to‑medium regional missions. It generally carries about 9 passengers (often up to 14–15 seats in high‑density layouts) and offers roughly 900–1,200 nm of range depending on payload and reserves. The Piper M600 SLS is also a single‑engine turboprop but positioned as a pressurized personal/business aircraft; it usually seats 5–6 passengers and has a longer typical range around 1,400–1,600 nm. The Leonardo AW189 is a medium twin‑engine helicopter designed for offshore, SAR, and utility transport. It commonly seats around 16 passengers in standard offshore configurations (higher in dense seating) and has an approximate range in the 400–500 nm class, varying with fuel tanks and mission equipment. The Sikorsky S‑92 is a larger heavy twin‑engine helicopter, also widely used offshore and for government/VIP roles; it typically carries about 19 passengers in offshore seating and has a similar medium‑range helicopter profile, often around 500–600 nm depending on configuration.
| Spec | AGUSTA / LEONARDO AW189 | Piper M600 SLS | Sikorsky S-92 |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 15.57 | $ 2.19 | $ 19.79 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 6 | 21 |
| Flight Rules | IFR | IFR | IFR |
| Manufacturer | Leonardo | Piper | Sikorsky |
| Aircraft Name | AW189 | M600 | S-92 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 651 | 1406 | 439 |
| DOC / nm / Seat | $ 0.74 | $ 0.55 | $ 0.94 |
| Max Cabin Seats | 19 | — | 19 |
| OEM Verification | Un-Verified | VERIFIED | Un-Verified |
| Standard Cabin Seats | 19 | 4 | 19 |
| Direct Operating Cost | $ 2,413 | $ 603 | $ 3,068 |
| Flight Deck (Base Spec) | EFIS | Garmin G3000 | EFIS |
| Max Cruise Speed (ktas) | 155 | 274 | 155 |
| Base Aircraft Price (USD) | $2,413,000 | $3,081,400 | $30,650,000 |
| Useful Load (lbs) | — | 2200 | 7417 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Min Crew | 1 | 1 | 2 |
| Total Seats | 21 | 5 | 21 |
| Max Cabin Seats | 19 | — | 19 |
| Standard Cabin Seats | 19 | 4 | 19 |
| Lavatory | — | No | — |
| Galley Location | — | MID | — |
| Cabin Pressure (psi) | — | 5.6 | — |
| Galley / Refreshment | — | Refreshment Centre | — |
| SL Cabin Altitude (ft) | — | 12600 | — |
| Max Cabin Altitude (ft) | — | 8644 | — |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | CT7-2E1 | PT6A-42A | CT7-8A |
| Fuel Type | JetFuel | — | JetFuel |
| TBO (hrs) | 4000 | 3600 | 4000 |
| Horsepower | 1983 | 600 | 2520 |
| No. of Engines | 2 | 1 | 1 |
| Flat Rating | — | ISA + 55 | — |
| Fuel Capacity (gal) | — | 260 | 760 |
| Dimensions | |||
| Length (ft) | 57.8 | 29.7 | — |
| Overall Height (ft) | 16.6 | 11.3 | 17.8 |
| Rotor Diameter (ft) | 48 | — | — |
| Cabin Volume (cu. ft) | 395 | 165 | 775 |
| Baggage Volume Ext. (cu. ft) | 85 | — | 140 |
| Wingspan (ft) | — | 43.2 | — |
| Cabin Width (ft) | — | 4.1 | — |
| Cabin Height (ft) | — | 4 | — |
| Cabin Length (ft) | — | 12.3 | — |
| Baggage Volume Int. (cu. ft) | — | 20 | — |