Cessna 182 Skylane vs Daher Tbm 960 vs Pilatus Pc 12 Ngx vs Piper M600 Sls
The Cessna 182 Skylane is a piston, fixed-gear single best suited to personal and training missions. It typically offers the shortest range of this group (often roughly 700–900 nautical miles depending on configuration and reserves) and usually seats four with a realistic load, sometimes up to five with compromises. The Piper M600 SLS is an entry-level pressurized single-engine turboprop aimed at owner-pilots stepping up in speed and altitude. It generally carries five to six people and offers mid-pack range (commonly around 1,000–1,300 nautical miles). The Daher TBM 960 is a high-performance, single-engine turboprop focused on fast point-to-point travel. It usually seats up to six and tends to provide the longest range among these singles (often about 1,400–1,700 nautical miles). The Pilatus PC-12 NGX is a larger, utility-oriented single-engine turboprop optimized for cabin space and flexibility. It commonly carries six to nine passengers and offers long range comparable to the TBM in many missions (often roughly 1,500–1,700 nautical miles), with superior payload and cabin volume.
| Spec | Cessna Skylane | Daher TBM 960 | Pilatus PC-12 NGX | Piper M600 SLS |
|---|---|---|---|---|
| Summary | ||||
| DOC / nm | $ 1.01 | $ 2.25 | $ 2.78 | $ 2.19 |
| Total Seats | 4 | 6 | 8 | 6 |
| Flight Rules | VFR | IFR | IFR | IFR |
| Manufacturer | Cessna | Daher TBM | Pilatus | Piper |
| Aircraft Name | 182 Skylane | TBM 960 | PC-12 NGX | M600 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 915 | 1730 | 1803 | 1406 |
| DOC / nm / Seat | $ 0.25 | $ 0.56 | $ 0.46 | $ 0.55 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Direct Operating Cost | $ 146 | $ 744 | $ 793 | $ 603 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Garmin G3000 | Honeywell Primus Apex | Garmin G3000 |
| Max Cruise Speed (ktas) | 145 | 330 | 290 | 274 |
| Base Aircraft Price (USD) | $530,000 | $4,450,000 | $5,350,000 | $3,081,400 |
| Cockpit | — | 2 | 2 | 2 |
| Min Crew | — | 1 | 1 | 1 |
| Aircraft Type | — | Turbo Prop | — | — |
| Useful Load (lbs) | — | 2908 | — | 2200 |
| Standard Cabin Seats | — | 4 | 6 | 4 |
| Max Cabin Seats | — | — | 9 | — |
| Cabin | ||||
| Total Seats | 4 | 6 | 8 | 5 |
| Cockpit | — | 2 | 2 | 2 |
| Lavatory | — | No | Optional | No |
| Min Crew | — | 1 | 1 | 1 |
| Galley Location | — | MID | — | MID |
| Cabin Pressure (psi) | — | 6.2 | 5.8 | 5.6 |
| Standard Cabin Seats | — | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | — | 14390 | 13100 | 12600 |
| Cargo Door | — | — | Yes | — |
| Max Cabin Seats | — | — | 9 | — |
| Lavatory Location | — | — | FWD | — |
| Galley / Refreshment | — | — | No | Refreshment Centre |
| Max Cabin Altitude (ft) | — | — | — | 8644 |
| Engine | ||||
| FADEC | No | Yes | Yes | No |
| Model | IO-540-AB1A5 | TBM 960 | PT6E-67XP | PT6A-42A |
| Fuel Type | AvGas | — | — | — |
| TBO (hrs) | 2000 | 3500 | 5000 | 3600 |
| TBO (yrs) | 12 | — | — | — |
| Horsepower | 245 | 850 | 1200 | 600 |
| Fuel Delivery | Fuel Injected | — | — | — |
| No. of Engines | 1 | — | 1 | 1 |
| Fuel Capacity (gal) | 87 | — | — | 260 |
| Flat Rating | — | ISA + 49 | ISA + 35 | ISA + 55 |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 29 | 35.3 | 47.25 | 29.7 |
| Wingspan (ft) | 36 | 42.1 | 53.33 | 43.2 |
| Cabin Width (ft) | 3.5 | 4 | 5 | 4.1 |
| Cabin Height (ft) | 4.1 | 4.1 | 4.9 | 4 |
| Cabin Length (ft) | 11.2 | 13.4 | 16.9 | 12.3 |
| Overall Height (ft) | 9.4 | — | 14 | 11.3 |
| Baggage Volume Int. (cu. ft) | 32 | — | 40 | 20 |
| Cabin Volume (cu. ft) | — | 123 | — | 165 |
| Cabin Width - Floor (ft) | — | — | 4.25 | — |