Cessna Grand Caravan Ex vs Md Helicopters Md 500e vs Pilatus Pc 12 Ngx
The Cessna Grand Caravan EX and Pilatus PC-12 NGX are single‑engine turboprop fixed‑wing aircraft, while the MD Helicopters MD 500E is a light turbine helicopter. In category terms, the Caravan EX is a rugged utility/commuter platform optimized for short, unimproved strips and high payload flexibility; the PC‑12 NGX is a higher‑performance turboprop suited to executive travel and longer regional missions; the MD 500E emphasizes vertical lift, tight-area access, and low-level operations where runways are unavailable. For range, the PC‑12 NGX generally offers the longest legs (roughly 1,500–1,800 nautical miles depending on load and reserves), the Grand Caravan EX is mid‑range (about 900–1,000 nautical miles), and the MD 500E is typically shorter (around 250–350 nautical miles, mission dependent). Passenger capacity also differs: the Grand Caravan EX commonly seats up to 9 passengers (plus pilot, with various configurations), the PC‑12 NGX typically carries 6–9 passengers in executive layouts (with higher-density options possible), and the MD 500E usually carries about 4 passengers plus a pilot.
| Spec | Cessna Grand Caravan EX | MD Helicopters MD 500E | Pilatus PC-12 NGX |
|---|---|---|---|
| Summary | |||
| Cockpit | 2 | 2 | 2 |
| DOC / nm | $ 3.15 | $ 2.95 | $ 2.78 |
| Min Crew | 1 | 1 | 1 |
| Total Seats | 10 | 4 | 8 |
| Flight Rules | VFR | VFR | IFR |
| Manufacturer | Cessna | MD Helicotpers | Pilatus |
| Aircraft Name | Grand Caravan EX | MD 500E | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 964 | 258 | 1803 |
| DOC / nm / Seat | $ 0.39 | $ 0.74 | $ 0.46 |
| Max Cabin Seats | 12 | 3 | 9 |
| OEM Verification | VERIFIED | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3332 | 1483 | — |
| Standard Cabin Seats | 8 | 2 | 6 |
| Direct Operating Cost | $ 614 | $ 398 | $ 793 |
| Flight Deck (Base Spec) | Garmin G1000 NXi | Gyro / Analog | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 195 | 135 | 290 |
| Base Aircraft Price (USD) | $2,695,000 | $ 2,750,000 | $5,350,000 |
| Cabin | |||
| Cockpit | 2 | 2 | 2 |
| Lavatory | No | — | Optional |
| Min Crew | 1 | 1 | 1 |
| Cargo Door | Yes | — | Yes |
| Total Seats | 10 | 4 | 8 |
| Max Cabin Seats | 12 | 3 | 9 |
| Cabin Pressure (psi) | Un-Pressurized | — | 5.8 |
| Galley / Refreshment | No | — | No |
| Standard Cabin Seats | 8 | 2 | 6 |
| Lavatory Location | — | — | FWD |
| SL Cabin Altitude (ft) | — | — | 13100 |
| Engine | |||
| FADEC | Yes | No | Yes |
| Model | PT6A-140 | 250-C20B | PT6E-67XP |
| TBO (hrs) | 4000 | 3500 | 5000 |
| Horsepower | 867 | 420 | 1200 |
| Flat Rating | ISA + 24 | — | ISA + 35 |
| No. of Engines | 1 | 1 | 1 |
| Fuel Capacity (gal) | 335 | 64 | — |
| Fuel Type | — | JetFuel | — |
| Fuel Burn (gph) | — | 35 | — |
| Usable Fuel (gal) | — | — | 402 |
| Dimensions | |||
| Length (ft) | 41.6 | 30.9 | 47.25 |
| Wingspan (ft) | 52.1 | — | 53.33 |
| Cabin Width (ft) | 5.4 | — | 5 |
| Cabin Height (ft) | 4.5 | — | 4.9 |
| Cabin Length (ft) | 16.8 | — | 16.9 |
| Overall Height (ft) | 15.1 | 8.7 | 14 |
| Baggage Volume Int. (cu. ft) | 32 | — | 40 |
| Rotor Diameter (ft) | — | 26.4 | — |
| Cabin Width - Floor (ft) | — | — | 4.25 |