Cessna Citation M2 vs Daher Tbm 960 vs Piaggio Avanti Evo vs Pilatus Pc 12 Ngx
The Cessna Citation M2 is a light jet aimed at short-to-medium business trips. It typically carries about 6–7 passengers in a compact cabin and offers roughly 1,200–1,500 nautical miles of range depending on reserves, payload, and conditions. The Daher TBM 960 is a high-performance single‑engine turboprop optimized for owner-operators; it generally seats 4–6 passengers in comfort (up to about 6–7 including crew configurations) and is usually in the ~1,300–1,700 nautical mile range. The Piaggio Avanti EVO is a twin‑engine turboprop with a stand‑up-style cabin feel for its class; it commonly accommodates 7–9 passengers and delivers about ~1,500–1,800 nautical miles. The Pilatus PC‑12 NGX is a utility‑oriented single‑engine turboprop with the most flexible cabin and baggage/cargo capability here; it typically carries 6–9 passengers (often up to 10 in high-density layouts) and offers roughly ~1,500–1,800+ nautical miles. In general, the M2 emphasizes jet speed and simplicity, the TBM 960 prioritizes efficient point-to-point performance, the Avanti EVO targets cabin comfort with turboprop economics, and the PC‑12 NGX leads in versatility.
| Spec | Cessna Citation M2 | Daher TBM 960 | Piaggio Avanti EVO | Pilatus PC-12 NGX |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 3.45 | $ 2.25 | — | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 6 | 8 | 8 |
| Manufacturer | Cessna Citation | Daher TBM | Piaggio | Pilatus |
| Aircraft Name | M2 | TBM 960 | Avanti EVO | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1730 | 1530 | 1803 |
| DOC / nm / Seat | $ 0.58 | $ 0.56 | — | $ 0.46 |
| Max Cabin Seats | 7 | — | 7 | 9 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | VERIFIED |
| Useful Load (lbs) | 3810 | 2908 | 3775 | — |
| Standard Cabin Seats | 6 | 4 | 6 | 6 |
| Direct Operating Cost | $ 1,395 | $ 744 | — | $ 793 |
| Flight Deck (Base Spec) | Garmin G3000 | Garmin G3000 | Rockwell Collins Pro Line 21 | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 404 | 330 | 400 | 290 |
| Base Aircraft Price (USD) | $5,150,000 | $4,450,000 | $ 7,695,000 | $5,350,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Aircraft Type | — | Turbo Prop | — | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | No | Optional |
| Min Crew | 1 | 1 | 1 | 1 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 8 | 6 | 8 | 8 |
| Max Cabin Seats | 7 | — | 7 | 9 |
| Lavatory Location | AFT | — | — | FWD |
| Cabin Pressure (psi) | 8.5 | 6.2 | 9 | 5.8 |
| Galley / Refreshment | No | — | No | No |
| Standard Cabin Seats | 6 | 4 | 6 | 6 |
| SL Cabin Altitude (ft) | 22027 | 14390 | 24000 | 13100 |
| Galley Location | — | MID | — | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Cargo Door | — | — | — | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | FJ44-1AP-21 | TBM 960 | PT6A–66B | PT6E-67XP |
| TBO (hrs) | 3500 | 3500 | 3600 | 5000 |
| Flat Rating | ISA + 7 | ISA + 49 | ISA + 28 | ISA + 35 |
| Thrust (lbs) | 1965 | — | — | — |
| No. of Engines | 2 | — | 2 | 1 |
| Fuel Burn (lbph) | 516 | — | — | — |
| Fuel Capacity (gal) | 492 | — | — | — |
| Horsepower | — | 850 | 850 | 1200 |
| Fuel Burn (gph) | — | — | 100 | — |
| Usable Fuel (gal) | — | — | — | 402 |
| Dimensions | ||||
| Length (ft) | 42.6 | 35.3 | 47.3 | 47.25 |
| Wingspan (ft) | 47.3 | 42.1 | 47.1 | 53.33 |
| Aisle Step (ft) | 0.4 | — | — | — |
| Cabin Width (ft) | 4.8 | 4 | 6.1 | 5 |
| Cabin Height (ft) | 4.8 | 4.1 | 5.8 | 4.9 |
| Cabin Length (ft) | 11 | 13.4 | 14.9 | 16.9 |
| Overall Height (ft) | 14 | — | 13.1 | 14 |
| Cabin Width - Floor (ft) | 3.1 | — | 3.5 | 4.25 |
| Cabin Length - Seating (ft) | 8.8 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 46 | — | — | — |
| Cabin Volume (cu. ft) | — | 123 | — | — |
| Baggage Volume Int. (cu. ft) | — | — | 35.2 | 40 |