Cessna Citation M2 vs Daher Tbm 910 vs Daher Tbm 960 vs Piaggio Avanti Evo
The Cessna Citation M2 is a light twin‑jet, typically used for short to midrange business hops. It generally offers about 1,550 nautical miles of range and is usually configured for around 5–7 passengers, trading maximum cruise comfort and jet smoothness for smaller cabin volume than larger jets. The Daher TBM 910 and TBM 960 are single‑engine turboprops in the fast personal/corporate transport category. Both are commonly equipped for about 4–6 passengers, with range typically around 1,700 nautical miles. The TBM 960 is the newer, more refined evolution, generally emphasizing improved automation, efficiency, and cabin/cockpit upgrades rather than a big step change in passenger count. The Piaggio Avanti EVO is a twin‑turboprop executive aircraft with a distinctive design and a cabin that often feels more spacious than typical single‑engine turboprops. It is commonly configured for about 6–7 passengers and offers roughly 1,700–1,800 nautical miles of range, positioning it as a higher‑capacity turboprop option with strong cruise performance.
| Spec | Cessna Citation M2 | Daher TBM 910 | Daher TBM 960 | Piaggio Avanti EVO |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 3.45 | $ 2.25 | $ 2.25 | — |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 6 | 6 | 8 |
| Manufacturer | Cessna Citation | Daher TBM | Daher TBM | Piaggio |
| Aircraft Name | M2 | TBM 910 | TBM 960 | Avanti EVO |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1730 | 1730 | 1530 |
| DOC / nm / Seat | $ 0.58 | $ 0.56 | $ 0.56 | — |
| Max Cabin Seats | 7 | — | — | 7 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3810 | 2908 | 2908 | 3775 |
| Standard Cabin Seats | 6 | 4 | 4 | 6 |
| Direct Operating Cost | $ 1,395 | $ 744 | $ 744 | — |
| Flight Deck (Base Spec) | Garmin G3000 | Garmin G1000 NXi | Garmin G3000 | Rockwell Collins Pro Line 21 |
| Max Cruise Speed (ktas) | 404 | 330 | 330 | 400 |
| Base Aircraft Price (USD) | $5,150,000 | $4,250,000 | $4,450,000 | $ 7,695,000 |
| Flight Rules | — | IFR | IFR | IFR |
| Aircraft Type | — | — | Turbo Prop | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | No | No |
| Min Crew | 1 | 1 | 1 | 1 |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 8 | 6 | 6 | 8 |
| Max Cabin Seats | 7 | — | — | 7 |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 8.5 | 6.2 | 6.2 | 9 |
| Galley / Refreshment | No | Refreshment Centre | — | No |
| Standard Cabin Seats | 6 | 4 | 4 | 6 |
| SL Cabin Altitude (ft) | 22027 | 14390 | 14390 | 24000 |
| Galley Location | — | MID | MID | — |
| Max Cabin Altitude (ft) | — | — | — | 6600 |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | FJ44-1AP-21 | PT6A-66D | TBM 960 | PT6A–66B |
| TBO (hrs) | 3500 | 3500 | 3500 | 3600 |
| Flat Rating | ISA + 7 | ISA + 49 | ISA + 49 | ISA + 28 |
| Thrust (lbs) | 1965 | — | — | — |
| No. of Engines | 2 | 1 | — | 2 |
| Fuel Burn (lbph) | 516 | — | — | — |
| Fuel Capacity (gal) | 492 | 291 | — | — |
| Horsepower | — | 850 | 850 | 850 |
| Fuel Burn (gph) | — | 37 | — | 100 |
| Dimensions | ||||
| Length (ft) | 42.6 | 35.3 | 35.3 | 47.3 |
| Wingspan (ft) | 47.3 | 42.1 | 42.1 | 47.1 |
| Aisle Step (ft) | 0.4 | — | — | — |
| Cabin Width (ft) | 4.8 | 4 | 4 | 6.1 |
| Cabin Height (ft) | 4.8 | 4.1 | 4.1 | 5.8 |
| Cabin Length (ft) | 11 | 13.4 | 13.4 | 14.9 |
| Overall Height (ft) | 14 | 14.3 | — | 13.1 |
| Cabin Width - Floor (ft) | 3.1 | — | — | 3.5 |
| Cabin Length - Seating (ft) | 8.8 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 46 | — | — | — |
| Cabin Volume (cu. ft) | — | 123 | 123 | — |
| Baggage Volume Int. (cu. ft) | — | 30 | — | 35.2 |