Cessna Citation M2 vs Daher Tbm 910 vs Piaggio Avanti Evo vs Piper M350
The Cessna Citation M2 is a light twin‑jet aimed at fast, short‑to‑medium business trips. It typically carries 5–7 people depending on layout and offers roughly a 1,300‑nautical‑mile range. The Daher TBM 910 is a high‑performance single‑engine turboprop focused on owner‑operators; it generally seats 4–6 in comfort (up to about 6) and is known for longer legs, around 1,700–1,800 nautical miles. The Piaggio Avanti EVO is a distinctive twin‑turboprop that competes on cabin comfort and speed; it commonly seats 7–9 and delivers about 1,700–1,800 nautical miles, making it a strong option for carrying more passengers farther than typical light jets while staying in turboprop economics. The Piper M350 is a pressurized piston single in the high‑end personal aviation category; it usually seats 5–6 and has a shorter range, roughly 1,200–1,300 nautical miles, best suited to regional trips rather than frequent long cross‑countries.
| Spec | Cessna Citation M2 | Daher TBM 910 | Piaggio Avanti EVO | Piper M350 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 3.45 | $ 2.25 | — | $ 1.34 |
| Min Crew | 1 | 1 | 1 | — |
| Total Seats | 8 | 6 | 8 | 6 |
| Manufacturer | Cessna Citation | Daher TBM | Piaggio | Piper |
| Aircraft Name | M2 | TBM 910 | Avanti EVO | M350 |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1730 | 1530 | 1343 |
| DOC / nm / Seat | $ 0.58 | $ 0.56 | — | $ 0.22 |
| Max Cabin Seats | 7 | — | 7 | — |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3810 | 2908 | 3775 | 1308 |
| Standard Cabin Seats | 6 | 4 | 6 | 4 |
| Direct Operating Cost | $ 1,395 | $ 744 | — | $ 285 |
| Flight Deck (Base Spec) | Garmin G3000 | Garmin G1000 NXi | Rockwell Collins Pro Line 21 | Garmin G1000 NXi |
| Max Cruise Speed (ktas) | 404 | 330 | 400 | 213 |
| Base Aircraft Price (USD) | $5,150,000 | $4,250,000 | $ 7,695,000 | $1,195,000 |
| Flight Rules | — | IFR | IFR | VFR |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | No | — |
| Min Crew | 1 | 1 | 1 | — |
| Crew Rest | No | — | — | — |
| Jump Seat | No | — | — | — |
| Total Seats | 8 | 6 | 8 | 6 |
| Max Cabin Seats | 7 | — | 7 | — |
| Lavatory Location | AFT | — | — | — |
| Cabin Pressure (psi) | 8.5 | 6.2 | 9 | 5.6 |
| Galley / Refreshment | No | Refreshment Centre | No | — |
| Standard Cabin Seats | 6 | 4 | 6 | 4 |
| SL Cabin Altitude (ft) | 22027 | 14390 | 24000 | — |
| Galley Location | — | MID | — | — |
| Max Cabin Altitude (ft) | — | — | 6600 | — |
| Engine | ||||
| FADEC | Yes | Yes | Yes | No |
| Model | FJ44-1AP-21 | PT6A-66D | PT6A–66B | TIO-540-AE2A |
| TBO (hrs) | 3500 | 3500 | 3600 | 2000 |
| Flat Rating | ISA + 7 | ISA + 49 | ISA + 28 | — |
| Thrust (lbs) | 1965 | — | — | — |
| No. of Engines | 2 | 1 | 2 | 1 |
| Fuel Burn (lbph) | 516 | — | — | — |
| Fuel Capacity (gal) | 492 | 291 | — | 120 |
| Horsepower | — | 850 | 850 | 350 |
| Fuel Burn (gph) | — | 37 | 100 | — |
| Fuel Type | — | — | — | AvGas |
| TBO (yrs) | — | — | — | 12 |
| Fuel Delivery | — | — | — | Fuel Injected |
| Dimensions | ||||
| Length (ft) | 42.6 | 35.3 | 47.3 | 29 |
| Wingspan (ft) | 47.3 | 42.1 | 47.1 | 43 |
| Aisle Step (ft) | 0.4 | — | — | — |
| Cabin Width (ft) | 4.8 | 4 | 6.1 | 4.1 |
| Cabin Height (ft) | 4.8 | 4.1 | 5.8 | 4 |
| Cabin Length (ft) | 11 | 13.4 | 14.9 | 12.3 |
| Overall Height (ft) | 14 | 14.3 | 13.1 | 11.4 |
| Cabin Width - Floor (ft) | 3.1 | — | 3.5 | — |
| Cabin Length - Seating (ft) | 8.8 | — | — | — |
| Baggage Volume Ext. (cu. ft) | 46 | — | — | 13 |
| Cabin Volume (cu. ft) | — | 123 | — | 165 |
| Baggage Volume Int. (cu. ft) | — | 30 | 35.2 | 20 |