Cessna Citation M2 vs Cessna Denali vs Daher Tbm 940
The Cessna Citation M2 and the Daher TBM 940 sit in different aircraft categories: the Citation M2 is a light twin‑engine business jet designed for faster high‑altitude jet travel, while the TBM 940 is a high‑performance single‑engine turboprop optimized for efficient point‑to‑point missions, often into shorter or more remote runways. In typical real‑world use, the TBM 940 generally offers longer range, often around 1,500+ nautical miles depending on payload and conditions, whereas the Citation M2 is usually closer to roughly 1,200–1,300 nautical miles with reserves, also varying by mission profile. For passenger capacity, both are commonly operated with about four to five passengers in comfort, but their maximum seating differs: the Citation M2 is typically configured for up to seven seats (including a belted lav in many layouts), while the TBM 940 typically seats up to six in the cabin plus a pilot seat, with some configurations emphasizing club seating and baggage over maximum occupancy. Overall, choose the M2 for jet speed and altitude, and the TBM 940 for range and turboprop versatility.
| Spec | Cessna Citation M2 | Daher TBM 940 |
|---|---|---|
| Summary | ||
| Cockpit | 2 | 2 |
| DOC / nm | $ 3.45 | $ 2.25 |
| Min Crew | 1 | 1 |
| Total Seats | 8 | 6 |
| Manufacturer | Cessna Citation | Daher TBM |
| Aircraft Name | M2 | TBM 940 |
| Certification | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1730 |
| DOC / nm / Seat | $ 0.58 | $ 0.56 |
| Max Cabin Seats | 7 | — |
| OEM Verification | VERIFIED | Un-Verified |
| Useful Load (lbs) | 3810 | 2908 |
| Standard Cabin Seats | 6 | 4 |
| Direct Operating Cost | $ 1,395 | $ 744 |
| Flight Deck (Base Spec) | Garmin G3000 | Garmin G3000 |
| Max Cruise Speed (ktas) | 404 | 330 |
| Base Aircraft Price (USD) | $5,150,000 | $4,450,000 |
| Flight Rules | — | IFR |
| Cabin | ||
| Cockpit | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No |
| Min Crew | 1 | 1 |
| Crew Rest | No | — |
| Jump Seat | No | — |
| Total Seats | 8 | 6 |
| Max Cabin Seats | 7 | — |
| Lavatory Location | AFT | — |
| Cabin Pressure (psi) | 8.5 | 6.2 |
| Galley / Refreshment | No | Refreshment Centre |
| Standard Cabin Seats | 6 | 4 |
| SL Cabin Altitude (ft) | 22027 | 14390 |
| Galley Location | — | MID |
| Engine | ||
| FADEC | Yes | Yes |
| Model | FJ44-1AP-21 | PT6A-66D |
| TBO (hrs) | 3500 | 3500 |
| Flat Rating | ISA + 7 | ISA + 49 |
| Thrust (lbs) | 1965 | — |
| No. of Engines | 2 | 1 |
| Fuel Burn (lbph) | 516 | — |
| Fuel Capacity (gal) | 492 | 291 |
| Horsepower | — | 850 |
| Dimensions | ||
| Length (ft) | 42.6 | 35.3 |
| Wingspan (ft) | 47.3 | 42.1 |
| Aisle Step (ft) | 0.4 | — |
| Cabin Width (ft) | 4.8 | 4 |
| Cabin Height (ft) | 4.8 | 4.1 |
| Cabin Length (ft) | 11 | 13.4 |
| Overall Height (ft) | 14 | 14.3 |
| Cabin Width - Floor (ft) | 3.1 | — |
| Cabin Length - Seating (ft) | 8.8 | — |
| Baggage Volume Ext. (cu. ft) | 46 | — |
| Cabin Volume (cu. ft) | — | 123 |
| Baggage Volume Int. (cu. ft) | — | 30 |