Cessna Citation M2 vs Cirrus Vision Jet G2 vs Daher Tbm 940 vs Honda Aircraft Hondajet Elite
The Cessna Citation M2 and HondaJet Elite are light jets, the Cirrus Vision Jet G2 is a very light single‑engine jet, and the Daher TBM 940 is a high‑performance single‑engine turboprop. In range, the TBM 940 generally leads (roughly 1,700+ nautical miles), followed by the Vision Jet G2 (about 1,200 nm), then the HondaJet Elite (about 1,150–1,200 nm), with the Citation M2 typically around the low‑1,000‑nm class depending on reserves and payload. For passenger capacity, the Vision Jet G2 is often marketed with up to seven seats (typically six passengers plus pilot, with a small “family” layout), the Citation M2 and HondaJet Elite commonly seat five to six passengers plus one or two pilots depending on configuration, and the TBM 940 typically carries four to six passengers plus a pilot. Overall, the M2 and HondaJet emphasize traditional light‑jet speed and cabin refinement, the Vision Jet prioritizes simplicity and owner‑pilot friendliness, and the TBM 940 trades jet speed for standout range and short‑field flexibility.
| Spec | Cessna Citation M2 | Cirrus Vision Jet G2 | Daher TBM 940 | Honda Aircraft HondaJet Elite |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 3.45 | $ 2.37 | $ 2.25 | $ 2.73 |
| Min Crew | 1 | 1 | 1 | 1 |
| Total Seats | 8 | 5 | 6 | 6 |
| Manufacturer | Cessna Citation | Cirrus | Daher TBM | Honda Aircraft |
| Aircraft Name | M2 | SF50 G2 | TBM 940 | HondaJet Elite |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1400 | 1219 | 1730 | 1495 |
| DOC / nm / Seat | $ 0.58 | $ 0.79 | $ 0.56 | $ 0.68 |
| Max Cabin Seats | 7 | 5 | — | 6 |
| OEM Verification | VERIFIED | Un-Verified | Un-Verified | Un-Verified |
| Useful Load (lbs) | 3810 | 2450 | 2908 | 3432 |
| Standard Cabin Seats | 6 | 3 | 4 | 4 |
| Direct Operating Cost | $ 1,395 | $ 711 | $ 744 | $ 1,135 |
| Flight Deck (Base Spec) | Garmin G3000 | Cirrus Perspective Touch+ (G3000) | Garmin G3000 | Garmin G3000 |
| Max Cruise Speed (ktas) | 404 | 311 | 330 | 419 |
| Base Aircraft Price (USD) | $5,150,000 | $2,315,000 | $4,450,000 | $ 5,400,000 |
| Flight Rules | — | — | IFR | — |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | No | 1 Enclosed Flushing |
| Min Crew | 1 | 1 | 1 | 1 |
| Crew Rest | No | — | — | No |
| Jump Seat | No | — | — | No |
| Total Seats | 8 | 5 | 6 | 6 |
| Max Cabin Seats | 7 | 5 | — | 6 |
| Lavatory Location | AFT | — | — | AFT |
| Cabin Pressure (psi) | 8.5 | 6.4 | 6.2 | 8.8 |
| Galley / Refreshment | No | No | Refreshment Centre | Galley |
| Standard Cabin Seats | 6 | 3 | 4 | 4 |
| SL Cabin Altitude (ft) | 22027 | — | 14390 | 23060 |
| Galley Location | — | — | MID | FWD |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | FJ44-1AP-21 | FJ33-5A | PT6A-66D | HF120-H1A |
| TBO (hrs) | 3500 | 4000 | 3500 | 5000 |
| Flat Rating | ISA + 7 | ISA + 10 | ISA + 49 | ISA + 10 |
| Thrust (lbs) | 1965 | 1846 | — | 2050 |
| No. of Engines | 2 | 1 | 1 | 2 |
| Fuel Burn (lbph) | 516 | 358 | — | — |
| Fuel Capacity (gal) | 492 | 320 | 291 | 439 |
| Horsepower | — | — | 850 | — |
| Dimensions | ||||
| Length (ft) | 42.6 | 30.7 | 35.3 | 42.7 |
| Wingspan (ft) | 47.3 | 38.7 | 42.1 | 39.8 |
| Aisle Step (ft) | 0.4 | — | — | 0.4 |
| Cabin Width (ft) | 4.8 | 5.1 | 4 | 5 |
| Cabin Height (ft) | 4.8 | — | 4.1 | 4.8 |
| Cabin Length (ft) | 11 | 11.5 | 13.4 | 12.1 |
| Overall Height (ft) | 14 | 10.9 | 14.3 | 14.9 |
| Cabin Width - Floor (ft) | 3.1 | 3.1 | — | — |
| Cabin Length - Seating (ft) | 8.8 | 9.8 | — | 10.2 |
| Baggage Volume Ext. (cu. ft) | 46 | 30 | — | 66 |
| Baggage Volume Int. (cu. ft) | — | 24 | 30 | — |
| Cabin Volume (cu. ft) | — | — | 123 | — |