Cessna Citation M2 vs Cirrus Vision Jet G2 vs Daher Tbm 910 vs Honda Aircraft Hondajet Elite
The Cessna Citation M2 and HondaJet Elite are very light jets aimed at short-to-midrange business trips, typically seating a single pilot plus about five to six passengers in practical layouts, with ranges generally around the 1,200–1,400 nautical mile class depending on reserves and mission profile. The Cirrus Vision Jet G2 is also a light jet but positioned as an owner-flown, single-engine personal jet; it commonly carries four to five passengers plus a pilot (with flexible seating), and its range is usually in a similar but slightly lower bracket, roughly around 1,000–1,200 nautical miles. The Daher TBM 910 is a high-performance single-engine turboprop rather than a jet; it often carries four to six passengers plus a pilot and is known for strong real-world range, commonly around 1,500 nautical miles or more, making it the longest-legged option of this group. Overall, the jets emphasize higher cruise speeds and jet comfort, while the TBM prioritizes efficiency and longer reach with excellent runway flexibility.
| Spec | Cessna Citation M2 | Cirrus Vision Jet G2 | Daher TBM 910 | 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 910 | 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 G1000 NXi | Garmin G3000 |
| Max Cruise Speed (ktas) | 404 | 311 | 330 | 419 |
| Base Aircraft Price (USD) | $5,150,000 | $2,315,000 | $4,250,000 | $ 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 | — |
| Fuel Burn (gph) | — | — | 37 | — |
| 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 | — |