Beechcraft Kingair Denali vs Cessna Citation Cj3 vs Cessna Citation Cj4 vs Cessna Citation M2 vs Daher Tbm 960 vs Embraer Phenom 300e vs Pilatus Pc 12 Ngx
The Beechcraft Denali, Daher TBM 960, and Pilatus PC-12 NGX are single‑engine turboprops, generally best for shorter-to-medium missions with excellent access to shorter or rougher runways. Among them, the PC‑12 NGX typically offers the most cabin and payload flexibility and commonly seats the most passengers (often 6–9), while the TBM 960 and Denali are usually configured around 4–6 passengers with a more “owner‑pilot” mission. In range, these turboprops commonly sit roughly in the 1,300–1,800 nm class depending on reserves and load, with the PC‑12 often competitive at the high end. The Cessna Citation M2 is an entry light jet, typically seating about 4–6 with the shortest range of the jets here (roughly ~1,000–1,300 nm). The Citation CJ3+ and CJ4 step up in cabin size and capability; both are commonly 6–9 seats, with CJ4 generally offering the longer range (often ~1,900–2,100 nm) versus CJ3+ (~1,800–2,000 nm). The Embraer Phenom 300E is a high‑performing light jet, typically 6–9 seats, with range broadly comparable to CJ4 (often ~1,900–2,000+ nm depending on configuration).
| Spec | Beechcraft KingAir Denali | Cessna Citation CJ3+ | Cessna Citation CJ4 | Cessna Citation M2 | Daher TBM 960 | Embraer Phenom 300E | Pilatus PC-12 NGX |
|---|---|---|---|---|---|---|---|
| Summary | |||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 | 2 |
| DOC / nm | $ 4.08 | $ 4.05 | $ 4.37 | $ 3.45 | $ 2.25 | $ 3.88 | $ 2.78 |
| Min Crew | 1 | 1 | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 9 | 9 | 8 | 6 | 10 | 8 |
| Flight Rules | IFR | — | — | — | IFR | — | IFR |
| Manufacturer | GE® Aerospace | Cessna Citation | Cessna Citation | Cessna Citation | Daher TBM | Embraer | Pilatus |
| Aircraft Name | KingAir Denali | CJ3+ | CJ4 | M2 | TBM 960 | Phenom 300E | PC-12 NGX |
| Certification | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 1600 | 1898 | 2170 | 1400 | 1730 | 2,010 | 1803 |
| DOC / nm / Seat | $ 0.68 | $ 0.58 | $ 0.62 | $ 0.58 | $ 0.56 | $ 0.55 | $ 0.46 |
| Max Cabin Seats | 9 | 8 | 8 | 7 | — | 10 | 9 |
| OEM Verification | VERIFIED | VERIFIED | VERIFIED | VERIFIED | Un-Verified | VERIFIED | VERIFIED |
| Useful Load (lbs) | 3280 | 5530 | 6914 | 3810 | 2908 | 6914 | — |
| Standard Cabin Seats | 7 | 7 | 7 | 6 | 4 | 6 | 6 |
| Direct Operating Cost | $ 1,111 | $ 1,680 | $ 1,970 | $ 1,395 | $ 744 | $ 1,758 | $ 793 |
| Flight Deck (Base Spec) | Rockwell Collins Pro Line Fusion | Garmin G3000 | Rockwell Collins Pro Line 21 | Garmin G3000 | Garmin G3000 | Prodigy Touch (G3000) | Honeywell Primus Apex |
| Max Cruise Speed (ktas) | 285 | 415 | 440 | 404 | 330 | 464 | 290 |
| Base Aircraft Price (USD) | $4,150,000 | $9,915,000 | $11,290,000 | $5,150,000 | $4,450,000 | $9,650,000 | $5,350,000 |
| Aircraft Type | — | — | — | — | Turbo Prop | — | — |
| Cabin | |||||||
| Cockpit | 2 | 2 | 2 | 2 | 2 | 2 | 2 |
| Lavatory | 1 Flushing | 1 Enclosed Belted Flushing | 1 Enclosed Belted Flushing | 1 Enclosed Belted Flushing | No | 1 Enclosed Flushing | Optional |
| Min Crew | 1 | 1 | 1 | 1 | 1 | 1 | 1 |
| Total Seats | 11 | 9 | 9 | 8 | 6 | 9 | 8 |
| Max Cabin Seats | 9 | 8 | 8 | 7 | — | 9 | 9 |
| Lavatory Location | AFT | AFT | AFT | AFT | — | AFT | FWD |
| Cabin Pressure (psi) | 5 | 8.9 | 9 | 8.5 | 6.2 | 9.4 | 5.8 |
| Galley / Refreshment | No | Galley | Galley | No | — | Galley | No |
| Standard Cabin Seats | 7 | 7 | 7 | 6 | 4 | 7 | 6 |
| SL Cabin Altitude (ft) | 11065 | 23586 | 24005 | 22027 | 14390 | 25560 | 13100 |
| Crew Rest | — | No | No | No | — | No | — |
| Jump Seat | — | No | No | No | — | No | — |
| Galley Location | — | FWD | FWD | — | MID | FWD | — |
| Cargo Door | — | — | — | — | — | — | Yes |
| Engine | |||||||
| Model | Catalyst™ | FJ44-3A | FJ44-4A | FJ44-1AP-21 | TBM 960 | Canada PW535E1 | PT6E-67XP |
| No. of Engines | 1 | 2 | 2 | 2 | — | 2 | 1 |
| FADEC | — | Yes | Yes | Yes | Yes | Yes | Yes |
| TBO (hrs) | — | 5000 | 5000 | 3500 | 3500 | 5000 | 5000 |
| Flat Rating | — | ISA + 11 | ISA + 11 | ISA + 7 | ISA + 49 | ISA + 15 | ISA + 35 |
| Thrust (lbs) | — | 2820 | 3621 | 1965 | — | 3360 | — |
| Fuel Burn (lbph) | — | 624 | 757 | 516 | — | 757 | — |
| Fuel Capacity (gal) | — | 703 | 870 | 492 | — | — | — |
| Horsepower | — | — | — | — | 850 | — | 1200 |
| Usable Fuel (gal) | — | — | — | — | — | — | 402 |
| Dimensions | |||||||
| Length (ft) | 14.86 | 51.2 | 53.4 | 42.6 | 35.3 | 51.2 | 47.25 |
| Wingspan (ft) | 54.3 | 53 | 50 | 47.3 | 42.1 | 52.16 | 53.33 |
| Cabin Width (ft) | 4.5 | 4.8 | 4.8 | 4.8 | 4 | 5.1 | 5 |
| Cabin Height (ft) | 4.8 | 4.8 | 4.8 | 4.8 | 4.1 | 4.9 | 4.9 |
| Cabin Length (ft) | 12.6 | 15.7 | 17.2 | 11 | 13.4 | 17.2 | 16.9 |
| Overall Height (ft) | 4.65 | 15.2 | 15.5 | 14 | — | 16.75 | 14 |
| Cabin Width - Floor (ft) | 4.1 | 3.1 | 3.1 | 3.1 | — | 3.6 | 4.25 |
| Cabin Length - Seating (ft) | 12.6 | 12.2 | 14.8 | 8.8 | — | 14.8 | — |
| Baggage Volume Int. (cu. ft) | 48 | — | 7 | — | — | 10 | 40 |
| Aisle Step (ft) | — | 0.4 | 0.4 | 0.4 | — | 0.3 | — |
| Baggage Volume Ext. (cu. ft) | — | 65 | 70 | 46 | — | 74 | — |
| Cabin Volume (cu. ft) | — | — | — | — | 123 | — | — |