Cessna Citation Longitude vs Daher Tbm 910 vs Pilatus Pc 12 Ngx vs Pilatus Pc 24
The Cessna Citation Longitude is a super‑midsize business jet aimed at longer, faster trips with typical range around 3,500 nautical miles and a common passenger load of about 8 to 12. The Daher TBM 910 is a high‑performance single‑engine turboprop, best viewed as an owner‑pilot “personal transport,” with roughly 1,700 nautical miles of range and usually 4 to 6 passengers in comfort (up to about 6 in typical configurations). The Pilatus PC‑12 NGX is a larger single‑engine turboprop optimized for versatility and short or unimproved fields, offering roughly 1,800 nautical miles of range and commonly seating about 6 to 9 passengers. The Pilatus PC‑24 is a light jet designed to combine jet speed with access to shorter runways, with range around 2,000 nautical miles and typical seating for about 6 to 10 passengers. In short, the Longitude leads on range and jet cabin comfort, the TBM 910 emphasizes efficient single‑pilot speed, the PC‑12 NGX prioritizes utility and payload flexibility, and the PC‑24 bridges utility and jet performance.
| Spec | Cessna Citation Longitude | Daher TBM 910 | Pilatus PC-12 NGX | Pilatus PC-24 |
|---|---|---|---|---|
| Summary | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| DOC / nm | $ 5.23 | $ 2.25 | $ 2.78 | $ 3.71 |
| Min Crew | 2 | 1 | 1 | 1 |
| Total Seats | 10 | 6 | 8 | 6 |
| Manufacturer | Cessna Citation | Daher TBM | Pilatus | Pilatus |
| Aircraft Name | Longitude | TBM 910 | PC-12 NGX | PC-24 |
| Certification | FAA Certified | FAA / EASA | FAA / EASA | FAA / EASA |
| Max Range (nm) | 3500 | 1730 | 1803 | 2076 |
| DOC / nm / Seat | $ 0.65 | $ 0.56 | $ 0.46 | $ 0.62 |
| Max Cabin Seats | 10 | — | 9 | 10 |
| OEM Verification | Un-Verified | Un-Verified | VERIFIED | VERIFIED |
| Standard Cabin Seats | 8 | 4 | 6 | 6 |
| Direct Operating Cost | $ 2,500 | $ 744 | $ 793 | $ 1,619 |
| Flight Deck (Base Spec) | Garmin G5000 | Garmin G1000 NXi | Honeywell Primus Apex | Pilatus ACE (Primus Apex) |
| Max Cruise Speed (ktas) | 481 | 330 | 290 | 440 |
| Base Aircraft Price (USD) | $29,965,000 | $4,250,000 | $5,350,000 | $11,800,000 |
| Flight Rules | — | IFR | IFR | — |
| Useful Load (lbs) | — | 2908 | — | 6680 |
| Cabin | ||||
| Cockpit | 2 | 2 | 2 | 2 |
| Lavatory | 1 Enclosed Belted Flushing | No | Optional | 1 Enclosed Flushing |
| Min Crew | 2 | 1 | 1 | 1 |
| Crew Rest | No | — | — | No |
| Jump Seat | No | — | — | No |
| Total Seats | 10 | 6 | 8 | 6 |
| Galley Location | FWD | MID | — | FWD |
| Max Cabin Seats | 12 | — | 9 | 10 |
| Lavatory Location | AFT | — | FWD | FWD |
| Cabin Pressure (psi) | 9.7 | 6.2 | 5.8 | 9.3 |
| Galley / Refreshment | Galley | Refreshment Centre | No | Optional Refreshment Center |
| Standard Cabin Seats | 8 | 4 | 6 | 6 |
| SL Cabin Altitude (ft) | 25400 | 14390 | 13100 | 23500 |
| Cargo Door | — | — | Yes | Yes |
| Engine | ||||
| FADEC | Yes | Yes | Yes | Yes |
| Model | HTF7700L | PT6A-66D | PT6E-67XP | FJ44-4A-QPM |
| TBO (hrs) | On-Condition | 3500 | 5000 | 5000 |
| Flat Rating | ISA + 19 | ISA + 49 | ISA + 35 | ISA + 23 |
| Thrust (lbs) | 7665 | — | — | 3435 |
| No. of Engines | 2 | 1 | 1 | 2 |
| Fuel Burn (lbph) | 1478 | — | — | — |
| Horsepower | — | 850 | 1200 | — |
| Fuel Burn (gph) | — | 37 | — | — |
| Fuel Capacity (gal) | — | 291 | — | — |
| Usable Fuel (gal) | — | — | 402 | — |
| Dimensions | ||||
| Length (ft) | 73.2 | 35.3 | 47.25 | 52.2 |
| Wingspan (ft) | 68.9 | 42.1 | 53.33 | 55.8 |
| Aisle Step (ft) | Flat Floor | — | — | Flat Floor |
| Cabin Width (ft) | 6.4 | 4 | 5 | 5.6 |
| Cabin Height (ft) | 6 | 4.1 | 4.9 | 5.1 |
| Cabin Length (ft) | 25.2 | 13.4 | 16.9 | 23 |
| Overall Height (ft) | 19.4 | 14.3 | 14 | 17.4 |
| Cabin Width - Floor (ft) | 4.1 | — | 4.25 | 3.8 |
| Cabin Length - Seating (ft) | 16.5 | — | — | 17 |
| Baggage Volume Int. (cu. ft) | 112 | 30 | 40 | 90 |
| Cabin Volume (cu. ft) | — | 123 | — | — |