N212LP

The airframe bearing registration N212LP is a 1998-built Cessna 560 Citation Ultra, serial number 560-0483, manufactured by Cessna (Textron Aviation). Publicly available records do not include a detailed ownership timeline; ownership timeline not published. The operator and home base for this specific airframe are not published in the provided data, and there are no listed notable registry actions in the supplied dataset. Condition and valuation details for this particular aircraft are not published.

The cabin of N212LP is configured with a forward single seat opposite a refreshment center, a mid-cabin four-place club arrangement with fold-out tables, and an aft pair of forward-facing seats plus a belted lavatory seat, supporting mixed executive transport and short-haul corporate missions. The avionics fit is a Honeywell Primus 1000 suite with triple DU-870 EFIS displays, enabling modern glass-cockpit situational awareness for precision navigation and reduced pilot workload. Typical mission profiles for this airframe, given its 1,960 nm range and 430 kt cruise, would include transcontinental U.S. hops and regional business trips; specific operator base and route logs for this tail number are not published. Maintenance considerations for the airframe follow those of late-1990s Citation Ultras, with attention to JT15D-5D engine programs and avionics life-cycle support for the Primus 1000 installation.

The Cessna 560 Citation Ultra occupies the light corporate jet niche, offering higher cruise speeds and service ceiling than many entry-level business jets of its era while keeping operating complexity moderate. Competing models in the late-1990s and early-2000s market included light jets equipped with similar range and speed, such as early Learjet and Hawker variants. Buyer and charter demand for a well-maintained Citation Ultra typically emphasizes cabin flexibility (notably the seven-seat layout shown on N212LP), reliable JT15D engine support, and avionics upgrades; resale considerations for this serial are influenced by engine program status, the condition of the Honeywell Primus 1000 installation, and the documented maintenance history, which is not published for this specific airframe.