N260NV

This airframe, registered as N260NV, is an Airbus A320-214 built in 2009 with manufacturer serial number 4104. The airframe is recorded as owned by the corporation BANK OF UTAH TRUSTEE, located in Salt Lake City, UT, US, and carries a US registration. No public record of a change in operational operator or home-base assignment is published for this specific airframe, and valuation and detailed condition reports are not published in the supplied data. Registry actions beyond the assignment of the US registration are not provided.

The airframe is outfitted in a 182-seat single-class high-density layout (operator configuration) tailored for high-capacity short- to medium-haul operations; this configuration emphasizes maximum passenger density over multi-class amenities. Specific avionics fit and in-service operator identity are not published in the supplied data, so details such as cockpit avionics suite, cabin entertainment, or seat pitch are not available. Typical mission profiles for this configuration, given the listed cruise speed and range, would concentrate on dense-route point-to-point services within the aircraft’s 3,300 nm capability, operating from bases consistent with a US registration. Maintenance considerations specific to this aircraft include management of the twin CFM56-5B4/3 engines and the airframe’s life since its 2009 build year, although documented maintenance status is not provided.

As an Airbus-manufactured A320-214 airframe, this example occupies the fixed-wing multi-engine narrow-body category with a 182-seat high-density layout emphasizing passenger throughput within the listed performance envelope (cruise 447 kts, ceiling 41,000 ft). Buyer and charter demand considerations for such an airframe typically hinge on seating density, engine type, and remaining structural life since manufacture; specific resale or market valuation data for N260NV are not published in the provided dataset. Maintenance and resale prospects will be influenced by hours, cycles, and engine condition tied to the twin CFM56-5B4/3 propulsion system.