N411XT

The airframe bearing tail number N411XT is a 2003-built Bombardier Global Express airliner, officially a Bombardier Global Express (BD-700-1A10) with manufacturer serial 9133. The airframe is registered in the US and is recorded as owned by TVPX Aircraft Solutions Inc Trustee, a corporate owner based in North Salt Lake, UT, US. The aircraft is a fixed-wing multi-engine transport configured for 23 seats in a transport layout; the operator layout may vary. Public registry traces and valuation specifics are not published beyond the corporate ownership and basic registration details.

This specific Global Express is noted in a 23-seat transport cabin configuration, though the operator’s layout may differ from the published transport fit. As registered to TVPX Aircraft Solutions Inc Trustee in North Salt Lake, UT, US, the aircraft’s operational basing is tied to that corporate owner location and to its US registration. Typical mission parameters for this airframe follow the published performance envelope: long-range flights up to 6,400 nm at high-altitude cruise near 51,000 ft and cruise speeds around 488 kts, supporting transcontinental or intercontinental transport missions in a commercial or corporate transport role. Specific avionics fit, interior appointments, and recent maintenance records for this airframe are not published in the supplied data.

As a member of the Bombardier Global Express family, the Bombardier Global Express (BD-700-1A10) airframe identified as N411XT leverages a high-thrust powerplant pair (BMW Rolls BR700-710A220, 14,750 lbf each) to achieve long-range, high-altitude performance, exemplified by its 6,400 nm range and 51,000 ft ceiling. The 23-seat transport configuration positions this airframe for high-capacity executive or specialized transport roles within the long-range business jet segment. Market considerations for this specific serial (9133) and build year (2003) hinge on registry, ownership, and any supplemental records not provided here; resale, maintenance, and conversion options would be evaluated against the airframe’s published performance and configuration data.