N804MS

The airframe bearing tail number N804MS is a Boeing 767-3P6 (767-300) built in 1993 with manufacturer serial number 27255. This airliner is registered in the United States (Registration: US) and is recorded as owned by INTERFACE OPERATIONS LLC, an LLC based in Las Vegas, NV, US. The documented ownership history for this specific airframe is limited to the current owner on file; no publicly noted earlier operators or major incident records are published. Condition and valuation notes for this individual ship are not published.

The Boeing 767-3P6 configuration for this registration supports a standard widebody passenger layout accommodating 290 seats, consistent with high-density three-class or typical two-class conversions for mainline and charter use. Avionics and systems fit for this airframe follow Boeing and operator retrofit practices for 767-300 type aircraft of the early 1990s; specific avionics fit for N804MS are not published. With a design range of 5,980 nautical miles and a cruise of 460 knots, typical mission profiles include transcontinental and transoceanic sectors as well as high-utilization charter operations originating from the owner’s Las Vegas base. Maintenance considerations reflect its vintage—airworthiness programs for 1993-build 767-300s emphasize structural inspection, engine shop visits for GE CF6-80 series modules, and systems upgrades when repurposed for VIP or high-density roles.

The Boeing 767-300 family occupies the medium widebody niche, offering long-range capability with efficient twin-engine economics; the CF6-80 series engines rated at 47,600 lbf each provide the thrust required for its 43,000 ft ceiling and extended-range missions. Competing types historically include the Airbus A330-200 and later-generation narrowbody transcontinental aircraft when configured in higher-density layouts. Market demand for 767-300 airframes tends toward cargo conversion, long-haul charter, or niche freighter/service roles, and resale maintenance considerations frequently center on engine life remaining, structural fatigue life, and required avionics modernization for current regulatory compliance.