Description
The 000-110011-602 is a genuine Textron Aviation front spar assembly that forms part of the wing's primary load-carrying structure. It carries an export classification of ECCN 9A991.
Structural parts like this carry and transfer loads through the airframe, so exact form and fit are essential to preserving the design's strength and fatigue life. OEM parts arrive to the specification the type design was certified against, preserving both airworthiness and the airframe's documented configuration.
Because interchangeability rules can apply, confirm the exact applicable part for your configuration in the IPC before installation. Because this is a component for a type-certificated aircraft, using the manufacturer's part keeps the installation within approved configuration and simplifies compliance.
Applicability should always be confirmed against the aircraft's IPC and effectivity records prior to fitting the part. Genuine sourcing means the part matches the drawing exactly, so fit and function are known quantities rather than a gamble at installation.
An unapproved or surplus substitute can introduce fit, material, or paperwork problems that surface at the next inspection; the genuine part avoids that risk. For a regulated aircraft component, correct identification by factory part number is what guarantees the exact form, fit, and function the design calls for.
Textron Aviation's roots reach back to Clyde Cessna's 1927 company and the Beech family's 1932 firm, both founded in Wichita, Kansas.
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