Description
The 0511162-11 is a genuine Textron Aviation spar assembly — a primary load-bearing member of the wing, carrying principal bending and flight loads. It is applicable to the Skyhawk. It carries an export classification of ECCN 9A991, weighs 3.26 pounds, and measures 47 (L) x 3 (W) x 2.5 (H) Inches.
As an original-equipment (OEM) structural part supplied directly by Textron Aviation, the 0511162-11 is manufactured to the aircraft maker's specification for material, dimensions, and finish, and cross-references the type design exactly as documented in the maintenance data. For a structural member, the genuine correctly identified part preserves the engineered load paths and keeps the airframe configuration-correct.
Parts like this are shared across the Cessna Skyhawk aircraft, reflecting how much structure and hardware these models have in common.
As a load-bearing element, a part in this role must match the original material and dimensions precisely to keep the airframe's engineered strength intact. Because substitutions on type-certificated aircraft require approved data, the genuine part is the straightforward, compliant choice for this application.
Genuine factory parts carry the documentation and traceability that maintenance and airworthiness records depend on — assurance a look-alike substitute cannot provide.
Cessna traces to the company Clyde Cessna founded in Wichita, Kansas in 1927; Textron Inc. acquired it in 1992, and since 2014 it has anchored Textron Aviation alongside Beechcraft and Hawker. With over 44,000 built, the Cessna Skyhawk is the best-selling aircraft ever made and is still produced today.
Request a quote for 0511162-11, or browse more Cessna Skyhawk parts on Flying411.
