STC SA01058SE
FAA DRS lists SA01058SE as Current · Issued, held by Micro AeroDynamics Inc, for Cessna Aircraft 210R, Cessna Aircraft P210R, and Cessna Aircraft T210R. Recorded change: Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2165, Revision IR, dated February 14, 2002, and Installation Manual MA2166, Revision IR, dated February 25, 2002, or later FAA approved revision of either of these documents. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2165, Revision IR, dated February 14, 2002, and Installation Manual MA2166, Revision IR, dated February 25, 2002, or later FAA approved revision of either of these documents.
SA01058SE identifies the approval, recorded holder, named aircraft, and modification scope. It does not confirm kit availability, serial-number effectivity, data rights, price, or installation authority.
Applicability
Aircraft named in FAA DRS
Named aircraft: Cessna Aircraft 210R, Cessna Aircraft P210R, and Cessna Aircraft T210R. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Cessna Aircraft 210R and Cessna Aircraft P210R, and 1 more aircraft configuration model, serial range, and configuration?
- 02Which configuration, parts, installation data, limitations, and ICAs apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
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