STC SA01137SE
FAA DRS lists SA01137SE as Current · Issued, held by Micro AeroDynamics Inc, for Univair Aircraft 108-5, Univair Aircraft 108, and Univair Aircraft 108-3, and 3 more aircraft configurations. Recorded change: Installation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2159, Revision IR, dated February 15, 2002, and Installation Manual MA2160, Revision IR, dated October 9, 2002, or later FAA approved revision to 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 MA2159, Revision IR, dated February 15, 2002, and Installation Manual MA2160, Revision IR, dated October 9, 2002, or later FAA approved revision to either of these documents.
SA01137SE 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: Univair Aircraft 108-5, Univair Aircraft 108, and Univair Aircraft 108-3, and 3 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Univair Aircraft 108-5 and Univair Aircraft 108, and 4 more aircraft configurations 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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Installation of evacuation slide container.
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Installation of Gables Engineering ATC control panel part number G6990-51. Approved only for those aircraft equipped with STC ST00137AT.
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