STC SA01447SE
FAA DRS lists SA01447SE as Current · Issued, held by Micro AeroDynamics Inc, for Cessna Aircraft 120 and Cessna Aircraft 140. Recorded change: Installation of vortex generators on the wings and horizontal tail surfaces of the above model aircraft in accordance with Drawing Package MA2201, Revision IR, dated July 28, 2004, and Installation Manual MA2202, Revision IR, dated August 16, 2004, 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 horizontal tail surfaces of the above model aircraft in accordance with Drawing Package MA2201, Revision IR, dated July 28, 2004, and Installation Manual MA2202, Revision IR, dated August 16, 2004, or later FAA approved revision to either of these documents.
SA01447SE 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 120 and Cessna Aircraft 140. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Cessna Aircraft 120 and Cessna Aircraft 140 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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