STC SA00743SE
FAA DRS lists SA00743SE as Current · Amended, held by Micro AeroDynamics Inc, for New Piper Aircraft PA-23-160 and New Piper Aircraft PA-23. Recorded change: Installation of vortex generators on the wing leading edge, underside of the horizontal stabilizer, and on the vertical fin in accordance with Micro AeroDynamics Drawing List MA2117, Revision IR, dated July 14, 1999, and Installation Instructions MA2118, Revision IR, dated September 21, 1999, or later FAA approved revisions to either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
SA00743SE 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: New Piper Aircraft PA-23-160 and New Piper Aircraft PA-23. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
Related aircraft structures STCs
Installation of vortex generators on the wing and verticle tail, and strakes on the nacelles.
FAA holder: Micro AeroDynamics Inc
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