STC SA01215SE
FAA DRS lists SA01215SE as Current · Issued, held by Micro AeroDynamics Inc, for Cessna Aircraft F337E, Cessna Aircraft F337F, and Cessna Aircraft F337G, and 25 more aircraft configurations. Recorded change: Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers. Snapshot dated June 30, 2026.
Recorded modification
What the FAA record covers
Installation of vortex generators on the leading edge of the upper side of the wing on the underside of the horizontal stabilizer, and on both vertical stabilizers.
SA01215SE 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 F337E, Cessna Aircraft F337F, and Cessna Aircraft F337G, and 25 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Buyer checks
Confirm before sourcing
- 01Does it cover the exact Cessna Aircraft F337E and Cessna Aircraft F337F, and 26 more aircraft configurations model, serial range, and configuration?
- 02Which configuration, loads, materials, inspections, and damage limits apply?
- 03Who can legally supply the design data, kit, instructions, and ICAs?
- 04What parts, labor, conformity, and return-to-service work are excluded?
Related aircraft structures STCs
Installation of Hoskins Supplemental Model A or B High Intensity Wing Tip Lights, Model C Tail Light, with or without Model 1 or 2 High Intensity Fuselage Lights.
FAA holder: BF Goodrich Aerospace
Installation of either the tail safe support angles or a stub spar at the 3% chord station on the root rib of horizontal stabilizer.
FAA holder: D'Shannon Products Ltd.
Installation of either the Tail Safe support angles or a Stub Spar at the 3% chord station on the root rib of the horizontal stabilizer per Smith Speed Conversions Drawing List No. 1006 with an FAA approved date of May 8, 1981, or later.
FAA holder: D'Shannon Products Ltd.
Installation of three (3) fuselage optical window assemblies to support atmospheric research and meteorological observations in accordance with National Center for Atmospheric Research Optical Window Project Drawing List DL-100-09, Revision A, dated May 26, 2010 or later FAA approved revision. This installation is complemented by STC No. ST03056AT that provides the fuselage view port locations for the optical window assemblies.
FAA holder: National Science Foundation