STC SA01033SE
FAA DRS lists SA01033SE as Current · Issued, held by Micro AeroDynamics Inc, for Cessna Aircraft 177A, Cessna Aircraft 177B, and Cessna Aircraft 177, and 2 more aircraft configurations. Recorded change: Installation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2162, Revision IR, dated November 1, 2001, and Installation Manual MA2163, Revision IR, dated December 3, 2001, or later FAA approved revisions. 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
SA01033SE 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 177A, Cessna Aircraft 177B, and Cessna Aircraft 177, and 2 more aircraft configurations. Confirm the approved model list, serial effectivity, configuration, and certificate revision.
Related other aircraft modifications STCs
Installation of four (4) galleys.
FAA holder: American Airlines Inc
Installation of GoGo ATG-4 System.
FAA holder: Chippewa Aerospace Inc
Installation of an ARINCDirect XPLORE System.
FAA holder: StandardAero Business Aviation Services, LLC
FAA record reference
- STC number
- SA01033SE
- Product
- Aircraft · Single-Engine
- Country
- United States
- Application date
- November 19, 2001
- Revision date
- January 8, 2002
- CFR references
- Part 21, Part 23