FAA-listed STC holder
Micro AeroDynamics Inc STCs
The Jun 30, 2026 FAA DRS snapshot lists 50 selected supplemental type certificates with status Current under Micro AeroDynamics Inc. The records span 529 public aircraft directories and 8 modification categories. This is a research directory, not a claim that any specific kit or service is currently offered.
50
listed Current at snapshot
529
aircraft directories
8
modification categories
Jul 28, 2020
latest recorded revision
Modification mix
Aircraft represented
Cessna Aircraft 182178 STCsCessna Aircraft 182A157 STCsCessna Aircraft 182E157 STCsCessna Aircraft 172154 STCsCessna Aircraft 182B154 STCsCessna Aircraft 182C152 STCsCessna Aircraft 182F152 STCsCessna Aircraft 182D150 STCsCessna Aircraft 182G150 STCsCessna Aircraft 182K149 STCsCessna Aircraft 182H148 STCsCessna Aircraft 182J148 STCsCessna Aircraft 182P148 STCsCessna Aircraft 172K147 STCsCessna Aircraft 182L146 STCsCessna Aircraft 172D146 STCsCessna Aircraft 172E146 STCsCessna Aircraft 172M146 STCsCessna Aircraft 172I145 STCsCessna Aircraft 172N145 STCs
Recently revised records
Showing the 50 most recently revised records. Category directories provide the complete paginated discovery path.
50 displayed records.
Search every indexed record for this holder. The table below contains the recently revised records shown on this page.
| STC and modification | Aircraft / model / TC | Source status and dates | Holder and authority |
|---|---|---|---|
SA00024SEInstallation of vortex generators on the wing and verticle tail, and strakes on the nacelles.Aircraft structuresView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA4934NMInstallation of vortex generators on the wing and vertical stabilizer, and 5% take off gross weight increase.Aircraft structuresView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01439SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA02304SEInstallation of vortex generators on the wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00403SEInstallation of Vortex Generators on the wings.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00178SEInstallation of vortex generators on the wing and tail surfaces of the above model aircraft.Aircraft structuresView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA02226SEInstallation of vortex generators on the wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA02194SEInstallation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics Drawing Package MA2233, Revision IR, dated September 27, 2010, Installation Manual MA2234, Revision IR, dated September 6, 2011, and Instructions for Continued Airworthiness, MA0666, Rev A, or later FAA approved revisions. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01003SEAddition of performance data to allow reduced RPM rating on takeoff. Incorporation of this rating requires the prior or concurrent incorporation of STC SA00887SE.Aircraft performanceView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA02098SEInstallation of vortex generators on the wings and tail surfaces and strakes on the engine nacelles.Engine and powerplantView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01266SEInstallation of vortex generators on the wings, and tail surfaces of the above model aircraft.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00668SEInstallation of vortex generators on the wing leading edge and underside of the horizontal stabilizer.Aircraft structuresView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00530SEInstallation of vortex generators on leading edge of upper side of wing.Aircraft structuresView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA02002SEInstallation of vortex generators on the above model aircraft.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01227SEFarication of Vortex Generator Kit.Electrical systemsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00803SEInstallation of vortex generators on wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01912SEInstallation of vortex generators on the wings, engine nacelle, horizontal tail surfaces, and leading edge of the rudder of the above model aircraft.Engine and powerplantView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01911SEInstallation of vortex generators on the wings and horizontal tail surfaces of the above model aircraft .Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01869SEInstallation of vortex generators on the wings and horizontal and vertical tail surfaces of the above model aircraft.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA5131NMInstall vortex genertors on the wing and vertical tail surfaces and an increase in maximum takeoff weight, maximum zero fuel weight, and maximum ramp weight.Fuel systemsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01807SEInstallation of vortex generators on the wings and horizontal and vertical tail surfaces of the above model aircraft.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01681SEInstallation of vortex generators on the wings, horizontal and vertical tail surfaces (all models), and an increase in maximum zero fuel weight (PA-34-200T and PZL M20 03 only).Fuel systemsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01646SEInstallation of vortex generators on wings, horizontal and vertical tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01555SEInstallation of vortex generators on the wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00232SEInstallation of vortex generators on the wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01447SEInstallation 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.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00097SEInstallation of a vortex generator kit.Electrical systemsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00796SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00743SEInstallation 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.Aircraft structuresView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00887SEInstallation of vortex generators on the wings, tail surfaces, and vertical fin, in accordance with Micro AeroDynamics Drawing Package MA2146, Revision A, dated March 11, 2004, and installed in accordance with Installation Manual MA2147, Revision IR, dated January 25, 2001 (for the 206 series) or MA2196, Revision IR, dated March 11, 2004 (for the 207 series), or later FAA approved revisions.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SR01362SEInstallation of the support assembly for the ground handling wheel on the skid tube of the above model rotorcraft.Landing gear and brakesView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01299SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics , Inc. Drawing Package Document MA2191, Revision IR, dated September 17, 2003, and Installation Manual MA2192, Revision IR, dated October 27, 2003, or later FAA approved revision to either of these documents.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01215SEInstallation 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.Aircraft structuresView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01192SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2178, Revision IR, dated January 17 2003, and Installation Manual MA2179, Revision IR, dated February 24, 2003, or later FAA approved revision to either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00170SEInstallation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics drawings and installation instructions specified on the attached FAA AML No. SA00170SE dated November 12, 1997, or later FAA approved revision. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01161SEApproval of this change in type design applies to the airplane models listed above, only. This approval should not be extended to other aircraft on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this Certificate must be maintained as part of the permanent records for the modified aircraft. If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01137SEInstallation 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.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01125SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2171, Revision IR, dated July 17, 2002, and Installation Manual MA2172, Revision IR, dated September 6, 2002, or later FAA approved revision of either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01065SEInstallation of vortex generators on the wings and vertical tail surfaces of the above model aircraft per Drawing Package MA2081, Revision IR, dated January 15, 2002, and Installation Manual MA2082, Revision IR, dated February 13, 2002, or later FAA approved revision of either of these documents.NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01058SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2165, Revision IR, dated February 14, 2002, and Installation Manual MA2166, Revision IR, dated February 25, 2002, or later FAA approved revision of either of these documents.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA01033SEInstallation 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.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00795SEInstallation of vortex generators on the wings and tail surfaces of the above model aircraft in accordance with Drawing Package MA2131, Revision A, dated April 22, 2001, and Installation Manual MA2132, Revision A, dated April 22, 2001, or later FAA approved revision of either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00941SEInstallation of vortex generators on wings and tail surfaces in accordance with Drawing Package MA2156, Revision IR, dated April 18, 2001, and Installation Manual MA2157, Revision IR, dated July 3, 2001, or later FAA approved revision to either of these documents. If more than five vortex generators are damaged or missing, the aircraft is not airworthy.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00930SEInstallation of vortex generators on the wing and flap surfaces in accordance with Drawing Package MA2153, Revision IR, dated January 26, 2001, and Installation Manual MA2154, Revision IR, dated May 29, 2001, or later FAA approved revision of either of these documents.Flight controlsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00865SEInstallation of vortex generators on the wings, horizontal tail surfaces and vertical fin.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00849SEInstallation of vortex generators on wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00834SEInstallation of vortex generators on wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00831SEInstallation of vortex generators on wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00832SEInstallation of vortex generators on wings and tail surfaces.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |
SA00785SEInstallation of vortex generators on the wings and tail surfaces in accordance with Micro AeroDynamics Drawing Package MA2125, Revision IR, dated January 18, 2000, and Installation Manual MA2126, Revision IR, dated January 21, 2000, or later FAA approved revisions.Other aircraft modificationsView record |
| Current at cited snapshot Application: | FAA holder: Micro AeroDynamics Inc FAA authority record |