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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

Other aircraft modifications34
Aircraft structures7
Engine and powerplant2
Electrical systems2
Fuel systems2
Aircraft performance1
Landing gear and brakes1
Flight controls1

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.

SA02194SEOther aircraft modifications

Installation 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.

FAA holder: Micro AeroDynamics Inc

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SA00743SEAircraft structures

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.

FAA holder: Micro AeroDynamics Inc

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SA00887SEOther aircraft modifications

Installation 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.

FAA holder: Micro AeroDynamics Inc

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SA01192SEOther aircraft modifications

Installation 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.

FAA holder: Micro AeroDynamics Inc

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SA01161SEOther aircraft modifications

Approval 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.

FAA holder: Micro AeroDynamics Inc

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SA01125SEOther aircraft modifications

Installation 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.

FAA holder: Micro AeroDynamics Inc

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