# STC SA00887SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Micro AeroDynamics Inc, United States - Description: 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. - Applied: December 21, 2000 - Status date: April 27, 2004 - Product: Aircraft, Single-Engine - Certification basis: Part 21 - Data sheets: [TCDS A16CE](https://openairdocs.org/tcds/A16CE), [TCDS A4CE](https://openairdocs.org/tcds/A4CE) - Certificate PDF: https://openairdocs.org/files/sha256/ba/da/bada01cefb246deaacd5bfa9180e13aa62fdca514dcc90e20e0c647b88cca281 - Approved model list and other attachments: [AML SA00887SE.pdf](https://openairdocs.org/files/sha256/73/e2/73e2210ea1a13d7316e309e7652e3e72ecfd90182a840082b6439c85fb454e16) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BCCF2D97E20D742A862578880064C6D6.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA00887SE ## ADs that name it (0) None. ## Approved models (33) - Cessna Aircraft Company 206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company 206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE)) - Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE)) - Cessna Aircraft Company P206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company P206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company T206H ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company T207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE)) - Cessna Aircraft Company T207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE)) - Cessna Aircraft Company TP206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TP206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206 ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206A ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206B ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206C ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206D ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206E ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206F ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) - Cessna Aircraft Company U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. Number SA00887SE This certificate, issued to Micro AeroDynamics, Inc. 4000 Airport Rd. Suite D Anacortes, WA 98221 Part * of the * Regulations. Original ProductType Certificate Number: * See attached FAA Approved Model List (AML) Make: No. SA00887SE for a list of approved airplane Model: models and applicable airworthiness regulations. Description of the Type Design Change: 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. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval should not be extended to other aircraft of this model 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. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy. 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. Date of application: December 21, 2000 Date reissued: Date of issuance: March 12, 2001 Date amended: April 27, 2004 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ### AML SA00887SE.pdf Micro AeroDynamics, Inc. FAA Approved Model List (AML) No. SA00887SE Installation of Micro AeroDynamics, Inc. Vortex Generator Kit Original Issue Date: March 12, 2001 Page 1 of 1 **FAA APPROVED** **INSTALLATION** **INSTRUCTIONS** **FAA APPROVED** **DRAWINGS AML** **REVISION DATE** **ITEM AIRCRAFT MAKE** **AIRPLANE MODEL TYPE CERT.** **NUMBER CERT. BASIS FOR** **ALTERATION NUMBER REV. DATE NUMBER REV. DATE** 1. Cessna 206, P206, P206A, P206B, P206C, P206D, P206E, U206, U206A, U206B, U206C, U206D, U206E, U206F, U206G, TP206A, TP206B, TP206C, TP206D, TP206E, TU206A, TU206B, TU206C, TU206D, TU206E, TU206F, TU206G, 206H, T206H A4CE CAR 3 FAR 23 MA2147 IR 1/24/01 MA2146 A 3/11/04 2. Cessna 207, T207, 207A, T207A A16CE FAR 23 MA2196 IR 3/11/04 MA2146 A 3/11/04 APPROVED__________________________________ Acting Manger, Seattle Aircraft Certification Office Amended: _4/27/2004_____________ Originally Signed By James Rehrl for ## Every issue (1) - April 27, 2004: Amended, Current. [certificate](https://openairdocs.org/files/sha256/ba/da/bada01cefb246deaacd5bfa9180e13aa62fdca514dcc90e20e0c647b88cca281), [AML SA00887SE.pdf](https://openairdocs.org/files/sha256/73/e2/73e2210ea1a13d7316e309e7652e3e72ecfd90182a840082b6439c85fb454e16) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.