# STC SA01033SE - Type: Supplemental type certificate - Status: Current, Issued - Holder: Micro AeroDynamics Inc - Description: 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. - Status date: January 8, 2002 - Data sheets: A13CE, A13CE, A13CE, A20CE, A26EU - Certificate PDF: https://openairdocs.org/files/sha256/da/c2/dac2cc87d223bdc94d6b4c751278e720a664316dfd01f9f6c2858b7e8fb09b93 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3B7C64745CD8A9E685256CC1007E0240.0001 - Page: https://openairdocs.org/stc/SA01033SE ## ADs that name it None. ## Approved models (5) - Reims Aviation S.A. F177RG (TCDS A26EU) - The Cessna Aircraft Company 177 (TCDS A13CE) - The Cessna Aircraft Company 177A (TCDS A13CE) - The Cessna Aircraft Company 177B (TCDS A13CE) - The Cessna Aircraft Company 177RG (TCDS A20CE) ## 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 SA01033SE This certificate, issued to Micro AeroDynamics, Inc. 4000 Airport Road, Suite D Anacortes, WA 98221 Part 23 of the Federal Aviation Regulations. Original ProductType Certificate Number: A13CE A20CE A26EU Make: Cessna Cessna Cessna Model: 177, 177A, 177B, 177RG, F177RG Description of the Type Design Change: Installation of vortex generators on the wings and tail surfaces of the above model aircraft 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 revision of either of these documents. NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy. Limitations and Conditions: Approval of this change in type design applies to the above aircraft 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 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. This certificate and the supporting data which is the ba sis for approval shall remain in effect until surrendered, suspended, revoked, or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: November 19, 2001 Date reissued: Date of issuance: January 8, 2002 Date amended: (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - January 8, 2002: Issued, Current. [certificate](https://openairdocs.org/files/sha256/da/c2/dac2cc87d223bdc94d6b4c751278e720a664316dfd01f9f6c2858b7e8fb09b93) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.