What it approves
Installation of vortex generators on the wings and tail surfaces.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00759SE This certificate issued to: Micro AeroDynamics, Inc.
4000 Airport Rd., Suite D Anacortes, WA 98221 Part 29 of the Federal Aviation Regulations.
Original Product -Type Certificate Number: A 19SO Make: Piper Model: PA-44-180 and PA-44-180T Description of Type Design Change: Installation of vortex generators on the wings and tail surfaces, in accordance with Drawing Package MA2119, Revision IR, dated October 13, 1999, and Installation Manual MA2120, Revision IR, dated November 24, 1999, 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 model 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.
Date of Application: October 13, 1999 Date Reissued:
Date of Issuance: December 13, 1999 Date Amended:
FEDERAL AVIATION I direction of the Stdm riste (Signature)
TOMINIST RATION Acting Manager, Seattle Aircraft Certification Office (L'itle)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.