What it approves
Installation of vortex generators on the wings, and tail surfaces of the above model aircraft
What the certificate says
From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.
Number SA01266SE
This certificate, issued to: Micro AeroDynamics, Inc.
4000 Airport Road, Suite D Anacortes, WA 98221
Part 3 of the Civil Air Regulations.
Original Product Type Certificate Number: A3SO Make: Piper Model: PA-32R-301(SP), PA-32R-301(HP), PA-32R-301T, PA-32-301, PA-32-301T, PA-32-301FT, PA-32-301XTC
Description of the Type Design Change: Installation of vortex generators on the wings, and tail surfaces of the above model aircraft in accordance with Micro AeroDynamics Drawing Package MA2188, Revision A, dated October 26, 2009, and Installation Manual MA2189, Revision B, dated October 26, 2009, or later FAA approved revisions.
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 model only.
This approval should not be extended to other aircraft of this model series unless the installer determines that the relationship between this change and any other previously incorporated approved modifications 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: August 6, 2003 Date reissued:
Date of issuance: September 16, 2003 Date amended: November 4, 2009
(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.