What it approves
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.
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 SA01161SE This certificate, issued to Micro AeroDynamics, Inc.
4000 Airport Road, Suite D Anacortes, WA 98221
Part 3 of the Civil Air Regulations.
Original ProductType Certificate Number: A3SO Make: Piper Model: PA-32-260, PA-32-300, PA-32S-300, PA-32R-300
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 MA2174, Revision IR, dated September 6, 2002, and Installation Manual MA2175, Revision IR, dated November 21, 2002, 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.
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: October 31, 2002 Date reissued:
Date of issuance: January 8, 2003 Date amended:
(Signature) Acting Manager, Seattle Aircraft Certification Office (Title)
ADs that name this STC · 0
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