What it approves
Installation of vortex generators on the wings, horizontal and vertical tail surfaces (all models), and an increase in maximum zero fuel weight (PA-34-200T and PZL M20 03 only).
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 SA01681SE 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: *See attached FAA Approved Model List (AML) Make: No. SA01681SE 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, horizontal and vertical tail surfaces (all models), and an increase in maximum zero fuel weight (PA-34-200T and PZL M20 03 only) in accordance with FAA-approved Micro AeroDynamics, Inc. Drawing Package MA2212, Revision A, dated August 14, 2006, and Installation Manual MA2213, Revision A, dated October 6, 2006, or later FAA-approved revisions to these documents.
NOTE: If more than five vortex generators are damaged or missing, the aircraft is not airworthy.
The increase in maximum zero fuel weight (PA-34-200T and PZL M20 03 only) is also applicable to installations done in accordance with Installation Manual MA2213, Revision IR dated May 15, 2006
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 and FAA-Approved Flight Manual Supplement MA2215 Revision IR dated October 25, 2006 (PA-34-200T and PZL M20 03 only) 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: March 17, 2006 Date reissued:
Date of issuance: June 16, 2006 Date amended: October 25, 2006
FAA FORM 8110-2(10-68) By direction of the Administrator Thomas E. Archer, II
(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.
Approved models · 4
Every issue · 1
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| October 25, 2006 | Amended, current | CertificateApproved model list |