What it approves
Installation of vortex generators on the wings, engine nacelle, horizontal tail surfaces, and leading edge of the rudder 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 SA01912SE 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: 3A16 Make: Hawker Beechcraft Model: G58, 58, 58A
Description of the Type Design Change: Installation of vortex generators on the wings, engine nacelle, horizontal tail surfaces, and leading edge of the rudder of the above model aircraft in accordance with Drawing Package, MA2226, Rev. IR, dated September 17, 2008, and Installation Manual, MA2227, Rev. IR, dated October 2, 2008, or later FAA-approved revisions to 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.
Date of application: September 18, 2008 Date reissued:
Date of issuance: October 16, 2008 Date amended:
(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.