What it approves
Install BRC Aviation dorsal fin, part number BRC 5302040-1.
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.
FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES N umber SA01410CH Reissued on February 5, 2019 to supersede the original STC, which has been lost or misplaced This certificate issued to
Part 23 of the Federal Aviation R egulations.
Original Product --Type Certificate N umber :
Install BRC Aviation Dorsal Fin, part number BRC 5302040-1 in accordance with Installation Instructions, Report 99-03005, Revision B, dated May 15, 2001, and Installation drawing BRC 5302020, Rev. C, dated October 15, 1999, or later FAA approved revisions.
1. Compatibility of this design change with previously approved modifications must be determined by the installer.
2. The Instructions for Installation, Report 99-03005 does not supersede the FAA Approved Weight and Balance Documentation and/or the FAA Approved Loading Documentation for this airplane. The FAA Approved Documentation referenced herein will take precedence if there is a conflict with any of the provisions of these Installation Instructions Report 99-03005.
3. 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
BRC Aviation 100 McKinley Dr. Unit 4A Camden, OH 45311 A16EA M ake : Tiger Aircraft LLC (American General) M odel : AA-5; AA-5A; AA-5B; AG-5B Date of app lication : May 15, 1999
Date of issuance : June 28, 2001
Date reissued : February 5, 2019
B y direction of the A dministrator Original Signed By:
Monica L. Nemecek
(Signature) Monica L. Nemecek, Manager Airframe & Administrative Services Section Chicago ACO Branch
(Title)
FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES
Number
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.