# STC SA01354CH

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: BRC Aviation, United States
- Description: Install BRC Aviation tailcone, part number BRC 5103011-1, -2, BRC 5103012, -2.
- Applied: November 5, 1999
- Status date: February 5, 2019
- Product: Aircraft, Single-Engine
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A16EA](https://openairdocs.org/tcds/A16EA)
- Certificate PDF: https://openairdocs.org/files/sha256/2f/c2/2fc2daf11b657cb59d21cef128d6c2ac799f9ae442c37abf0372459b35849323
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/35C5B2ED44117A358625843900698277.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA01354CH

## ADs that name it (0)

None.

## Approved models (4)

- Tiger Aircraft LLC AA-5 ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))
- Tiger Aircraft LLC AA-5A ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))
- Tiger Aircraft LLC AA-5B ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))
- Tiger Aircraft LLC AG-5B ([TCDS A16EA](https://openairdocs.org/tcds/A16EA))

## What the certificate says

Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record.

FAA FORM 8110-2(10-68) PAGE 1 of 2 PAGES N umber SA01354CH 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. (See Type Certificate Data Sheet Number A16EA for the complete certification basis)

Original Product --Type Certificate N umber :

Install BRC Aviation Tailcone, part numbers BRC 5103011-1, -2, BRC 5103012-1, -2 in accordance with Installation Instructions, Report 99-07005, Revision IR, dated November 15, 1999, and Installation drawing BRC 53 02500, Rev. C, dated January 15, 2001, 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 99-07005 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 Installation Instructions Report 99-07005.

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 application : November 15, 1999

Date of issuance : June 29, 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

## Every issue (1)

- February 5, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/2f/c2/2fc2daf11b657cb59d21cef128d6c2ac799f9ae442c37abf0372459b35849323)

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