# STC SA02251NM

- Type: Supplemental type certificate
- Status: Historical, Issued
- Holder: Gary L. Vogt (d/b/a AuCountry Aviation), United States
- Description: Installation of fiberglass cowling and improved engine baffles.
- Applied: December 19, 2006
- Status date: August 13, 2009
- 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/a3/36/a33619cbcf8b9c68b72230ec43628a238a5bb12d5fa748d9546ab5becfcb29e6
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/56341B01C56D2FB686257616006DC8D9.0001
- DRS record last changed: December 14, 2009
- Page: https://openairdocs.org/stc/SA02251NM

## ADs that name it (0)

None.

## Approved models (1)

- Tiger Aircraft LLC AA-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.

This Certificate issued to Gary L. Vogt (d/b/a AuCountry Aviation) 2945 Bell Road #150 Auburn, CA 95603 Part 23 of the Federal Aviation Regulations.

A16EA Tiger Aircraft LLC AA-5B Description of Type Design Change : Installation of fiberglass cowling and improved engine baffles in accordance with FAA approved AuCountry Aviation Master Drawing List 510000-MDL, Revision N/C, dated June 13, 2008 or later FAA-approved revision. See continuation sheet.

Limitations and Conditions : This installation must be done concurre ntly with Power Flow Systems Inc.

STC No. SA02448AT, installation of a tuned exhaus t system; and Air Mods, NW STC No. SA3326NM, installation of a Sensenich Propeller and Gulfstream Aerospace spinner assembly. The installation should not be incorporated in any airplane unless it is determined that the interrelationship between this installation and any previously approved confi guration will not introduce any adverse effect upon the airworthiness of the airplane.

Date of application : December 19, 2006

Date of issuance : August 13, 2009

( Signature) Manager, Propulsion Branch Los Angeles Aircraft Certification Office ( Title)

NOTE:

**DO NOT DELETE THIS PAGE.**

**DO NOT ADD ANY DATA TO THIS PAGE.**

**THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.**

Number SA02251NM

Revision Control:

Page No. 1 2 3 Rev. No. - - -

Description of Design Changes – continued:

The following AuCountry Aviation instructions for c ontinued airworthiness supplement is applicable to airplane modified in accordance with this STC:

AuCountry Aviation, Instructions for Continued Airworthiness, Document No. ICA-AA5B-01

Certification Basis for this modification: See TCDS A16EA.

It was determined that there is no acoustical change in accordance with § 21.93(b)(3)(iii) as a result of this modification.

Limitations and Conditions – continued:

The installer must determine whether this design change is compatible w ith previously approved modifications. The approval of this modification appli es to the above-noted airplane model series only. A copy of this STC must be included in the permanent r ecords of the modified airplane. If the holder agrees to permit another person to use this certificate to alter th e product, the holder shall give the other person written evidence of that permission.

A copy of this certificate must be maintained as part of the permanent records of the modified aircraft.

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## Every issue (1)

- August 13, 2009: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/a3/36/a33619cbcf8b9c68b72230ec43628a238a5bb12d5fa748d9546ab5becfcb29e6)

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