# STC SA02370AK

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: Burl's Aircraft LLC, United States
- Description: Option (1) Installation of a replacement main tank fuel valve
- Applied: September 20, 2009
- Status date: May 13, 2010
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A-759](https://openairdocs.org/tcds/A-759), [TCDS A-761](https://openairdocs.org/tcds/A-761), [TCDS A-796](https://openairdocs.org/tcds/A-796)
- Certificate PDF: https://openairdocs.org/files/sha256/d7/57/d757b33366aa631780008c0c10886eec7a378f226a0894f183de96b92d4a3aac
- Approved model list and other attachments: [SA02370AK.pdf](https://openairdocs.org/files/sha256/9e/b3/9eb30599a023504d674f343dd950dd18016052b36638418b752e06a48850ef7a)
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D64807EF322CDA138625772F007AECAD.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA02370AK

## ADs that name it (0)

None.

## Approved models (16)

- American Champion Aircraft Corp. 11AC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. 11BC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. 11CC ([TCDS A-796](https://openairdocs.org/tcds/A-796))
- American Champion Aircraft Corp. 7AC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7ACA ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7BCM (Army L-16A) ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7CCM (Army L-16B) ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7DC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. 7EC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. S11AC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. S11BC ([TCDS A-761](https://openairdocs.org/tcds/A-761))
- American Champion Aircraft Corp. S11CC ([TCDS A-796](https://openairdocs.org/tcds/A-796))
- American Champion Aircraft Corp. S7AC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. S7CCM ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. S7DC ([TCDS A-759](https://openairdocs.org/tcds/A-759))
- American Champion Aircraft Corp. S7EC ([TCDS A-759](https://openairdocs.org/tcds/A-759))

## 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 APPROVED MODEL LIST (AML) SA02370AK FOR Burl’s Aircraft LLC.

STC Issue date: April 23, 2010

**AIRPLANE MAKE**

**AIRPLANE MODEL SERIAL**

**NUMBERS T.C.**

No.

**CERT.**

**BASIS**

American Champion 7AC 7ACA S7AC 7BCM 7CCM S7CCM 7DC S7DC 7EC S7EC

All All All All All All All All All 1 to 999

A-759 CAR 4a American Champion 11AC S11AC 11BC S11BC

All All All All

A-761 CAR 4a

American Champion 11CC S11CC All All

**A-796 CAR 3**

FAA APPROVED:

Manager, Anchor age Aircraft Certification Office Federal Aviation Administration Anchorage, Alaska

Revision: Initial Release Date: April 23, 2010

### SA02370AK.pdf

United States of America Department of Transportation -- Federal Aviation Administration Supplemental Type Certificate

_____________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

_____________________________________________________________________________________________________________________________________ FAA FORM 8110-2(10-68) PAGE 1 of 3 PAGES T his certificate may be transferred in accordance with FAR 21.47.

Number SA02370AK

This certificate issued to Burls Aircraft, LLC P.O. Box 671487 Chugiak, Alaska 99576

certifies that the change in the type design for the following product with the limitations and conditions therefore as specified hereon meets the airworthiness requirements of * of the * Regulations

Original Product — Type Certificate Number:

Make:

Model:

Description of Type Design Change:

Option (1) Installation of a replacement main tank fuel valve in accordance with Instruction No. BAR-1-2403, Revision: Original Issue, dated February 01, 2010 or later FAA approved revision.

Option (2) Installation of a replacement auxiliary fuel tank shutoff valve in accordance with Instruction No. BAR-100-HD-06, Revision: Original Issue, dated February 01, 2010 or later FAA approved revision.

Limitations and Conditions:

1) The installer must determine whether this design change is compatible with previously approved modifications.

Limitations and Conditions (continued on page 3 of 3):

This certificate and the supporting data which is the basis for approval shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration.

Date of application: September 20, 2009 Date reissued: May 13, 2010 Date of issuance: April 23, 2010 Date amended:

By direction of the Administrator

_______________________________________________________ ( Signature) August A. Asay Manager, Anchorage Aircraft Certification Office _______________________________________________________ ( Title)

* Refer to FAA Approved Model List (AML) Number SA02370AK, dated April 23, 2010 or later FAA approved revision, for approved airplane makes and models, corresponding Type Certificate Numbers, and applicable airworthiness regulations.

United States of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet)

___________________________________________________________________________________________________________________________________ Any alteration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, or both.

___________________________________________________________________________________________________________________________________ FAA FORM 8110-2-1(10-69) PAGE 3 of 3 PAGES This certificate may be transferred in accordance with FAR 21.47.

Limitations and Conditions (continuation): ( SA02370AK)

2) For instructions for continued airworthiness when installed as a replacement main fuel tank valve, refer to Installation Instructions and Instructions for Continued Airworthiness of the BAR-1-2403 Replacement Fuel Valve in the Aeronca 7 & 11 Series Aeronca/Champion Airplanes, Instruction No. BAR-1-2403, Revision:

Original Issue, dated February 1, 2010, or later FAA accepted revision. For instructions for continued airworthiness when installed as an auxiliary tank valve, refer to Installation Instructions and Instructions for Continued Airworthiness for the BAR-100-HD-06 Installed as Auxiliary fuel valve (7 Series Champion) And Main/Aux fuel valve (11 Series Chief) Aeronca Airplanes, Instruction No. BAR-100-HD-06 Revision:

Original Issue, dated February 1, 2010, or later FAA accepted revision.

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.

************************************* E N D *****************************************

## Every issue (2)

- May 13, 2010: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d7/57/d757b33366aa631780008c0c10886eec7a378f226a0894f183de96b92d4a3aac), [SA02370AK.pdf](https://openairdocs.org/files/sha256/9e/b3/9eb30599a023504d674f343dd950dd18016052b36638418b752e06a48850ef7a)
- April 23, 2010: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/d7/57/d757b33366aa631780008c0c10886eec7a378f226a0894f183de96b92d4a3aac), [SA02370AK.pdf](https://openairdocs.org/files/sha256/27/99/2799c5de8e32cdf2749d1a642856ea2398fee7a1a6bc5d92f8569cbf3b804176)

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