# STC SA03861NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Beringer Aero, France
- Description: Installation of Main Wheels and Brake System
- Applied: June 3, 2015
- Status date: January 31, 2017
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A67EU](https://openairdocs.org/tcds/A67EU)
- Certificate PDF: https://openairdocs.org/files/sha256/a2/28/a228d1756bf09f29496d5f59b7145f30b0df3eb45ae026cae8e3a73c282de54f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/AE1958A6B132FC36862580CE0074E076.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA03861NY

## ADs that name it (0)

None.

## Approved models (5)

- Extra Flugzeugproduktions- und Vertriebs- GmbH EA 300/LC ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300 ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300/200 ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300L ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))
- Extra Flugzeugproduktions- und Vertriebs- GmbH EA-300S ([TCDS A67EU](https://openairdocs.org/tcds/A67EU))

## 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 (5/14) Page 1 of

Part of the

Signature

Title SA03861NY Beringer Aero S.A.S.

Aeropole 05130 Tallard France Federal Aviation Regulations.

1. Installation of Main Wheels and Brake System in accordance with Beringer Dossier de Modification, DM-STC-012, revision 4, dated August 3, 2016 or later EASA approved revisions.

2. Beringer Aero Instructions for Continued Airworthiness, Maintenance and Overhaul Manual MM-STC-012, revision 2, dated September 14, 2015 or later EASA accepted revisions is required with this modification.

1. Mandatory replacement time and/or inspection intervals are defined in the approved “Airworthiness Limitations” section of Beringer Aero Maintainance and Overhaul Manual document MM-STC-012, revision 2, dated September 14, 2015 or later EASA approved revision.

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

3. If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission.

Gaetano Sciortino Manager New York Aircraft Certification Office Extra Flugzeugproduktions- und Vertriebs- GmbH EA 300, EA 300/S, EA 300/L, EA 300/200, EA 300/LC June 3, 2015 January 31, 2017 IMPORT A67EU 2

FAA Form 8110-2 (5/14) Page 2 of

To (Name and address of transferee)

From (Name and address of grantor)

2 SA03861NY

## Every issue (1)

- January 31, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/a2/28/a228d1756bf09f29496d5f59b7145f30b0df3eb45ae026cae8e3a73c282de54f)

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