# STC SA03372NY

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: Beringer Aero, France
- Description: Installation of RF-006(A) main wheel well and RA-002(A) nose wheel well with EA-003.4N(B) brake system
- Applied: February 22, 2013
- Status date: February 25, 2014
- Product: Aircraft, Small Airplane
- Certification basis: Part 21, Part 23
- Data sheets: [TCDS A00009CH](https://openairdocs.org/tcds/A00009CH)
- Certificate PDF: https://openairdocs.org/files/sha256/c9/64/c964b4b90fe27e1bb13ed48342ece101216407c5a4998e971f7d12e6122d513a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B19C4016F53D795886257D10004DB8A4.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA03372NY

## ADs that name it (0)

None.

## Approved models (3)

- Cirrus Design Corporation SR20 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH))
- Cirrus Design Corporation SR22 ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH))
- Cirrus Design Corporation SR22T ([TCDS A00009CH](https://openairdocs.org/tcds/A00009CH))

## 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.

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

This certificate issued to

Part 23 of the Federal Aviation R egulations.

Original Product -Type Certificat e N umber :

Description of Type Design Chang e:

1. Installation of RF-006(A) main wheel well and RA-002(A) nose wheel well with EA-003.4N(B) brake system in accordance with, EASA approved, Dossier De Modification, DM-STC-004, Revision 2, dated July 16, 2013, or later EASA approved revisions.

2. The following Beringer Aero document are required with this installation:

a. Aircraft is to be maintained in accordance with, EASA Approved, Maintenance and Overhaul Manual, MM-STC- 004, Revision 2, dated January 20, 2014, or later EASA accepted revisions.

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

Beringer Aero Aeropole 05130 Tallard France Cirrus Design Corportation M ake :

M odel:

A00009CH SR20, SR22, SR22T Date reissued:

B y direction of the A dministrator

(Signature) Gaetano Sciortino Manager New York Aircraft Certification Office

(Title)

Date of application : February 22, 2013

Date of issuance: February 25, 2014

FAA Form 8110-2-1(10-69) Page 3 of 3

N umber SA03372NY

Date of Issuance: February 25, 2014

Limitations and Conditions : (Continued)

2. If the holder agrees to permit another person to use the certification to alter a product, the holder must give the other per son written evidence of that permission.

3. 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-004, revision 2, dated January 20, 2014, or later EASA approved revision.

..……………END………………..

## Every issue (1)

- February 25, 2014: Issued, Current. [certificate](https://openairdocs.org/files/sha256/c9/64/c964b4b90fe27e1bb13ed48342ece101216407c5a4998e971f7d12e6122d513a)

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