STC SA03372NY

Supplemental type certificate · Beringer Aero

Holder
Beringer Aero · France
Status
Current · Issued
Status date
February 25, 2014
Applied
February 22, 2013
Product
Aircraft · Small Airplane
Certification basis
Part 21, Part 23
Data sheet
TCDSA00009CH

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 6, 2025.

What it approves

Installation of RF-006(A) main wheel well and RA-002(A) nose wheel well with EA-003.4N(B) brake system

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may 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………………..

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 3

MakeModelData sheet
Cirrus Design CorporationSR20A00009CH
Cirrus Design CorporationSR22A00009CH
Cirrus Design CorporationSR22TA00009CH