STC SA03777NY

FAA Form 8110-2 (5/14) Page 1 of

Part of the

Signature

Title SA03777NY Beringer Aero S.A.S.

Aeropole 05130 Tallard FRANCE Federal Aviation Regulations.

1. Installation of RF-006(A) Main Wheel and RA-002(A) Nose Wheel with EA-003.3N Brake System in accordance with Beringer Dossier de Modification, DM-STC-010, revision 2, dated October 28, 2015 or later EASA approved revisions.

2. Beringer Aero Instructions for Continued Airworthiness, Maintenance and Overhaul Manual MM-STC-010, revision 2, dated October 28, 2015 or later EASA accepted revisions is required with this modification.

3. Beringer Aero Airplane Flight Manual Supplement, AFMS-STC-010, revision 0, dated October 20, 2015 or later EASA accepted revisions is required with this modification.

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

2. 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.

3. The main and nose wheel are from different size as well as the axles so the wheels/tires cannot be intermixed.

(Limitations and Conditions Continued on Page 3 of 3) Raymond H. Reinhardt Acting Manager New York Aircraft Certification Office Cirrus Design Corporation SR20 SR22 SR22T April 18, 2014 July 28, 2016 IMPORT A00009CH 3

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

To (Name and address of transferee)

From (Name and address of grantor)

3 SA03777NY

FAA Form 8110-2 (5/14) Page 3 of

3 Date of Issuance: July 28, 2016

4. Mandatory replacement time and/or inspection intervals are defined in the approved “Airworthiness Limitations” section of Beringer Aero Maintenance and Overhaul Manual document MM-STC-010, revision 2, dated October 28, 2015 or later EASA approved revision.

5. In accordance with FAA Chicago Aircraft Certification Office letter dated June 3, 2016, Beringer brake part number (P/N) EA-003.3N(B) is FAA-approved as an Alternative Method of Compliance (AMOC) to the requirements of paragraphs e(1), e(2), e(3), and e(5) of Airworthiness Directive (AD) 2006-21-03, applicable only to Cirrus Design Corporation Model SR20 Airplanes, serial numbers (S/Ns) 1005 through 1600 (Group 1) and S/Ns 1005 through 1592 (Group 3); and Model SR22 Airplanes, S/Ns 0002 through 1739 (Group 2) and S/Ns 0002 through 1727 (Group 4).

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