STC SA03962AT

Number SA03962AT This certificate issued to:

Part 23 of the Federal Aviation Regulations.

Installation of Continental Motors, Inc. TSIO-550-N engine on SR22 aircraft previously modified by STC SA10588SC in accordance with Installation Instructions IMSR22T550N, Rev. ~, dated April 11, 2012, or later FAA approved revision. Type design data is contained in Master Drawing List Number B-500, Revision ~, dated April 12, 2012, or later FAA approved revision. Required airplane flight manual data is contained in AFM supplement number AFMSSR22T550N, Rev. ~, dated April 5, 2012 or later FAA approved revision. Required instructions for continued airworthiness are contained in Continental Motors, Inc. Aircraft Maintenance Manual Supplement Number AMMSSR22T550N.

1. Approval of this change in type design applies to the above model aircraft only.

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

This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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.

Continental Motors, Inc.

2039 South Broad Street Mobile, Alabama 36615 A00009CH Make: Cirrus Design Corporation Model: SR22

Date of Application: February 16, 2011

Date of Issuance: April 19, 2012

(Signature) Melvin D. Taylor Manager Small Aircraft Certification Office

(Title)

Number: SA03962AT

United States O Revision Original Issue f America Department of Transportation Federal Aviation Administration Supplemental Type Certificate

Number SA03962AT Date of Issuance: April 19, 2012

Limitations and Conditions: (Continued):

3. A copy of this Certificate and the FAA approved Flight Manual Supplement, AFMSSR22T550N, Revision. ~, dated 04/05/2012, or later FAA approved revision, must be maintained as part of the permanent records of the modified aircraft.

4. An oxygen system meeting the requirements of 14 CFR Part 23, Secs. 23.1441 through 23.1449 must be installed in conjunction with this STC.

Certification Basis: The type certification basis is as shown on TCDS A00009CH plus the equivalent level of safety to FAR 23. 1091(b)(4) number ACE-06-06.

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