STC SA02249SE

Number SA02249SE

This certificate, issued to CarpenterDev, LLC 21012 NE 36th St Sammamish, WA 98074

Part * of the * Regulations.

Original ProductType Certificate Number: * See attached Federal Aviation Administration (FAA) Make: Approved Model List (AML) SA02249SE for approved Model: aircraft models and applicable airworthiness regulations

Description of the Type Design Change: Installation of a silicone rubber wingtip device intended as a provision for mounting battery powered devices such as strobes or air temperature sensor in accordance with CarpenterDev Installation Instructions 10000, Revision 002, dated May 12, 2012, and Installation Guide CDEV-002, dated October 22, 2012, or later Federal Aviation Administration (FAA) approved revisions .

Fabrication controlled by CarpenterDev Drawing Part Number 10001, Revision 04, Sheets 1 and 2, dated May 12, 2012, or later FAA-approved revision. Maintained in accordance with CarpenterDev Instructions for Continued Airworthiness (ICA) CDEV-003 or later FAA-accepted revision.

Limitations and Conditions: Approval of this change in type design applies to the aircraft listed on AML SA02249SE only. 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 relationship between this change and other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate, the AML, Installation Instructions, Installation Guide, and ICA must be maintained as part of the permanent records for the modified aircraft.

Date of application: March 9, 2012 Date reissued: June 10, 2013 Date of issuance: December 5, 2012 Date amended: September 18, 2013

(Signature)

Manager, Seattle Aircraft Certification Office (Title)

Number SA02249SE

CarpenterDev, LLC Issued: December 5, 2012 Reissued: June 10, 2013 Amended: September 18, 2013

The equipment listed in the Accepted Equipment List (AEL), document CDEV-013, Rev. 001, dated August 21, 2013, or later FAA-accepted AEL, has been found acceptable for installation in this application.

Equipment providing flight guidance information including attitude, altitude, heading, navigation, angle of attack, or speed information cannot be installed without separate FAA approval.

It is the responsibility of the pilot-in-command to ensure that equipment installed per this STC does not interfere with the proper operation of any required aircraft systems.

The certification basis for this modification is based upon Part 3 of Civil Air Regulations as listed in AML SA02249SE.

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.

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