STC SA11115SC

Part 23 of the Federal Aviation Regulations.

Description of Type Design Change: Installation of a standby flap travel limiting system in accordance with Aircraft Structures International Corp., Master Data List, ASIC208-6000-01MDL, Revision D, released September 22, 2011, or later FAA approved revision. The aircraft is to be maintained per the “Instructions for Continued Airworthiness for Modification to Existing Standby Flap System for Cessna 208 & 208B”, ASIC Document Number ASIC-002ICA, Revision C released January 6 2012, or later FAA accepted revision. Airplane Flight Manual Supplement (AFMS) titled “Airplane Flight Manual Supplement for Standby Flap System Limit Switches Installed in Cessna Model 208 or 208B Aircraft”, Document Number ASIC208-6000-29, Revision IR, dated December 13, 2012, or later FAA approved revision is required.

Limitations and Conditions: The installer must determine whether this design change is compatible with previously approved modifications. 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.

Aircraft Structures International Corp.

Hangar 31, Enid Woodring Regional Airport Enid, OK 73701 A37CE Make : Cessna Model : 208 & 208B Date of application : February 12, 2009

Date of issuance : December 13, 2012

( Signature) S. Frances Cox Manager, Special Certification Office Southwest Region

( Title)

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

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

Number SA11115SC Date of Issuance: December 13, 2012

Certificate Basis: All regulations are at the amendment levels identified in Type Certificate Data Sheet (TCDS) A37CE except for the following regulations that have been complied with at a higher amendment level:

14 CFR 23.305(a)(b), Amendment 45 14 CFR 23.1309(d)(e)(f) Amendment 49

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