STC SA10840SC

Supplemental Type Certificate Number SA10840SC

Part 23 of the Federal Aviation Regulations.

Original Product – Type Certificate Number: A37CE

Make: Cessna Model: 208 Series Description of Type Design Change:

Installation of wing jack pads on the Cessna 208 Series aircraft in accordance with Aircraft Structures International Corporation (ASIC) MasterData List ASIC-351MDL, Rev IR, dated December 6, 2007 or later FAA approved revision. The aircraft is to be maintained per the “Instructions for Continued Airworthiness for ASIC-351 MDL, Cessana 208 Series Auxiliary Jack Pad Installation”, ASIC Report number ASIC-208ICA, Rev IR, dated December 6, 2007, or later FAA accepted revision.

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.

Date of application: December 18, 2007 Date reissued:

Date of issuance: June 26, 2008 Date amended: January 8, 2014

Signature S. Frances Cox

Manager, Special Certification Office, Title Southwest Region

FAA Form 8110-2 (8/13) Page 1 Aircraft Structures International Corp.

Enid Woodring Regional Airport Hangar 31 RR 5, Box 41B Enid, OK 73701

SUPPLEMENTAL TYPE CERTIFICATE, FAA FORM 8110-2 (CONTINUED)

To (Name of transferee)

(Address of transferee)

(Number and street)

(City, State, and ZIP Code)

From (Name of grantor)

(Address of grantor)

(Number and street)

(City, State, and ZIP Code)

FAA Form 8110-2 (8/13) Page 2