STC SA01850WI

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

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Title Aircraft Structures International Corporation 620 N. Rock Road, Suite 230, #233 Derby, KS 73701 3 SA01850WI Federal Aviation Regulations.

23 Remove and replace fuselage-strut, main landing gear, wing and wing-flap track fitting in accordance with Master Data List (MDL), Document No. 11534000-300, Rev. B, dated 7/21/17, or later FAA Approved revision.

1. This installation should not be incorporated on any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce adverse effect upon the airworthiness of the airplane.

(See continuation sheet page 3) Textron Aviation 208, 208B November 10, 2015 August 28, 2017 A37CE Linda Dicken Associate ACO Manager, AIR-7K3 Wichita ACO Branch

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

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3 SA01850WI

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

3 Date Issued: August 28, 2017

Limitations and Conditions: (continued from page 1)

2. Model 208, s/n 20800001 and On, and Model 208B, s/n 208B00001 and On, with maximum takeoff and flight weights of 8750 pounds or less.

3. Instructions for Continued Airworthiness (ICA), Document No. 11534000-600, Rev. B, dated 7/21/17, or later FAA accepted revision, must be made available to the operator at the time of installation. The ICA does not change the Textron Aviation ICA limitations. It provides a procedure to reset the inspection requirements for the replacement fittings, thus zeroing the in service hours for the new fittings. Subsequent inspections for fittings installed per the MDL Document No. 11534000-300, Rev.

B, dated 7/21/17, or later FAA Approved revision, will be as defined in the Textron Aviation ICA limitations.

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