STC SA3113WE

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number SA3113WE This certificate issued to: Thermal Aircraft Company Part 3 of the CiVil Air Engine Indud fye betiale Mitication basis. Regulalions, dated Nov. 1, 1949. *Refer to Type Certificate Data Sheet No. 3A13 for a Cessna Model: 182, 182A thru H, J thru N, P & Q, Description of Type Design Change: T182, R182, TR182 Installation of flap gap fairing in accordance with Thermal Aircraft Company Drawing No. 5 dated September 6, 1975.

Thermal Aircraft Company Drawings No. 2, 3, and 4 (September 6, 1975) contain production data for this assembly.

Limitations and Conditions: The approval of this change in type design applies basically to the above listed aircraft only. This approval should not be extended to other aircraft of these models on which other previously approved modifications are incorporated, unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of that aircraft.

Date of Application: September 6, 1975 Date Reissued:

Date of Issuance: December 15, 1975 Jale mended August 22, 1977; December 29, 1983 EDERAL AVIATION By Direction of the Administrator OMINIS Supervisor, Aircraft Modification Section ames A (Signature) ruge 47