STC SA8031NM

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA8031NM This certificate issued to: The 195 Factory, LLC 550 Myrtle Field Road Perry, GA 31069 Part *3 of the Civil Air Regulations.

Original Product Type Certificate Number: A-790 Make: Cessna Aircraft Company Description of Type Design Change: Model: 190, 195 (LC-126A, B, C), 195A, 195B Installation of locking tail wheel mechanism on existing tail wheel strut in accordance with FAA approved Ray's Aircraft Service Inc.- Drawing List, Report No. 1, revision Original, dated July 29, 1993, or later FAA approved revision. FAA approved Airplane Flight Manual Supplement, dated September 9, 1994, or later FAA approved revision is required as part of this installation.

The approval of this modification apploes to the above-noted airplane model series only.

** See continued Limitations and Conditions on Continuation sheet 2 NOTES page

Date of Application: 09/03/1993 Date Reissued: 07/02/2008 07/28/2026 Date of Issuance: 09/26/1994 Date Amended:

Title: for Michael P. Linegang Manager, East Certification Branch Possession of this Supplemental Type permission acceptable to the FAA. (Ref. 14 CFR 21.120).

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA8031NM Effective Date: 07/28/2026

Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number. _ To (Name and address of transferee):

or propeller. The ST's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC holder.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA8031NM Effective Date: 07/28/2026 NOTES:

*See Aircraft Specification No. A-790 for complete Certification Basis Limitations and Conditions: Continued: This approval should not be extended to other specific airplanes of this model series on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously approved modifications will introduce no adverse effect upon the airworthiness of the aircraft.

This STC is not compatible with aircraft equipped with cross wind landing gear installation. 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.

--END -