What it approves
Installation of Cleveland Part No. 040-19900 Tail Wheel Assembly and 10 x 3.50 4 tire and tube. Installation.
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4546NM 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 Cleveland Part No. 040-19900 Tail Wheel Assembly and 10 x 3.50 - 4 tire and tube. Installation in accordance with Ray's Aircraft Service drawings 0342140-90, Revision NC dated November 1988, and R0342006-21, Revision NC dated October 12, 1988, or later FAA sealed revisions.
*See continued Limitations and Conditions on Continuation sheet 2 NOTES page
Date of Application: 12/15/1988 Date Reissued: 06/10/2008 07/28/2026 Date of Issuance: 08/08/1989 Date Amended:
Title: for Michael P. Linegang Manager, East Certification Branch holder.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA4546NM Effective Date: 07/28/2026
Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number. _ To (Name and address of transferee):
Possession of this Supplemental Typ Certificate (STC) document by persons other than the STC holder does not constitute rights to the design data nor to alter an aircraft, aircraft engine 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: SA4546NM Effective Date: 07/28/2026 NOTES:
Limitations and Conditions: Continued: This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. 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-.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.
Approved models · 4
Every issue · 2
DRS keeps each issue of an STC as its own record, with its own certificate and attachments.
| Date | Status | Files |
|---|---|---|
| July 28, 2026 | Reissued, current | Certificate |
| June 10, 2008 | Reissued, earlier issue | Certificate |