# STC SA00023SE - Type: Supplemental type certificate - Status: Current, Amended - Holder: Trevor Burward-Hoy, United States - Description: Installation of modified control yoke and instrument panel. - Applied: December 27, 1993 - Status date: November 20, 2002 - Product: Aircraft, Small Airplane - Certification basis: Part 23 - Data sheets: [TCDS 3A24](https://openairdocs.org/tcds/3A24), [TCDS 5A6](https://openairdocs.org/tcds/5A6) - Certificate PDF: https://openairdocs.org/files/sha256/e2/4a/e24a87a5eac09269b9d92a4a881b8bb638fb64fa493e4c1579c88ede63b06365 - Approved model list and other attachments: [SA00023SE_AML.pdf](https://openairdocs.org/files/sha256/23/af/23af8dc523759fa7aa30b025d84b0cff734ae56d37b07e8d2d3ad616ec8b5f73) - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID197340880720231106211336.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA00023SE ## ADs that name it (0) None. ## Approved models (19) - The Cessna Aircraft Company 180 ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180A ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180B ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180C ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180D ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180E ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180F ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180G ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180H ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180J ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 180K ([TCDS 5A6](https://openairdocs.org/tcds/5A6)) - The Cessna Aircraft Company 185 ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company 185A ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company 185B ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company 185C ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company 185D ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company 185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company A185E ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) - The Cessna Aircraft Company A185F ([TCDS 3A24](https://openairdocs.org/tcds/3A24)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. S United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00023SE This certificate issued to: Trevor Burward-Hoy 10384 Dempster Avenue Cupertino, California 95014 Part * of the Federal Aviation Porgulations. Original Product Type Berlificate Number: * *See Attached FAA Approved Model List (AML) No. SA00023SE for list of approved Make: * aircraft models and applicable airworthiness regulations. Model: * Description of Type Design Change: Installation of modified control yoke and instrument panel in accordance with Avion Research International Master Drawing List C180-ML001, Revision 5, dated January 27, 1994, or later FAA approved revisions. NOTE: This installation includes provisions for installation of modified control yoke, radios and instruments in a new instrument panel. Any additions or changes to the original control yoke, radios or instruments will require separate FAA approval. The maximum weight of equipment installed in the panel should not exceed that of the suggested control yoke, instrument and radio layout shown in drawing 180-6011-1, Revision A, dated September 13, 1988. Limitations and Conditions: Approval of this change in type design applies to the aircraft models listed on AML No. SA00023SE only. This approval should not be extended to aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any previously approved modifications, including changes in type design will not introduce any adverse effect upon the airworthiness of the aircraft. Date of Application: December 27, 1993 Date Reissued: December 21, 2000 Date of Issuance: February 24, 1994 Dale unended: November 20, 2002 FEDERAL AVIATIO By Direction of the Administrator (Signature) TOMINSTRATO Manager, Airframe Branch. Los Angeles Aircraft Certification Office (Title) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA00023SE Limitations and Conditions: (Continued) A copy of this Certificate and FAA Approved Model List (AML) No. SA00023SE, dated November 20, 2002, or later FAA Approved revision, must be maintained as part of the permanent records of the modified 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 - ### SA00023SE_AML.pdf FAA APPROVED MODEL LIST (AML) NO. SA00023SE Avion Research Corporation for Installatio ·n of Instrument Panel in Cessna 180, 180A, 180B, 180C, 180D, 180E, 180F, 180G, 180H, 180J , 180K, 185, 185A, 185B, 185C, 185D, 185E, A185E, A185F Aircraft ISSUE DATE: Novemb er 20 2002 **ITEM** **AIRCRAFT MAKE** **AIRCRAFT MODEL** **ORIGINAL TYPE** **CERTIFICATE NUMBER** **CERTIFICATION** **BASIS FOR** **ALTERATION** **INSTALLATION** **INSTRUCTIONS** AFM **SUPPLEMENT** **NUMBER/DATE** AML **AMENDMENT DATE** **REPORT NO.** **REV.NO.** **AND DATE** I Cessna Cessna 180, 180A, 5A6 CAR Part 3 and Cl80-8001 Revision 3 Revision 3 NIA 180B, 180C, Amendments 180D, 180E, Listed On TCDS 180F, 180G, 5A6 180H, 180J, 180K 185, 185A, 3A24 CAR Part 3, FAR Cl80-8001 NIA 185B, 185C, Parts 23 and 21 185D, 185E, (Section 21.25) and A185E, Al85F Amendments Listed On TCDS 3A24 FAAAPPROVED:_/'2 a:t **R, AIRFRAME BRANCH LOS ANGELES AIRCRAFT CERTIFICATION OFC.** Page 1 of 1 ## Every issue (1) - November 20, 2002: Amended, Current. [certificate](https://openairdocs.org/files/sha256/e2/4a/e24a87a5eac09269b9d92a4a881b8bb638fb64fa493e4c1579c88ede63b06365), [SA00023SE_AML.pdf](https://openairdocs.org/files/sha256/23/af/23af8dc523759fa7aa30b025d84b0cff734ae56d37b07e8d2d3ad616ec8b5f73) --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.