# STC SA02423AK - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Dakota Mustang Inc, United States - Description: Relocation of Circuit Breakers and Switches to the Instrument Panel - Applied: March 13, 2013 - Status date: January 10, 2014 - Product: Aircraft, Small Airplane - Certification basis: Part 3, Part 21, Part 43 - Data sheets: [TCDS 1A2](https://openairdocs.org/tcds/1A2) - Certificate PDF: https://openairdocs.org/files/sha256/c0/20/c02021d73cc3fa29aafcd56c2ad2c743e10725369e7665bcf0329a1b163f7d78 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/820F932CFE6F308786257C60005A868D.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA02423AK ## ADs that name it (0) None. ## Approved models (1) - Piper Aircraft Inc. PA-18-150 ([TCDS 1A2](https://openairdocs.org/tcds/1A2)) ## What the certificate says Read from the PDF's text layer, without the form's printed wording; the layout is lost and the order can differ. The PDF is the record. This Certificate issued to Dakota Mustang, Inc. 1251 Pegasus Road Wahpeton, North Dakota 58075 Part 3 of the Civil Air Regulations. Original Product – Type Certificate Number: 1A2 Make: Piper Model: PA-18 “150” Description of Type Design Change: Relocation of Circuit Breakers and Switches to the Instrument Panel in accordance with Dan’s Aircraft Approved Specification #2007, dated 11/29/99, Installation of Rear Baggage Cargo Door in accordance with Dan’s Aircraft Approved Specification #2010, dated 11/29/99, Installation of Aluminum Floorboards in accordance with Dan’s Aircraft Approved Specification #2018, dated 11/29/99, Installation of a Long Upper Baggage Compartment in accordance with Dan’s Aircraft Approved Specification #2044, dated 03/15/00, and Installation of a Lower Extended Baggage Compartment in accordance with Dan’s Aircraft Approved Specification #2045, dated 03/15/00. Limitations and Conditions 1) Descriptive data about this design change cannot be used to duplicate other products. This approval is limited to only the installation made in Piper PA-18 “150” Serial No. 18-7809074. No additional modifications of this type are to be approved solely by reference to this STC. 2) Compatibility of this modification with other FAA approved modifications must be evaluated by the installer. 3) Aircraft Flight Manual Supplement Piper Model PA-18-150 N4122E, S/N: 18-7809074, Revision IR, dated December 20, 2013, or later FAA approved revision is a required part of this installation. 4) 14 CFR Part 43 is adequate to ensure continued airworthiness of this modification. 5) This STC does not permit manufacturing of parts for multiple installations. 6) This STC approves the electrical aspects for the relocation of the circuit breakers and switches to the instrument panel only. All other changes to the electrical system or installation of equipment must be separately approved. Date reissued: January 10, 2014 Date amended: (Signature) August A. Asay Manager, Anchorage Aircraft Certification Office (Title) Date of application: March 13, 2013 Date of issuance: December 20, 2013 FAA Form 8110-2-1(10-69) Page 2 of 2 ## Every issue (1) - January 10, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c0/20/c02021d73cc3fa29aafcd56c2ad2c743e10725369e7665bcf0329a1b163f7d78) --- 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.