# STC ST04500CH - Type: Supplemental type certificate - Status: Current, Issued - Holder: GoAeroMx LLC, United States - Description: Installation of ADS-B OUT Global Positioning Satellite System (GPSS)/Space-Based Augmentation System (SBAS) & ADS-B IN Flight Information Services-Broadcast (FIS-B) system in accordance with GoAeroMx, LLC Master Data List Doc. No. 767-MDL-00001 Revision B, or later FAA-approved revisions. - Applied: July 2, 2019 - Status date: January 8, 2021 - Product: Aircraft - Certification basis: Part 21, Part 25, Part 26 - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) - Certificate PDF: https://openairdocs.org/files/sha256/79/b5/79b524786350153dd26f3b54eae01fb013d6433a893ac3b9be6392334ea3d3de - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/3CB338C4D113BD44862586620059AE55.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST04500CH ## ADs that name it (0) None. ## Approved models (3) - The Boeing Company 767-200 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM)) - The Boeing Company 767-300 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM)) - The Boeing Company 767-300F Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM)) ## 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. Part 25 of the Federal Aviation Regulations. (See Page 2 of 2 complete certification basis) Installation of ADS-B OUT Global Positioning Satellite System (GPSS)/Space-Based Augmentation System (SBAS) & ADS-B IN Flight Information Services-Broadcast (FIS-B) system in accordance with GoAeroMx, LLC Master Data List Doc. No. 767-MDL- 00001 Revision B, or later FAA-approved revisions. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. FAA Approved Airplane Flight Manual Supplement 767-AFMS-00001, Revision IR, approved 7 January, 2021, or later FAA approved revision or 767-AFMS-00002, Revision IR, approved 7 January, 2021, or later FAA approved revision, is required on board the modified aircraft. 3. FAA Accepted Instructions for Contuied Airworthiness, 767-ICA-00001, Revsion IR, dated 9 July 2020, or later FAA accepted revision is required for this modification. 4. If the holder agrees to permit another person to use this certificate to alter the product, the holder must give the other person written evidence of that permission. GoAeroMx, LLC 3815 North Mulford Rd. Rockford, IL 61114 A1NM Make : Boeing Model : 767-200 Series 767-300 Series 767-300F Series Date of application : July 2, 2019 Date of issuance : January 8, 2021 J Date reissued : (Signature) Steven L. Lardinois, Manager Systems Section Chicago ACO Branch (Title) FAA FORM 8110-2-1(10-69) PAGE 2 of 2 PAGES Number ST04500CH Date of issuance: Januarary 8, 2021 Certification Basis: Based on 14 CFR ยง 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the changed Boeing 767-200 Series, 767-300 Series, and 767-300F Series aircraft as described in this certificate is as follows: a. The type certification basis for Boeing 767-200 Series, 767-300 Series, and 767-300F Series airplane is shown on TCDS A1NM for parts not changed or not affected by this change. b. The certification basis for parts changed or affected by this change since the reference date of application, July 2, 2019 is as follows: Regulations at the latest amendment 25-0 through 25-125 581(b)(1) [25-23]; 601 [25-0]; 609(a)(b) [25-0]; 869(a)(1) [25-123]; 869(a)(3) [25-123]; 25.1301(a) [25-123]; 1301(b) [25-123]; 1307(c) [25-72]; 1309(a) [25-123]; 1309(b) [25-123]; 1309(c) [25-123]; 1309(d) [25-123]; 1309(e) [25-123]; 1309(f) [25-123]; 1321(e) [25-41]; 1322(a) [25-131]; 1322(e)(1) [25-131]; 1351(a) [25-72]; 1353(a) [25-123]; 1353(c) [25-123]; 1381(a) [25-72]; 1381(b) [25-72]; 1431(a) [25-113]; 1431(b) [25-113]; 1431(c) [25-113]; 1431(d) [25-113]; 1501(a) [25-42]; 1501(b) [25-42]; 1529 [25-54]; 1585(a)(1) [25-105]; 1585(a)(2) [25-105]; 1585(a)(3) [25-105]; 1713(a) [25-123]; 1713(c) [25-123] Regulations at the latest amendment 26-0 through 26-1 26.11(c) [26-0]; 26.47(b) [26-1]; 26.47(c) [26-1] This modification does not affect or create fatigue critical structure. -----END---- ## Every issue (1) - January 8, 2021: Issued, Current. [certificate](https://openairdocs.org/files/sha256/79/b5/79b524786350153dd26f3b54eae01fb013d6433a893ac3b9be6392334ea3d3de) --- 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.