# STC ST04408AT - Type: Supplemental type certificate - Status: Current, Issued - Holder: Avionics Support Group Inc. - Description: Installation of Rockwell Collins TPR-901 Automatic Dependent Surveillance - Broadcast (ADS-B) Out Transponder(s) - Status date: October 4, 2017 - Data sheets: A16WE, A16WE, A16WE, A16WE - Certificate PDF: https://openairdocs.org/files/sha256/bc/92/bc9240b1e774545b7742192518043f218cd461e3f1a5218bdda69cd141c4cb72 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/224FFDBFD92039E3862581B00044AAC5.0001 - Page: https://openairdocs.org/stc/ST04408AT ## ADs that name it None. ## Approved models (4) - The Boeing Company 737-600 Series (TCDS A16WE) - The Boeing Company 737-700 Series (TCDS A16WE) - The Boeing Company 737-800 Series (TCDS A16WE) - The Boeing Company 737-900 Series (TCDS A16WE) ## 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 certifi cate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of t his Supplemental Type 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. FAA Form 8110-2 (5/14) Page 1 of 3 Number: ST04408AT This certificate issued to: Avionics Support Group, Inc. 13155 SW 132 Avenue Miami, FL 33186 Part 25 of the Federal Aviation Regulations. Original Product – Type Certificate Number: A16WE Make: Boeing Model: 737-600/-700/-800/-900 Series Description of Type Design Change: Installation of Rockwell Collins TP R-901 Automatic Dependent Surveillance - Broadcast (ADS -B) Out Transponder(s) in accordance with Master Data List (MDL) 216307-MDL, Rev. B, dated August 17, 2017, or later FAA approved revision. 1. The installer must determine whether this design change is compatible with previously approved modification. 2. 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. 3. Instructions for Continued Airworthiness (ICA) document 216307-ICA, Rev. A, dated May 19, 2017 or later FAA accepted revision must be made available to the operator at the time of installation. Date of Application: December 16, 2016 Date Reissued: Date of Issuance: October 04, 2017 Date Amended: Signature Title: (for) Christina M. Underwood AIR-7A0 Manager, Atlanta ACO Branch This certifi cate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of t his Supplemental Type 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. FAA Form 8110-2 (5/14) Page 2 of 3 Transfer the ownership of Supplemental Type Certificate Number: ST04408AT To (Name and address of transferee) From (Name and address of grantor) United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST04408AT Data of Issuance This certifi cate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. Possession of t his Supplemental Type 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. FAA Form 8110-2 (5/14) Page 3 of 3 Certification Basis: Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for the Boeing 737-600/-700/-800/-900 Series aircrafts is as follows: a. The type certification basis for the Boeing 737-600/-700/-800/-900 Series aircrafts are shown on TCDS A16WE for parts not changed or not affected by the change. b. The certification basis for parts changed or affected by the change since the reference date of application, December 16, 2016, is based upon part 25 as amended by Amendment 25-143. Based on 14 CFR 21.115 and 21.101, and the FAA policy for significant changes in FAA Order 8110.48, the certification basis for this modification was determined to be: Regulations at the latest amendment 25-0 through 25-143 § 25.29 § 25.771 § 25.773 § 25.777 § 25.1301(a) § 25.1307(c) § 25.1309 § 25.1322 § 25.1351(a) § 25.1353(a) § 25.1357(a) § 25.1360 § 25.1431(a)(c) § 25.1529 § 25.1541 § 25.1581 Regulations at an intermediate amendment None Regulations at the amendment level in TCDS A16WE None 14 CFR Part 26 Regulations Based on 14 CFR 21.101(g), applicable provision of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendments, the holder of this STC must demo nstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulation: **14 CFR 26.11 --------------------------END---------------------------** ## Every issue (1) - October 4, 2017: Issued, Current. [certificate](https://openairdocs.org/files/sha256/bc/92/bc9240b1e774545b7742192518043f218cd461e3f1a5218bdda69cd141c4cb72) --- From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.