# STC SA04009NY - Type: Supplemental type certificate - Status: Current, Issued - Holder: Aerospace Design & Compliance LLC, United States - Description: Installation of the ACSS Automatic Dependent Surveillance - Broadcast (ADS-B) Out System - Applied: February 6, 2018 - Status date: March 13, 2018 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25, Part 26 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/2c/3a/2c3ad86cdcb0cca39713943b475003e6c5c793bfa794ca22d92c38065cf1cc1f - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/07A530DDF760EA80862583010051E9C2.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA04009NY ## ADs that name it (0) None. ## Approved models (3) - The Boeing Company 737-600 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-700 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-800 Series ([TCDS A16WE](https://openairdocs.org/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. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. FAA Form 8110-2 (5/14) Page 1 of This certificate issued to: Part of the Signature Title ST04009NY Aerospace Design & Compliance, LLC. 750 Shipyard Drive, Suite 215 Wilmington, DE 19801 Federal Aviation Regulations.25 Installation of the ACSS Automatic Dependent Surveillance – Broadcast (ADS-B) Out System in accordance with Aerospace Design & Compliance, LLC. (1) Master Data List B738-MDL-0017, Rev IR, dated 3/13/2018, or later FAA approved revision. (2) Instructions for Continued Airworthiness (ICA) B738-ICA-0017, Rev IR, dated 03/02/2018, or later FAA accepted revision. The ICA and its contents must be incorporated into the operator's maintenance program. (3) Aircraft Flight Manual Supplement (AFMS) B737-AFM-0017, Rev IR, dated 3/13/2018, or later FAA approved revision. 1. The installer must determine whether this design change is compatible with previously approved modifications. 2. If the holder agrees to permit another person to use the certificate to alter the product, the holder must give the other person written evidence of that permission. 3. The existing Transponder System must be in compliance with Mode S, Mode S ELS, and Mode S EHS and the Transponder Control Panel must provide an ATC/XPDR Failure Indication. Administrator, ODA-834634-NE The Boeing Company 737-600/-700/-800 Series August 31, 2018 February 6, 2018 March 13, 2018 A16WE 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) Extent of Authority (if licensing agreement): 3 ST04009NY This certificat e may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21.47. FAA Form 8110-2 (5/14) Page 3 of 3 --- Date Amended: August 31, 2018 --- 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 Company model B737-600/-700/-800 Series is as follows: (1) The type certification basis for The Boeing Company model B737-600/-700/-800 Series airplane is shown on TCDS A16WE for parts not changed or not affected by the change. (2) The certification basis for parts changed or affected by the change since the reference date of application February 6, 2018, is based upon Part 25 as amended by Amendment 25-77 with the exception of those above amendment 25-77 listed below. Regulations at later amendment than 25-77: 14 CFR §25.305(a)(b) amdt 25-86 14 CFR §25.307(a) amdt 25-139 14 CFR §25.561(a)(b)(c) amdt 25-91 14 CFR §25.613(a)(b)(c) amdt 25-112 14 CFR §25.773(a)(2) amdt 25-144 14 CFR §25.869(a)(4) amdt 25-113 14 CFR §25.1316(b)(c)(4)(5)(6)(7) amdt 25-80 14 CFR §25.1317(c) amdt 25-122 14 CFR §25.1353(a)(b)(d)(1)(2)(3) amdt 25-113 3) Compliance has been demonstrated to 14 CFR § 26.11(c) amdt 26-0 and 14 CFR §26.47(c) amdt 26-1. ----------END---------- ST04009NY ## Every issue (1) - March 13, 2018: Issued, Current. [certificate](https://openairdocs.org/files/sha256/2c/3a/2c3ad86cdcb0cca39713943b475003e6c5c793bfa794ca22d92c38065cf1cc1f) --- 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.