# STC ST11386DS - Type: Supplemental type certificate - Status: Current, Issued - Holder: Aircraft Systems and Manufacturing Inc., United States - Description: Installation of USB Charging Hubs on the Flight Deck - Applied: June 30, 2023 - Status date: October 9, 2023 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/0a/42/0a42f676d9ed46acf5a394cd0667ebadcfc088d2e565c2a3304bc85701ae4066 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID145851810720231205221459.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST11386DS ## ADs that name it (0) None. ## Approved models (9) - 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 737-700C Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-8 ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-800 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-8200 ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-9 ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-900 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - The Boeing Company 737-900ER 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. FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 1 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST11386DS Aircraft Systems and Manufacturing, Inc. 1717 Universal City Boulevard Universal City, Texas 78148 Part 25 Title14 of the Code of Federal Regulations A16WE Boeing 737-600/-700/-700C/-800/-900/-900ER/-8/-9/ -8200 Installation of USB Charging Hubs on the Flight Deck in accordance with JANA Engineering Master Data List, Doc. No. 5775-0000-00, Rev IR, dated October 9, 2023, or later approved revision. The FAA Approved Airplane Flight Manual Supplement, Doc. No. 5775-2160-00, Rev IR, dated August 28, 2023, or later approved revision, must be attached to the Airplane Flight Manual when this STC is incorporated. The installer must determine whether this design change is compatible with previously approved modifications. 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. See continuation on Page 3 of 3. June 30, 2023 October 9, 2023 Robert H. Wilcox ODA Administrator, ODA-834704-SW 3 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page 2 of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST11386DS 3 FAA Form 8110-2 (11/20) SUPERSEDES PREVIOUS EDITION Page ___ of ___ United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST11386DS Limitations and Conditions continued: In addition to the basic aircraft maintenance manuals, the aircraft must be maintained in accordance with the Instructions for Continued Airworthiness (ICA) Document No. 5773-2170-00, Rev A, dated October 4, 2023, or later FAA accepted revision. Airworthiness Limitations inspections per 14 CFR Part 25, Appendix H are contained in Chapter 7 of the ICA. The FAA has reviewed the applicant's assessment showing that this modification does not impact the existing electrical wiring interconnection system instructions for continued airworthiness (EWIS ICA) and found that no additional EWIS ICA tasks are required. Certification Basis: The type certification basis for the Boeing 737-600/-700/-700C/-800/-900/-900ER/-8/-9/-8200 series aircraft for parts not changed or not affected by this change is shown on TCDS A16WE, Revision 73, dated March 15, 2023. The certification basis for parts changed or affected by this change since the reference date of STC application, 30-June-2023, is based upon Part 25 as amended through Amendment 25‐148 and Part 26 as amended through Amendment 26‐7. Based on 14 CFR Sections 21.115 and 21.101, and FAA policy for non‐significant changes in FAA Order 8110.48A, the certification basis for the aircraft to be modified by the STC design data are as follows: Regulations at the latest Amendment 25‐0 through 25‐146 used for this modification: 14 CFR § 25.29(b), 25.301(a)(b), 25.303, 25.305(a,b), 25.307(a), 25.561(a,b3), 25.601, 25.603(a,b), 25.605(a), 25.609(a), 25.611(a), 25.613(a,b,c), 25.625(a,b,c), 25.771(a)(e), 25.773(a), 25.777(a), 25.853 (a), 25.1301(a), 25.1307(c), 25.1309(a,b,d), 25.1351(a), 25.1353(a), 25.1355(a), 25.1357(a,c,e), 25.1360 (a,b), 25.1431(a,b,c,d), 25.1529, 25.1541, 25.1581(a,b,c), 25.1583(e), 25.1585(a) Regulations at the latest amendment 26‐0 through 26‐7 used for this modification: 14 CFR § 26.1, Amdt. 26-0; § 26.11(c), Amdt. 26-7 Regulations at an intermediate amendment: 25.869(a1,4) Amdt. 113 -END- ## Every issue (1) - October 9, 2023: Issued, Current. [certificate](https://openairdocs.org/files/sha256/0a/42/0a42f676d9ed46acf5a394cd0667ebadcfc088d2e565c2a3304bc85701ae4066) --- 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.