# STC ST09885AC - Type: Supplemental type certificate - Status: Current, Issued - Holder: Aircraft Systems and Manufacturing Inc, United States - Description: Installation of a Cabin Lighting Control Module - Applied: July 7, 2017 - Status date: January 9, 2018 - Product: Aircraft, Large Airplane - Certification basis: Part 15, Part 21, Part 25, Part 26 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/66/8a/668aae4ebbfdde3e1aae440bf7f8c91855c9b8653bcf59982b2ac90b287343a0 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6BEC41A0515C50BF8625821F004A80B5.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/ST09885AC ## ADs that name it (0) None. ## Approved models (1) - 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. FAA Form 8110-2 (5/14) Page 1 of Part of the Signature Title Aircraft Systems & Manufacturing, Inc. 104 Golden Oaks Drive Georgetown, TX 78628 3 ST09885AC Federal Aviation Regulations. 25 Boeing 737-800 Series Installation of a Cabin Lighting Control Module in accordance with the Aircraft Systems & Manufacturing, Inc. Top Drawing List, document number 5730-0001-00, Revision B, dated November 17, 2017, or later FAA approved revision. Instructions for Continued Airworthiness (ICA), ASM Inc., Document No. 5730-2170-00, Revision A, dated October 10, 2017, or later FAA accepted revision must be made available to the operator at the time of installation. 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 shall give the other person written evidence of that permission. (Limitations and Conditions continued on page 3 of 3) July 7, 2017 January 9, 2018 A16WE Jim Grigg Manager, Fort Worth ACO Branch Airworthiness & Compliance Division FAA Form 8110-2 (5/14) Page 2 of To (Name and address of transferee) From (Name and address of grantor) 3 ST09885AC FAA Form 8110-2 (5/14) Page 3 of Note: 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 certification basis for this installation is per Type Certificate Data Sheet A16WE, revision 58, dated March 8, 2017, and the following 14 CFR § 25 paragraphs for Amendment 25-1 through 25-144, and with exceptions as noted in the TCDS A16WE, revision 58. Regulations at amendments 25-0 through 25-77 14 CFR § 25.29a, 25.301, 25.303, 25.305, 25.307, 25.561, 25.601, 25.603, 25.605, 25.609, 25.619, 25.789, 25.1301, 25.1351, 25.1355, 25.1529, 25.1541 Regulations at an intermediate amendment 25-0 through 25-144 14 CFR § 25.869 Amdt 25-113 Regulations at the latest amendment 25-0 through 25-144 14 CFR § 25.611, 25.613, 25.899, 25.981, 25.1309, 25.1353, 25.1357, 25.1360, 15.1431 Regulations at amendments 26-0 through 26-4 14 CFR § 26.11(c) ---------------------------------------------------------------------------------END------------------------------------------------------------------------------------- ST09885AC ## Every issue (1) - January 9, 2018: Issued, Current. [certificate](https://openairdocs.org/files/sha256/66/8a/668aae4ebbfdde3e1aae440bf7f8c91855c9b8653bcf59982b2ac90b287343a0) --- 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.