# STC ST04547AT - Type: Supplemental type certificate - Status: Current, Issued - Holder: Woven Electronics LLC - Description: Replacement of Various Existing LRU's with Rockwell Collins LRU's - Status date: August 25, 2022 - Data sheets: A16WE, A16WE, A16WE, A16WE, A16WE, A16WE - Certificate PDF: https://openairdocs.org/files/sha256/14/fc/14fc96c6c7e0b9f1ffcadf1051b553b8d1c0fd4879383a21e9fae55e8d0c549a - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/316379C0FC7B136F862588AD0049859F.0001 - Page: https://openairdocs.org/stc/ST04547AT ## ADs that name it None. ## Approved models (6) - The Boeing Company 737-600 Series (TCDS A16WE) - The Boeing Company 737-700 Series (TCDS A16WE) - The Boeing Company 737-700C Series (TCDS A16WE) - The Boeing Company 737-800 Series (TCDS A16WE) - The Boeing Company 737-900 Series (TCDS A16WE) - The Boeing Company 737-900ER 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. ST04547AT Woven Electronics, LLC 16000 Pines Blvd #824431 Pembroke Pines, FL 33082-9599 Part 25 Federal Aviation Regulations. A16WE The Boeing Company B737-600/700/700C/800/900/900ER Replacement of Various Existing LRU's with Rockwell Collins LRU's in accordance with Master Drawing List 2-240579-001, Revision IR, dated May 25, 2022 or later FAA approved revision. (See Continuation Sheet 3 of 4) February 15, 2022 August 25, 2022 4 ST04547AT 4 ST04547AT Limitations and Conditions (continued) 1. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is determine by the installer that the interrelationship between this change and any other previously approved modifications will produce no adverse effect upon the airworthiness of that airplane. 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 No. 2-240579-802, Rev IR, dated May 6, 2022 or later FAA approved revision must be made available to the operator at the time of installation. ST04547AT 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 Boeing 737 series aircraft is as follows: a. The type certification basis Boeing 737 aircraft is 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, February 15, 2022 is based upon Part 25 as amended by Amendment 25-146. 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 25-146 25.23(a), 25.301(a)(b), 25.303, 25.305(a), 25.561(c), 25.581(a)(b)(1), 25.601, 25.603 (b)(c), 25.609, 25.853(a), 25.863(a), 25.1351(a)(1), 25.1431(a)(c), 25.1529 Regulations at an intermediate amendment 25.1353(a)(b)(d) Amdt. 25-113 Regulations at the amendment level in TCDS A16WE 25.307(a), 25.611, 25.1301(a)(b)(c)(d), 25.1309(a)(b)(d), 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 demonstrate compliance with the applicable sections. As of the issuance date of this STC, compliance has been found for the following regulations: None --------- END -------- 4 4 ## Every issue (1) - August 25, 2022: Issued, Current. [certificate](https://openairdocs.org/files/sha256/14/fc/14fc96c6c7e0b9f1ffcadf1051b553b8d1c0fd4879383a21e9fae55e8d0c549a) --- 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.