# STC ST04492AT - Type: Supplemental type certificate - Status: Current, Reissued - Holder: ZIM Aircraft Cabin Solutions LLC - Description: Cabin Interior Reconfiguration in a Boeing 737-900/900ER Series aircraft - Status date: February 29, 2024 - Data sheets: A16WE, A16WE - Certificate PDF: https://openairdocs.org/files/sha256/03/a7/03a7cac54a34b079d4421a8171616ea9ef8c8921f657e9ac0e0ac58037144373 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID143047057720240320143315.0001 - Page: https://openairdocs.org/stc/ST04492AT ## ADs that name it None. ## Approved models (2) - 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. 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: ST04492AT ZIM Aircraft Cabin Solutions, LLC 8010 Piedmont Triad Parkway Greensboro, NC 27409 25 Federal Aviation Regulations A16WE Boeing 737-900/-900ER Series Cabin Interior Reconfiguration in a Boeing 737-900/900ER Series aircraft in accordance with HAECO Cabin Solutions Master Data List 22T003L001, Revision A, dated 28 Jul 2023, or later FAA approved revision. HAECO Cabin Solutions Instructions for Continued Airworthiness 22T003R009, Revision 01, dated 18 Aug 2023, or later FAA accepted revision is a required part of this STC. (Limitations and Conditions continued on page 3) December 5, 2022 February 29, 2024 July 28, 2023 David Pikett ODA Administrator ODA-100214-CE 4 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: ST04492AT 4 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: ST04492AT Date Reissued: February 29, 2024 (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 determined by the installer that the interrelationship between this change and any of those 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. 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 737-900/-900ER Series aircraft is as follows: a. The type certification basis for Boeing 737-900/-900ER Series 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, 05 Dec 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: (Certification Basis continued on next page) 3 4 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: ST04492AT Date Reissued: February 29, 2024 (Certification Basis continued) Regulations at the latest amendment 25-0 through 25-146: 25.1, 25.23(b)(2), 25.29, 25.301, 25.303, 25.305(a)(b), 25.561(a)(b)(3)(c), 25.562(a)(b)(c)(1)(2)(3)(4)(5)(6)(7)(8), 25.601, 25.603, 25.605(a), 25.609, 25.619, 25.625, 25.785(a)(b)(c)(d)(f)(1)(3)(i)(j)(k), 25.789(a), 25.791, 25.803, 25.811(b)(c)(d), 25.815, 25.853(a)(c)(d)(e), 25.1529, 25.1541(a)(1)(b). Regulations at an intermediate amendment: None. Regulations at the amendment level in TCDS A16WE: 25.307(a)(d), 25.611, 25.613(a)(b), 25.787(a)(b), 25.812(e), 25.813(a)(b)(c)(d)(f), 25.853(a)(c), 25.1301. 14 CFR Part 26 Regulations Based on 14 CFR 21.101(g), applicable provisions of 14 CFR part 26 are included in the certification basis. For any future 14 CFR part 26 amendment, 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 regulations (Amdt 26-0 through 26-7): 26.11(c). -----------------------------------------------------END------------------------------------------------------ 4 4 ## Every issue (2) - February 29, 2024: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/03/a7/03a7cac54a34b079d4421a8171616ea9ef8c8921f657e9ac0e0ac58037144373) - July 28, 2023: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/20/25/202590e8f36b9585e53aa670c459ae151c27d212fb010aa863828e96cfca5b94) --- 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.