# STC SA2483NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States - Description: Installation of Cabin Divider P/N 13290, with or without Header Assembly P/N 13295. - Applied: March 22, 1985 - Status date: July 17, 2014 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) - Certificate PDF: https://openairdocs.org/files/sha256/6a/5c/6a5cf718fa3a991b41802713b7390fd4497dafa5f5a791698e9a12d538a41777 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/998F340D8911B4E786257D9B00718E61.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2483NM ## ADs that name it (0) None. ## Approved models (2) - The Boeing Company DC-9-51 ([TCDS A6WE](https://openairdocs.org/tcds/A6WE)) - The Boeing Company DC-9-81 (MD-81) ([TCDS A6WE](https://openairdocs.org/tcds/A6WE)) ## 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 certificate has been reissued to replace the original certificate reported as lost. This Certificate issued to Driessen Aircraft Interior Systems, Inc. DBA: Zodiac Galleys USA Inc. 17311 Nichols Lane Huntington Beach, California 92647 Part 4b of the Civil Air Regulations. (For Certification Basis See T.C. Data Sheet A6WE) Original Product Type Certificate Number : A6WE The Boeing Company DC-9-51 and DC-91-81 Description of Type Design Changes: Installation of Cabin Divider Part Number 13290, With or Without Header Assembly Part Number 13295, in accordance with FAA Approved Stowe Corporation Drawing List 13283, Revision “C”, dated March 26, 1985, or later FAA approved revision. Limitations and Conditions: The approval of this change in type design applies to the aftermentioned models only. This approval should not be extended to other aircraft models 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 introduce no adverse effect upon the airworthiness of the aircraft. This determination should include consideration of significant changes in weight distribution, such as an increase in the fixed disposable weight in the fuselage. 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. Date of application : March 22, 1985 Date of issuance : April 8, 1985 Date reissued: May 19, 1987; October 30, 1989; May 24, 1996; March 27, 1998; April 9, 2003; July 17, 2014 Date amended : May 2, 1985 (Signature) Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Title) NOTE: **DO NOT DELETE THIS PAGE.** **DO NOT ADD ANY DATA TO THIS PAGE.** **THIS PAGE IS FOR PAGE NUMBERING PURPOSES, PLEASE DISCARD PRINTED COPY.** ## Every issue (1) - July 17, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6a/5c/6a5cf718fa3a991b41802713b7390fd4497dafa5f5a791698e9a12d538a41777) --- 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.