# STC SA7096NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States - Description: Installation of closet assemblies. - Applied: January 20, 1994 - Status date: July 17, 2014 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) - Certificate PDF: https://openairdocs.org/files/sha256/5a/42/5a420ebfb4c9a74111385b4459f49cab21eaf00c4680f321a1d28559c3b3cc3c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/A0843975D1510A6B86257D500055E24B.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA7096NM ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 767-200 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM)) ## 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. This Certificate issued to Driessen Aircraft Interior Systems, Inc. DBA: Zodiac Galleys USA Inc. 17311 Nichols Lane Huntington Beach, California 92647 P art *25 of the F ederal A viation R egulations . *Certification basis is set forth in Type Certificate Data Sheet A1NM Original Product Type Certificate N umber : M ake : M odel : A1NM The Boeing Company 767-200 Series Description of Type Design Changes : Installation of Closet Assemblies in accordance with FAA Approved Driessen Aircraft Interior Systems, Inc. Master Drawing List No. MDL-101474, Revision “A”, dated April 20, 1994, or later FAA approved revisions. Limitations and Conditions : The approval of this modification applies to the above noted airplane model series only. The installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previous approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. Note: The closet assemblies installed by this STC have been demonstrated to meet the heat release requirement (65/65) and the smoke emission requirement (200) of FAR 25.853 (a-1), amendment 25-66. A copy of this STC must be included in the permanent records of the modified aircraft. 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 : January 20, 1994 Date of issuance : June 13, 1994 Date reissued: July 17, 2014 B y direction of the A dministrator (Signature) Haifa Haj-Eid 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.** N umber (STC No.) ## Every issue (1) - July 17, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5a/42/5a420ebfb4c9a74111385b4459f49cab21eaf00c4680f321a1d28559c3b3cc3c) --- 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.