# STC SA6091NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States - Description: Installation of Galleys, G1, G2, G4B - Applied: August 3, 1993 - Status date: July 17, 2014 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/6e/3e/6e3e5c142ae105e516328aea9f4dde35c2ac779f432712b01d4b7ba453f52424 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8639A92D07D0588786257D3C004DF9EE.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA6091NM ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 737-300 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. This Certificate issued to Driessen Aircraft Interior Systems, Inc. DBA: Zodiac Galleys USA Inc. 17311 Nichols Lane Huntington Beach, California 92647 Part 25 of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet A16WE. A16WE The Boeing Company 737-300 Description of Type Design Change: Installation of Galleys, G1, G2, G4B in accordance with FAA Approved Driessen Aircraft Interior Systems, Inc. Master Data List MDL-101462, Revision “C”, dated December 13, 1993, or later FAA approved revisions. Limitations and Conditions: The approval of this modification applies to the above noted airplane model series only. This installation should not be incorporated in any aircraft unless it is determined that the interrelationship between this installation and any previously approved configuration will not introduce any adverse effect upon the airworthiness of the aircraft. Note: All of the components installed by the STC meet the heat release requirement (65/65) and smoke emission requirement (200) of 14 CFR 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 : August 3, 1993 Date of issuance : December 17, 1993 Date reissued : July 17, 2014 (Signature) Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Title) Transfer the ownership of the Supplemental Type Certificate Number to (Name of transferee) (Address of transfer) (Number and street) (City, State, and Zip code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and Zip code) Extent of Authority (if licensing agreement): Signature of grantor (In ink): ## Every issue (1) - July 17, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6e/3e/6e3e5c142ae105e516328aea9f4dde35c2ac779f432712b01d4b7ba453f52424) --- 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.