# STC ST00062LA - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Safran Cabin Inc., United States - Description: Installation of galley modules and stowage units. - Applied: August 22, 1994 - Status date: July 18, 2025 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/3e/3d/3e3ddd98920b256b423b67a6315446960cbca344d80fe57909463cb734421501 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID139727576020260209200832.0001 - DRS record last changed: February 9, 2026 - Page: https://openairdocs.org/stc/ST00062LA ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 737-200 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) ## What the certificate says This is OCR from the scanned FAA certificate. OCR can misread letters and numbers. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00062LA This certificate issued to: Safran Cabin Inc. 7330 Lincoln Way Garden Grove, CA 92841 Part 25 of Title 14, Code of Federal Regulations Type Certificate Number: A16WE Original Product Make: The Boeing Company Description of Type Design Change: Model: 737-200 Series Installation of Galley Modules and Stowage Units in accordance with FAA Approved Driessen Aircraft Interior Systems Master Drawing List MDL-101001, Revision "NC" dated January 9, 1995, or later FAA approved revisions. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated, unless it is found by the installer that the interrelationship between this change, and any of those previously approved modifications will introduce no adverse effect upon the aircraft's airworthiness. Note: The components installed by the STC have been demonstrated to meet the Heat Release Requirements (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: 08/22/1994 Date Reissued: 07/17/2014 03/15/2023 07/18/2025 Date of Issuance: 03/29/1995 Date Amended: see continuation sheet for additional dates By Direction of the Administrator signature: BroolG.Chwth Title: ODA Administrator, ODA-606394-NM United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: ST00062LA Effective Date: 07/18/2025 Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number. _ To (Name and address of transferee): Date of transfer. Signature of grantor. The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STO hofder. ## Every issue (3) - July 18, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/3e/3d/3e3ddd98920b256b423b67a6315446960cbca344d80fe57909463cb734421501) - March 15, 2023: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/40/44/40447aa58fc7411351a04bb4f732312dadd1e432215f0dfb92bb9fae1a147bc6) - July 17, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/e4/c7/e4c75b7c38f011f99baf4b90c8f48992702ffb0fa331021f7a97ba523c86f9c9) --- 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.