# STC SA2307WE - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Safran Cabin Inc., United States - Description: Installation of drink trolly 744000. (747-257B) - Applied: June 18, 1970 - Status date: July 18, 2025 - Product: Aircraft, Large Airplane - Certification basis: Part 25 - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) - Certificate PDF: https://openairdocs.org/files/sha256/52/53/52534a6b6368b434c31545fe4b11f6bd5d2ec71782dd06bf914403db0365f143 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID187422819620260112191439.0001 - DRS record last changed: January 12, 2026 - Page: https://openairdocs.org/stc/SA2307WE ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 747-200B Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE)) ## 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: SA2307WE 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: AZOWE Original Product Make: Boeing Description of Type Design Change: Model: B747-257B Modification of the Boeing 747-257B airplane by the installation of the Drink Trolley 744000 in accordance with the Sealed Drawing List No. 744-5. (Dash number suffixes of the above Drawing List refer to the change status) Limitations and Conditions: The approval of this change in type design applies basically to the Boeing 747-257B aircraft only. 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 previously approved modifications will introduce no adverse effect upon the airworthiness of that 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: 06/18/1970 Date Reissued: 08/03/1971 09/12/1983 11/12/1993 Date of Issuance: 02/05/1971 Date Amended: Title: ODA Administrator, ODA-606394-NM United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA2307WE Effective Date: 07/18/2025 EDERAL AVIATION Department of Transportation United States of America Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA2307WE Effective Date: 07/18/2025 Date Reissued: - cont.: 12/29/2005; 12/03/2018; 07/18/2025 ---END--- This certificate may be transferred or made available to third persons by licensing agreements in accordance with 14 CFR 21,47. ## Every issue (2) - July 18, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/52/53/52534a6b6368b434c31545fe4b11f6bd5d2ec71782dd06bf914403db0365f143) - December 29, 2005: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/22/91/22914447ac57fce332c2e1e3a02c8ef4891e285fde116a16ecf30d91031603e7) --- 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.