# STC SA3133NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Safran Cabin Inc., United States - Description: Installation of Windscreen Stowage Unit. - Applied: November 27, 1985 - 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/sha256/80/03/8003337f2b6e648bbc4b510c0ef208a4b060c6edd8a3ba8b13706401cd22697d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/DRSDOCID142954457720260203145035.0001 - DRS record last changed: February 3, 2026 - Page: https://openairdocs.org/stc/SA3133NM ## ADs that name it (0) None. ## Approved models (2) - The Boeing Company 737-100 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) - 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: SA3133NM This certificate issued to: Safran Cabin Inc. 7330 Lincoln Way Garden Grove, CA 92841 Part 25 of Title 14, Code of Federal Regulations Original Product Type Certificate Number: AGWE Make: The Boeing Company Description of Type Design Change: Model: 737-100, -200 Series Installation of the Windscreen Stowage Unit in accordance with FAA Approved Stowe Corporation Date List DL-14766, N/C dated November 27, 1985, or later FAA approved revision. If the holder agrees to permit another person to use the certificate to alter the product, the holder shall give the other person written evidence of that permission. The installation should not be incorporated in any aircraft unless it is determined by the installer that the interrelationship between this change and any of those other previously approved configurations will not introduce any adverse effect upon the airworthiness of the aircraft. A copy of this STC must be included in the permanent records of each rotorcraft modified in accordance with this STC. Date of Application: 11/27/1985 Date Reissued: 05/19/1987 08/30/1989 05/24/1996 Date of Issuance: 02/18/1986 Date Amended: Title: ODA Administrator, ODA-606394-NM The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the STC older. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA3133NM Effective Date: 07/18/2025 Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number. The STC's supporting documentation (drawings, instructions, specifications, flight manual supplements, etc.) is the property of the ST older. United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA3133NM Effective Date: 07/18/2025 Date Reissued: - cont.: 03/27/1998; 04/09/2003; 05/23/2023; 07/17/2014; 03/15/2023; **07/18/2025 ---END---** ## Every issue (3) - July 18, 2025: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/80/03/8003337f2b6e648bbc4b510c0ef208a4b060c6edd8a3ba8b13706401cd22697d) - May 23, 2023: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/a3/a2/a3a2512f1a16d255cf6e64bc41ce27aee6f7b0eb07a82f0ba08e1585f881a270) - July 17, 2014: Reissued, Historical. [certificate](https://openairdocs.org/files/sha256/6f/5a/6f5a3769cb4b30bce2eacedb08e44b1de9fdd72cb47cc754a96480a239605354) --- 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.