# STC SA2742NM-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: United Airlines Inc, United States - Description: Installation of a new galley system, waste drain system, and a seat mix revision. Approved for 737-291 and 737-2A1. - Applied: April 17, 1991 - Status date: November 30, 2011 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/f8/ce/f8ce712426e49461c17380784a1b163ee0d418b5340c51846c2c9794aa0b396d - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B2B9054370A261648625799E0071F355.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2742NM-D ## 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 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 United Air Lines, Inc. 600 Jefferson Street Houston, Texas 77002 Part 25 of the Federal Aviation RlOriginal Product Type Certificate Number : A16WE Boeing 737-291/2A1 Description of Type Design Change: Installs a new galley system, waste drain system, and a seat mix revision. This will be done according to United Air Lines DAS-1-WE Approved Master Drawing List No. 2742, dated May 22, 1991, or later FAA approved revisions. Limitations and Conditions: This approval should not be exte nded to other aircraft of this model on which other previously approved m odifications are incorporated unless it is determined by the installer that the interrelati onship between this change and any of those previously approved modifications will introdu ce no adverse effect upon the airworthiness of that aircraft. This determination should include consideration of signifi cant changes in weight distribution such as an increase in the fixed dis posable weight in the fuselage. If the holder agrees to permit another person to use this certif icate to alter the product, the holder shall give the other person written evidence of that permission. This certificate and the supporting data, which is the basis for approval, shall remain in effect until surrendered, suspended, revoked or a termination date is otherwise established by the Administrator of the Federal Aviation Administration. Date of application: April 17, 1991 Date of issuance: May 22, 1991 Date reissued: November 30, 2011 Date amended: August 22, 1991 ( 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.** ## Every issue (1) - November 30, 2011: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/f8/ce/f8ce712426e49461c17380784a1b163ee0d418b5340c51846c2c9794aa0b396d) --- 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.