# STC ST09823DS - Type: Supplemental type certificate - Status: Current, Reissued - Holder: United Airlines Inc, United States - Description: Interior Reconfiguration - Applied: January 18, 2019 - Status date: June 30, 2019 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A1NM](https://openairdocs.org/tcds/A1NM) - Certificate PDF: https://openairdocs.org/files/sha256/d9/95/d995ad63b39443918047fdba02e613f0f83989b2bf1d5c58150ad7e2bb205766 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/46CD3E339C980967862585CA00543035.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST09823DS ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 767-300 Series ([TCDS A1NM](https://openairdocs.org/tcds/A1NM)) ## 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. FAA Form 8110-2 (5/14) Page 1 of 3 Number: ST09823DS This certificate issued to: United Airlines 600 Jefferson St. Houston, TX 77002 Parts 25 & 26 of the Federal Aviation Regulations Original Product – Type Certificate Number: Make: The Boeing Company A1NM Model: 767-300 Series Description of Type Design Change: 767-300 Interior Reconfiguration in accordance with United Airlines Master Drawing List 2500DA15209 Revision ‘B’, dated June 29, 2019 or later FAA approved revision. Instructions for Continued Airworthiness, Document Number 2500R01520C Revision ‘-’, dated May 10, 2019, or later FAA accepted revision is required for this installation. No AFM Supplement or EWIS ICA is required for this modification. 1) The 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. 2) If the holder agrees to permit another person to use this certificate to alter a product, the holder must give the other person written evidence of that permission. Date of Application: January 18, 2019 Date Reissued: June 30, 2019 Date of Issuance: June 16, 2019 Date Amended: By Direction of the Administrator Signature Title Patrick Ashton, STC Administrator United Airlines Organization Designation Authorization FAA Form 8110-2 (5/14) Page 2 of 3 Transfer Endorsement Transfer the ownership of Supplemental Type Certificate Number: ST09823DS To (Name and address of transferee) From (Name and address of grantor) FAA Form 8110-2 (5/14) Page 3 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09823DS 3) Prior or concurrent installation of the following modifications is required with this STC (aircraft applicability is identified within the following documentation): - Boeing Service Bulletin 767-25-0570, Issue 01, dated May 28, 2019, or later FAA approved revision - Boeing Service Bulletin 767-33-0107, Issue 01, dated December 21, 2018, or later FAA approved revision - Boeing Service Bulletin 767-52-0102, Issue 02, dated June 28, 2019, or later FAA approved revision - Boeing Service Bulletin 767-53-0291, Issue 01, dated November 19, 2018, or later FAA approved revision - Boeing Service Bulletin 767-53-0292, Issue 02, dated January 31, 2019, or later FAA approved revision - Delta Engineering Corporation FAA STC ST03205NY, issued October 29, 2014, or later amendment Certification Basis: Based on 14 CFR § 21.115 and § 21.101, and the FAA policy for design changes that are not significant in FAA Order 8110.48, the certification basis for this modification is as follows: a. The type certification basis for parts not changed or not affected by the change is shown in TCDS A1NM. b. The certification basis for parts changed or affected by this modification since the reference application date January 18, 2019, is based upon the type certification basis shown in TCDS A1NM with the following exceptions. 14 CFR Part Amdt 14 CFR Part Amdt 25.613 25-72 25.851 25-74 25.785(h) 25-51 25.853 25-83 25.793 25-51 25.854 25-74 25.807 25-67 25.856 25-111 25.812 25-58 25.869 25-72 25.813(c) 25-76 25.981 25-125 c. The modification certification basis also includes Special Conditions Number 25 -369-SC, dated February 7, 2008. --END-- FAA Form 8110-2 (5/14) Page 4 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09823DS FAA Form 8110-2 (5/14) Page 5 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09823DS FAA Form 8110-2 (5/14) Page 6 of 3 United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: ST09823DS ## Every issue (2) - June 30, 2019: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d9/95/d995ad63b39443918047fdba02e613f0f83989b2bf1d5c58150ad7e2bb205766) - June 16, 2019: Issued, Historical. [certificate](https://openairdocs.org/files/sha256/8e/bf/8ebf87f937bff640ca49cb5222950ca07b757aebdf7cb29245d1bec8c38fb2bb) --- 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.