# STC SA2817WE-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: United Airlines Inc, United States - Description: Two additional serving cart tie down fittings are installed at Fus. Sta. 1289.0, Butt Line 86.20 left and right. Two cart tie down fittings are relocated from Fus. Sta. 816.00 to Sta. 821.75, Butt Line 86.20 left and right. Installations in accordance with DAS-1-WE United Air Lines Drawing List 2817 dated October 1, 1974 or later FAA approved revision. - Applied: October 1, 1974 - Status date: November 30, 2011 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A22WE](https://openairdocs.org/tcds/A22WE) - Certificate PDF: https://openairdocs.org/files/sha256/79/fd/79fdd244745fe20bf40900ce1e59af7f3e61f3e87ede0eb25de7c92d11519c8b - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/6FB2A09D8546FF4086257996005CC99A.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2817WE-D ## ADs that name it (0) None. ## Approved models (2) - The Boeing Company DC-10-10 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE)) - The Boeing Company DC-10-30 ([TCDS A22WE](https://openairdocs.org/tcds/A22WE)) ## 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 Regulations. (See Type Certificate Data Sheet A22WE for special conditions.) A22WE Boeing DC-10-10, DC-10-30 Description of Type Design Change: Two additional serving cart tie down fittings are installed at Fus. Sta. 1289.0, Butt Line 86.20 left and right. Two cart tie down fittings are relocated from Fus. Sta. 816.00 to Sta. 821.75, Butt Line 86.20 left and right. Installations in accordance with DAS-1-WE United Air Lines Drawing List 2817 dated October 1, 1974 or later FAA approved revision. Limitations and Conditions: This approval should not be incorporated in any aircraft of this specific model on which other approved modifications are incorporated, unless it is determined that the interrelationship between this change and any of those other previously incorporated approved modifications will not introduce any adverse effect upon the airworthiness of the 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. 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: October 1, 1974 Date of issuance: October 1, 1974 Date reissued: November 30, 2011 Date amended: April 18, 1984 ( 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/sha256/79/fd/79fdd244745fe20bf40900ce1e59af7f3e61f3e87ede0eb25de7c92d11519c8b) --- 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.