# STC SA2700NM-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: United Airlines Inc, United States - Description: Cabin configuration changed to accommodate 40 first class and 230 coach passengers. Crew rest facility located forward of Door 2RH and closet located at Door 2LH removed. - Applied: September 5, 1984 - 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/sha256/69/66/6966b675ecaf06b9a3f804fd3ecd171e166aa4390e5fe69beb54551f097d6006 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/60F1BF0451EA720D8625799900705255.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA2700NM-D ## ADs that name it (0) None. ## Approved models (1) - 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. (For Special Conditions see Type Certificate A22WE.) A22WE Boeing DC-10-30 Description of Type Design Change: Cabin configuration changed to accommodate 40 first class and 230 coach passengers. Crew rest facility located forward of Door 2 RH and closet located at Door 2 LH will be removed in accordance with United Air Lines DAS-1-WE Approved Drawing List #2700 dated October 26, 1984 or later FAA approved revisions. Limitations and Conditions: The approval of this change in type d esign applies basically to DC-10-30. The approval does not extend to other aircraft of this mode l on which other previously approved modifications are incorporated unless it is determined by the installer that the interrelationship between this change and any of those other previously approved modifications will in troduce 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 we ight 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. 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: September 5, 1984 Date of issuance: October 26, 1984 Date reissued: November 30, 2011 ( 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/sha256/69/66/6966b675ecaf06b9a3f804fd3ecd171e166aa4390e5fe69beb54551f097d6006) --- 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.