# STC SA2730NM-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: United Airlines Inc, United States - Description: Install fuselage-mounted white anti-collision strobe lights. - Applied: May 20, 1987 - Status date: November 30, 2011 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) - Certificate PDF: https://openairdocs.org/files/sha256/cf/d9/cfd9c0017309350171699aee96f26645a3d48b6db3fb038109fe04e721175b6c - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/69DA1098EE7D88818625799E006FB66E.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/SA2730NM-D ## ADs that name it (0) None. ## Approved models (2) - The Boeing Company 747-100 Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE)) - The Boeing Company 747SP Series ([TCDS A20WE](https://openairdocs.org/tcds/A20WE)) ## 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 A20WE for Special Conditions Original Product Type Certificate Number : A20WE Boeing 747-100 series, 747SP series Description of Type Design Change : Modifies the aircraft to install fuselage-mounted white anticollision strobe lights. The installation is in accordance with United Air Lines, DAS-1-WE, Drawing List No. 2730 dated September 30, 1987, or later FAA approved revisions. Limitations and Conditions: The approval of this change in type design applies basically to the 747-100, 747SP series only. This approval should not be extended to other aircraft of this model on which other previously approved modifications ar e incorporated, unless it is determined that the interrelationship between this cha nge and any of those other previ ously approved modifications will introduce no adverse effect upon the airworthiness of that 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: May 20, 1987 Date of issuance: October 1, 1987 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/cf/d9/cfd9c0017309350171699aee96f26645a3d48b6db3fb038109fe04e721175b6c) --- 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.