# STC SA1999NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States - Description: Installation of Stowe Corporation Cart, P/N 12700-1. - Applied: March 17, 1983 - Status date: July 17, 2014 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A20WE](https://openairdocs.org/tcds/A20WE) - Certificate PDF: https://openairdocs.org/files/sha256/46/1f/461f0413a89a40ab7f776247c7a0068c8ae3504e8420d22b20190cdd8a7a798e - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8B022954616440BE86257D960068F739.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA1999NM ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 747-100 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. United States Of America Department of Transportation - Federal Aviation Administration Supplemental Type Certificate This certificate has been reissued to replace the original certificate reported as lost. This Certificate issued to Driessen Aircraft Interior Systems, Inc. DBA: Zodiac Galleys USA Inc. 17311 Nichols Lane Huntington Beach, California 92647 Part 25* of the Federal Aviation Regulations. *Certification basis is set forth in Type Certificate Data Sheet A20WE Original Product Type Certificate Number : A20WE The Boeing Company 747-131, 747-136, 747-156A Description of Type Design Changes: Installation of Stowe Corporation Cart, P/N 12700-1 in accordance with FAA approved Stowe Corporation Drawing List labeled Tray Modules, P/N 12700-1, Revision “E”, dated July 29, 1983, or later FAA approved revisions. Limitations and Conditions: The approval of this change in type design applies to the Boeing 747-131, 747-136, 747-156A aircraft model only. This approval should not be extended to other aircraft of this model 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 introduce no adverse effect upon the airworthiness of these aircraft. This determination should include consideration of significant changes in weight distribution such as an increase in the fixed disposable weight of 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 ii Date of application : March 17, 1983 Date of issuance : August 5, 1983 Date reissued: October 30, 1989; July 17, 2014 (Signature) 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) - July 17, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/46/1f/461f0413a89a40ab7f776247c7a0068c8ae3504e8420d22b20190cdd8a7a798e) --- 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.