# STC SA8010NM - Type: Supplemental type certificate - Status: Current, Reissued - Holder: Driessen Aircraft Interior Systems, Inc DBA Zodiac Galleys USA Inc, United States - Description: Installation of Windscreen Assembly. - Applied: May 12, 1994 - Status date: July 17, 2014 - Product: Aircraft, Large Multi-Engine - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A2NM](https://openairdocs.org/tcds/A2NM) - Certificate PDF: https://openairdocs.org/files/sha256/6d/cb/6dcb4ecd2aed3d7e8e1896f1d0ce59bce83003c24f05ee213532f4e5b44baacf - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D3149750B032ED5E86257D50005772D5.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA8010NM ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 757-200 Series ([TCDS A2NM](https://openairdocs.org/tcds/A2NM)) ## 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 Driessen Aircraft Interior Systems, Inc. DBA: Zodiac Galleys USA Inc. 17311 Nichols Lane Huntington Beach, California 92647 P art *25 of the F ederal A viation R egulations . *Certification basis is set forth in Type Certificate Data Sheet A2NM Original Product Type Certificate N umber : M ake : M odel : A2NM The Boeing Company 757-200 Series Description of Type Design Changes : Installation of Windscreen Assembly in accordance with FAA Approved Driessen Master Drawing List No. MDL-101631, Revision “B”, dated June 16, 1994, or later FAA approved revisions. Limitations and Conditions : 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 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. Note: The components installed by this STC have not been demonstrated to meet the heat release requirement (65/65) and the smoke emission requirement (200) of FAR 25.853 (a-11), amendment 25-66. A copy of this STC must be included in the permanent records of the modified aircraft. T his 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 A dministrator of the F ederal A viation A dministration. Date of applic ation : May 12, 1994 Date of issuance : July 25, 1994 Date reissued: October 6, 1997; March 27, 1998; April 14, 2003; July 17, 2014 B y direction of the A dministrator (Signature) Haifa Haj-Eid Supervisor, Technical & Administrative Support Staff Los Angeles Aircraft Certification Office (Ti l ) 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.** N umber (STC No.) ## Every issue (1) - July 17, 2014: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/6d/cb/6dcb4ecd2aed3d7e8e1896f1d0ce59bce83003c24f05ee213532f4e5b44baacf) --- 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.