# STC ST00308SE-D - Type: Supplemental type certificate - Status: Current, Reissued - Holder: TASS Inc, United States - Description: Installation of a Rockwell Collins Global Navigation Landing System (GNS/GNLS) provisions - Applied: October 6, 1998 - Status date: April 27, 2012 - Product: Aircraft, Large Airplane - Certification basis: Part 21, Part 25 - Data sheets: [TCDS A16WE](https://openairdocs.org/tcds/A16WE) - Certificate PDF: https://openairdocs.org/files/sha256/d2/e1/d2e173349476132489177b9fa8b911004b029b3533d9443f993ea2e1ec61da90 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/02EDE45B3A6094B8862579F400701D73.0001 - DRS record last changed: December 5, 2025 - Page: https://openairdocs.org/stc/ST00308SE-D ## ADs that name it (0) None. ## Approved models (1) - The Boeing Company 737-200 Series ([TCDS A16WE](https://openairdocs.org/tcds/A16WE)) ## 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. Number ST00308SE-D This certificate, issued to TASS, Inc. 12016 115th Ave NE, Suite 100 Kirkland, WA 98034 Part 25 of the Federal Aviation Regulations.(See Type Certificate Data Sheet A16WE for complete certification basis) Original ProductType Certificate Number: A16WE Make: Boeing Model: B737-200 Description of the Type Design Change: Installation of a Rockwell Collins Global Navigation Landing System (GNS/GNLS) provisions in accordance with BF Goodrich Master Drawing List (MDL) 98-125, Sheet 1, Revision New, dated November 5, 1998, or later Federal Aviation Administration (FAA) or Designated Alteration Station (DAS) approved revision. Limitations and Conditions: Approval of this change in type design applies to the above model aircraft only. This approval is applicable to the full provisions for the Rockwell Collins GNS/GNLS only and does not approve the installation of the actual Rockwell Collins GNS/GNLS equipment. This approval should not be extended to other aircraft of this model on which other previously approved modifications are incorporated unless it is determined that the relationship between this change and any of those other previously incorporated approved modifications, including changes in type design, will introduce no adverse effect upon the airworthiness of that aircraft. A copy of this certificate and BF Goodrich Aerospace, Inc. MDL 98-125, Sheet 1, Revision New, dated November 5, 1998, or later FAA/DAS-approved revision must be maintained as part of the permanent records for the modified 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. Date of application: October 6, 1998 Date reissued: April 27, 2012 Date of issuance: November 6, 1998 Date amended: May 5, 2000 (Signature) Acting Manager, Seattle Aircraft Certification Office (Title) ## Every issue (1) - April 27, 2012: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d2/e1/d2e173349476132489177b9fa8b911004b029b3533d9443f993ea2e1ec61da90) --- 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.