# STC SA6084SW-D - Type: Supplemental type certificate - Status: Current, Amended - Holder: S-TEC Corporation, United States - Description: Installation of S-TEC system 65two axis automatic flight guidance system Model ST-372. - Applied: September 25, 1986 - Status date: March 6, 1995 - Product: Aircraft, Small Multi-Engine - Certification basis: Part 21 - Data sheets: [TCDS 3A16](https://openairdocs.org/tcds/3A16) - Certificate PDF: https://openairdocs.org/files/sha256/36/98/3698a36aa9a8b5fbbb87e00615aeab2f8b4ff601e63f65940fd26ef477e8bb33 - FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/95AF274743ECF8D386257F540054896C.0001 - DRS record last changed: December 6, 2025 - Page: https://openairdocs.org/stc/SA6084SW-D ## ADs that name it (0) None. ## Approved models (10) - Raytheon Aircraft Company 95-55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-A55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-B55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-B55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-C55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company 95-C55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company D55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company D55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company E55 ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) - Raytheon Aircraft Company E55A ([TCDS 3A16](https://openairdocs.org/tcds/3A16)) ## 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. 3tata o Santa Btpartmnit of transportation —federal 3triation administration Supplemental t^pc Certificate SA6084SW-D S-TEC Corporation 946 Pegram Mineral Wells, TX 76067 ^ 3 Civil Air 3 A 1 6 Beech 95-55, 95-A55, 95-B55, 95-B55A, 95-B55B, 95-C55, 95-C55A, D55, D55A, E55, E55A, 56TC, A56TC Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System, Model ST-372, according to Bulletin No. 472, Revision 2, dated 1-31-95 and Master Drawing List No. 92388, Revision B, dated 1-31-95 with Optional Flight Director/ Steering Horizon or later FAA Approved revisions of the above data (28 Volt System) 1. Only eligible on Model 95-B55B When Modified Per Beech Drawing 96-002000 (Civilian Conversion). (See Continuation Sheet, Page 2, a part of this STC.) e£^jX^ -&^^e**rit*i^ $Zc/Tn*ruAJra£>*- *J J&t 9-25-86 <5T->. _•.. -J. 9-29-86 tpMAMrrH^Sn/- 3-06-95, Revision 1 Willianr J. Thomas DAS Staff Coordinator, DAS 5 SW (Title) fine of not exceeding f! ,000, or imprisonment not exceeding 3 years, or both. ttrtijttale may br traiuferrtd in ttmdantt until FAR 21.17. Umiri Starts of 3nrrra Bepartmoit of Transportation— jfotaal 3tJiarion administration (dantinuanon £?hKt) SA6084SW-D, Revision 1 Limitations and Conditions (con't.) 2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89689, dated 9-29-86 is required for Beech Models 95-55, 95-A55, 95-855, and 95-B55A or later FAA Approved revisions of the above supplement. 3. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 89689-1, dated 3-06-95 is required for Beech Models 95-55 95-A55, 95-B55, 95-B55A; and 95-B55B When Modified Per Beech Drawing 96-002000 (Civilian Conversion) or later FAA Approved revisions of the above supplement. 4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89690, dated 9-29-86 is required for Beech Models 95-C55, 95-C55A, 055, D55A, E55, and E55A or later FAA Approved revisions of the above supplement. 5. FAA/DAS Approved Pilot's Operating Handbook and/or Airplane Flight Manual Supplement, P/N 891147, dated 3-06-95 is required for Beech Models 56TC and A56TC or later FAA Approved revisions of the above supplement. 6. Compatibility of this modification with other previously approved modifications must be determined by the installer. Mitrution of this cerafieatt is piuoshabU by a fin* of not exeteding SI,OOP, or imprisonment not txeeeding 3 years, or hmh. *O»M •nu.i-i no-W Thi eatifeatt may bi trmtftrrtii m aetordanti ictih l-'Alt ;7.V* PACC 2 OF 2 PACES 1 INSTRUCTIONS: The transfer endowment below m.y be used to notify the appropriate FAA Kepon.l Office of the transfer of thu Supplemental Type Certificate. The FAA will reissue the certificate in the name of the transferee and forward il 10 Mm. TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee). (Address of transferee). ( ,V«mA«r md Oral) from (Name of grantor) (Print or type). (Address of grantor) (Off. Signature of grantor (In ink): ## Every issue (1) - March 6, 1995: Amended, Current. [certificate](https://openairdocs.org/files/sha256/36/98/3698a36aa9a8b5fbbb87e00615aeab2f8b4ff601e63f65940fd26ef477e8bb33) --- 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.