# STC SA8380SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 two axis automatic flight guidance system, Model ST-512.
- Applied: November 11, 1993
- Status date: December 6, 1993
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 779](https://openairdocs.org/tcds/779)
- Certificate PDF: https://openairdocs.org/files/sha256/eb/4b/eb4b484db8d577355e9a6342126976b5a7faae8ec399f47a215058b0ae065895
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0DDC829FD672F1FA85256CC20058E769.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA8380SW-D

## ADs that name it (0)

None.

## Approved models (1)

- Raytheon Aircraft Company G17S ([TCDS 779](https://openairdocs.org/tcds/779))

## 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.

Btpartmnit of Transportation—Jfotaal Station administration topplemcntal 'Cgpc Certificate *SUvmv0rt'SA8380SW-D S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 760671/^ta.^Ay*^ s/m*y*^j&~.rf*.^//n^-.£.J*~*V,,nf^~'/4 S/A^. A^SfjmS;,**^. r—'ST{*-1f/1/irTt<) *e&j(+jufwnJ(j*ieA+*ea^wi*r*&'<af£!*f/ 23 ^J&> Federal Aviation 779 BEECH Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-512, according to Bulletin No. 612, dated 11-09-93 and Master Drawing List No.

92602, dated 11-09-93 with Optional Flight Director/Steering Horizon or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible on the above model when modified with IR-985-APS-4 Engine.

(See Continuation Sheet, Page 2, a part of this STC.)

^ j>^^^e*rT^ SZt/miniA/ra/^r-^jA* 11-11-93 12-06-93 Stuff*) WillianTJ. Thomas DAS Staff Coordinator, DAS 5 SU Any alteration of this errtificate is punishablt by a fint of not txcttding tlflOO, or imprisonment not exceeding 3 years, or both.

Tku arlifiettt may tr tiaraftrrid m ttcttdtna until FAR 21.47.

Hiritd Skarrs of 3ntnra Bcpartmtnt of transportation— Jfcdcral 3tnation administration Supplemental TCgpe Certificate(Continuation

SASSSOSW-D Limitations and Conditions (con't.)

2. FAA/DAS Approved Supplemental Flight Manual, P/N 891046, dated 12-06-93 is required for Beech Model G17S And The Above Model When Modified With IR-985-APS-4 Engine or later FAA Approved revisions of the above supplement.

3. Compatibility of this modification with other previously approved modifications must be determined by the installer.

.•I'n Mtfiiittun nf this ctrtifitatt is pumsfigblt by afint of not excitding 11,000, or imprisonment not exceeding 3 years, nr h<tih.

FA* FORM «iio-2.| (10.«») TAu eatifeaU may »« IramfernJ in accordant! uiilfi /•".!/< .'/.^' PAGE 2 Or 2 PAGES

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and <7P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE : 1966 OF—205-579

## Every issue (1)

- December 6, 1993: Issued, Current. [certificate](https://openairdocs.org/files/sha256/eb/4b/eb4b484db8d577355e9a6342126976b5a7faae8ec399f47a215058b0ae065895)

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