# STC SA5243SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System, 40/50 single and two axis automatic flight guidance systems Model ST-219-40/50.
- Applied: October 19, 1983
- Status date: November 28, 1983
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 1, Part 21
- Data sheets: [TCDS A29CE](https://openairdocs.org/tcds/A29CE)
- Certificate PDF: https://openairdocs.org/files/sha256/da/f8/daf8f9a789fef9639484197c0897ccd8560e91d82cf772b95a20605b995ab43e
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/031C43B1894A488885256CC2001227CD.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5243SW-D

## ADs that name it (0)

None.

## Approved models (1)

- Beechcraft Corporation 76 ([TCDS A29CE](https://openairdocs.org/tcds/A29CE))

## 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 Starts of anmca Btpartment of transportation —jfderal atriation administration Supplemental 'Cgpe Certificate SA5243SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex :

Mineral Wells, TX 76067 \.Jevru/,cf>n£u£*>nA &^4cj£edAe*e*>n-*n4^jA**i4*wf>v>^^ 23 ^J&v Federal Aviation isf&2A&c&&f>nA,, A£ :? L t BEECH 76 Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-219-40/50, according to Bulletin No. 319, dated 9-13-83 and Master Drawing List No. 92246, dated 9-13-83 and/or later FAA Approved revisions of the above data (28 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89340, dated 11-28-83 is required for S-TEC System 40 and/or later FAA Approved revisions of the above supplement.

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

"Aj sM*~*j*i'A *, 44 /(r/t/r'ft^^sS jiy, M* ££dmvrUjlJr<l/&r-MjSl» 10-19-83 11-28-83 (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW (TitU)

TAit certificate may bt traufrmc in tenrtotttt with FAR 21.47.

FAA tavi II1O-2 (1O-6*1

•Hnitrfl &tatu of SLmcrica Bepartmtnt of ^Transportation— federal atriation administration Supplemental t:jjpe Certificate(Continuation £heet) SA5243SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89341, dated 11-28-83, is required for S-TEC System 50, and/or later FAA Approved revisions of the above supplement.

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

FAA FORM 8110-2-1 (IO-69) This certificate may be tranrj'crred in acemdanrt with FAR i'1.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee).

(Address of transferee). (Number and street) (City, State, and Z.IP code) from (Name of grantor) (Print or type).

(Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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

## Every issue (1)

- November 28, 1983: Issued, Current. [certificate](https://openairdocs.org/files/sha256/da/f8/daf8f9a789fef9639484197c0897ccd8560e91d82cf772b95a20605b995ab43e)

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