# STC SA5159SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 pitch stabilization system Model ST-152 with optional automatic electric trim.
- Applied: April 22, 1983
- Status date: June 21, 1984
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A18CE](https://openairdocs.org/tcds/A18CE)
- Certificate PDF: https://openairdocs.org/files/sha256/47/85/4785332d63e234e05ff4ed5ee25e233bdee9a16de8c8943cf5192853f106222f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/0A0D5643E20278EB86257EC9004F3AEE.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5159SW-D

## ADs that name it (0)

None.

## Approved models (3)

- Alexandria Aircraft LLC 17-30A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31A ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))
- Alexandria Aircraft LLC 17-31ATC ([TCDS A18CE](https://openairdocs.org/tcds/A18CE))

## 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.

Bratri States of 2Untnca Bepartmcnt of transportation — jFedcral 2toiation administration Supplemental 'Cfipe Certificate iSiu#n<vevt' SA5159SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wo Hers Industrial Complex Mineral Wells, TX 76067 r^fw*^^ 23 ^&t> Federal Aviation CSrtainaJ <JrvcUt£/' —— •JiuJi&'&e'i^^icM&iSlu'rnver-: A-18CE

BELLANCA 17-30A, 17-31A AND 17-31ATC '-naf •' Installation of S-TEC System 60 Pitch Stabilization System Model ST-152, with Optional Automatic Electric Trim System according to Bulletin No. 252, Revision 1, dated 5-04-84, and Master Drawing List No. 92189, Revision A, dated 5-04-84 and/or later FAA Approved revisions of the above data (14 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89204, dated 5-2-83, is required and/or later FAA Approved revisions of the above supplement.

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

^ SXf^n^rnA^a^c-f-^ 4-22-83 @L&~*4~*J: 6-21-84, Revision 1 ~^— >r y^- (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW \ *"-- /

FAA taw •! 10-J (IO-6«)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee) (A ddress of transferee) (Number and street) (City, State, and £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)

- June 21, 1984: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/47/85/4785332d63e234e05ff4ed5ee25e233bdee9a16de8c8943cf5192853f106222f)

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