# STC SA6032SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 pitch stabilization system, Model ST-152, with optional automatic electric trim system.
- Applied: July 9, 1985
- Status date: August 1, 1985
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 1A3](https://openairdocs.org/tcds/1A3)
- Certificate PDF: https://openairdocs.org/files/sha256/2c/35/2c35b7979f1becdbccff619ba9ce653fb10e35505ce4e0e45069486082cb68d0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/B92406FF8DA79F2585256CC200569DFF.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA6032SW-D

## ADs that name it (0)

None.

## Approved models (3)

- Alexandria Aircraft LLC 17-30 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-31 ([TCDS 1A3](https://openairdocs.org/tcds/1A3))
- Alexandria Aircraft LLC 17-31TC ([TCDS 1A3](https://openairdocs.org/tcds/1A3))

## 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.

Umtri Starts of aartica Bepartmcnt of tensportation —federal 2toiation administration Supplemental 'Cgpe Certificate SA6032SW-D

- S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Mineral Wells, TX in JSLS /ufu dtA^an fif &f <Ja . . sltaAi C***a* Complex 76067 aiawm 1A3

BELLANCA 17-30, 17-31 AND 17-31TC Civil Air ft -siuSi* Installation of S-TEC System 60 Pitch Stabilization System, Model ST-152, with Optional Automatic Electric Trim System, according to Bulletin No. 252, Revision 3, dated 6-20-85 and Master Drawing List No. 92189, Revision C, dated 6-20-85 and/or later FAA Approved revisions of the above data (14 Volt System).

FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89610, dated 8-01-85 is required for Bellanca Models 17-30, 17-31 and 17-31TC and/or later FAA Approved revisions of the above supplement.

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

7-09-85 8-01-85 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Tttlt)

fAA fottt S110-3 (1O-6i) This artifuatt may k* ttansfrrrtj in mctmtkina with FAR 21.47.

INSTRUCTIONS: The transferendowment below may be u.ed .o notify the appropriate FAA Kcgion.1 Office of the transfer of thu Supplemcnul Type Certificate.

The FAA will remue the certificate in the name of the transferee and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee).

(Address of transferee). ( Xutntxr *nJ ttrttt) (Cit>. State.

from (Name of grantor) (Print or type).

(Address of grantor) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- August 1, 1985: Issued, Current. [certificate](https://openairdocs.org/files/sha256/2c/35/2c35b7979f1becdbccff619ba9ce653fb10e35505ce4e0e45069486082cb68d0)

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