# STC SA5324SW-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-042, with optional automatic electric trim system.
- Applied: April 13, 1984
- Status date: May 25, 1984
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A18EU](https://openairdocs.org/tcds/A18EU)
- Certificate PDF: https://openairdocs.org/files/sha256/69/d3/69d3de662dd21c56ae4ed14718327e3451a631a6d66e09178fef691e9a99ddc7
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F4BEC116AF21FC6885256CC200122864.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5324SW-D

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company FR172J ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))
- Cessna Aircraft Company FR172K ([TCDS A18EU](https://openairdocs.org/tcds/A18EU))

## 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.

Hiritrd £tatti ofSUntnta Bepartmcnt of transportation— federal atoiation administration Supplemental 'Cgpe Certificate iSLumve?" SA5324SW-D **/*, ***„*<//<- na* S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 ai&v*e-rri >i&jA&£>T^ 3 d^n*. Civil Air

•-Stf&t&tG&t'nA .

fsriatnaJ \Jrvducf —— • A 1 8 E U

REIMS-CESSNA FR172J AND FR172K -naf :

Installation of S-TEC System 60 Pitch Stabilization System Model ST-042, with Optional Automatic Electric Trim System, according to Bulletin No. 145, Revision 2, dated 3-20-84 and Master Drawing List No. 9244, Revision B, dated 3-20-84 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89432, dated 5-25-84 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.

4-13-84 5-25-84 £$ctrnAm4&&a£y*-^4n* (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

This certificate may kt transferrtd in atcordana with FAR 21.17.

FAA FO«M»! 10-2 (10-68)

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

## Every issue (1)

- May 25, 1984: Issued, Current. [certificate](https://openairdocs.org/files/sha256/69/d3/69d3de662dd21c56ae4ed14718327e3451a631a6d66e09178fef691e9a99ddc7)

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