# STC SA7200SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 single axis automtic flight guidance system Model ST-094.
- Applied: October 5, 1989
- Status date: October 27, 1989
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4EU](https://openairdocs.org/tcds/A4EU)
- Certificate PDF: https://openairdocs.org/files/sha256/d6/ca/d6ca3cbc7611ce68860a6938961c3426fd9d1bb92f4acccba566a9fa0e957e17
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F12A183E795B09B085256CC20056A201.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA7200SW-D

## ADs that name it (0)

None.

## Approved models (5)

- Cessna Aircraft Company F172F ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172G ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172H ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172K ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))
- Cessna Aircraft Company F172L ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

niced States of Barice Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA7200SW-D This certificate issued to: S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 Certifies that the change in the type design for the following product with the limitations and condilions thorefor as specified hereon meels the airworthiness requiroments of Part 3 of the CiVil Air Regulations.

Original Product _ Type bortificate Numben: AAEU Make: Reims-Cessna Model: F172F, F172G, F172H, F172K and F172L Description of Type Design Change:

Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-094, according to Bulletin No. 197, Revision 2, dated 10-03-89 and Master Drawing List No. 92145, Revision B, dated 10-03-89 and/or later FAA Approved revisions of the above data (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89829, dated 10-27-89 is required and/or later FAA Approved revisions of the above supplement.

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

Date of Application: 10-05-89 Dolevissued:

Tiale of issuanco: 10-27-89 Date Amended:

EDERAL AVIATIO By Direction of the Administrator (Signalure) TOMINISTA TIO Harold W. Holdeman DAS Statt Coordinator, DAS 5 SW (Title)

47.

**PAN FORM 8110-2 (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 ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ZIP code) Exent of Authority (if licensing agreement) :

Signature of grantor (In ink) :

## Every issue (1)

- October 27, 1989: Issued, Current. [certificate](https://openairdocs.org/files/sha256/d6/ca/d6ca3cbc7611ce68860a6938961c3426fd9d1bb92f4acccba566a9fa0e957e17)

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