# STC SA5293SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 single axis automatic flight guidance system Model ST-012.
- Applied: January 6, 1984
- Status date: August 22, 1986
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4EU](https://openairdocs.org/tcds/A4EU)
- Certificate PDF: https://openairdocs.org/files/sha256/21/65/216569962b224377358224a36d87b2f24d6623b9147113b345546e249ea11d52
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1F87C9FBA11B24CC86257ECA0077CF48.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5293SW-D

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company F172N ([TCDS A4EU](https://openairdocs.org/tcds/A4EU))

## 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.

Hratri £ntti of aatnca

•Btpartmcnt of transportation — federal atriation Administration Supplemental TCuje Certificate iSiivmvev' SA5293SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 ^ *^ 3 j^^A^ Civil Air (sriairui/ J/pvcutc/ —— I/yfve 'l^fr^uKca^e^/l^rn^ef' A4 E U

REIMS-CESSNA F172N -J *eAA&n ~fzAjma* :

Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-012, according to Bulletin No. 112, Revision 4, dated 7-01-86 and Master Drawing List No. 9225, Revision D, dated 7-01-86 and/or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible on the above Model when modified by 180 H.P. Engine Conversion.

2. FAA Approved Supplemental Flight Manual, P/N 89385, dated 3-27-84 is required and/or later FAA Approved revisions of the above supplement.

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

Ze>r*rU^^ S&cJmvni&Jfa£>r-<afj 1-6-84 ^4-*«ju««y.- 8-22-86, Revision 1 3-27-84 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW(Title)

TAu certificate may b* traiuftmd in accordant* with FAR 21.17.

FAA row 1110-2 (10-«t)

United £tatts of amenta Bepartment of transportation— federal Sttnation administration Supplemental HDgpe Certificate(Continuation £hett) SA5293SW-D, Revision 1 Limitations and Conditions (con't)

3. FAA Approved Supplemental Flight Manual, P/N 89385-1, dated 8-22-86 for Reims- Cessna Model F172N and Reims-Cessna Model F172N when modified by 180 H.P.

Engine Conversion.

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

/l)iV alteration (if this certificate is punishable by a fine oj not exceeding Sl,000, or imprisonment not exceeding .3 years, or both.

I-AA FORM 8110-2-1 (10-69) Thii Certificate may be transferred in accordance with I-'AR -I.!?.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZJP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^IP cade) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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

## Every issue (1)

- August 22, 1986: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/21/65/216569962b224377358224a36d87b2f24d6623b9147113b345546e249ea11d52)

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