# STC SA4197SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC system 60 two axis flight guidance system, Model ST-011, with optional autotrim system
- Applied: August 18, 1980
- Status date: September 9, 1981
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/78/78/7878a01d7f0f57b2a3b1851de8cdf7d0c6469548c2bd8780ba247c2399f8768f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/75294EECCDF7204086257DF80072BE98.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA4197SW

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company 182P ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Cessna Aircraft Company 182Q ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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.

United $tatu of amenta Bepartment of transportation—jfeieral aviation administration Supplemental "Cuje Certificate SA4197SU S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ^JwJy^deAt^w.f^^fofittcu'ts^/iw^^ 3 ^J&& Civil Air i/l&zttfa&vnfr.

: 3A13 : Cessna 182P, 182r Installation of S-TEC System 60 Two Axis Flight Guidance System, Model ST-011 with Optional Autotrim System, according to Bulletin No. Ill, Revision 3, dated 7-18-81 and Master Drawing List No. 9216, Revision C, dated 7-18-81 with Optional Flight Director Steering Horizon according to Bulletin No. 120, dated 6-02-80 and Master Drawing List No. 9209, dated 6-02-80, or later FAA approved revision. (14 Volt System) See Continuation Sheet, page 2 of this STC.

>^,<^^ ^w August 18, 1980 ^~^«~/ 5/14/81; 9/9/81 Revision 2 September 9, 1980 L/***,,,*,,*/*/:

(Signatur/7 P. Watson Chief, Engineering and Manufacturing Branch (Title) ~~~

ttnftti £tatts of amtrica Btpartment of transportation— federal aviation administration Supplemental ICgpe Certificate(Continuation Revision 2 Limitations and Conditions:

1. FAA Approved Supplemental Flight Manual P/N 8912 dated 9/9/80 is required with S-TEC System 60 Two Axis Automatic Flight Control System Model ST-011.

2. FAA Approved Supplemental Flight Manual P/N 8912-1 dated 5/14/81 is required with S-TEC System 60 Two Axis Automatic Flight Control System Model ST-011 with or without optional Autotrim System;

or FAA Approved Supplemental Flight Manual P/N 8912-2 dated 9-9-81 is required for Cessna Model 182P and Cessna Model 182$, S/N 18266590 and BELC&7 with S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-011, with or without optional Autotrim System;

or Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8973 dated 9-9-81 is required for Cessna Model 182q, S/N 18266591 and UP with S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-011, with or without optional Autotrim System.

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

**FAA FORM 8HO-2-I (10-69) PAGE 2 OF**

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name, of transferee) (Address of transferee) (Number and street) (City, Slate, and ^IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Stale, and <7P code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- September 9, 1981: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/78/78/7878a01d7f0f57b2a3b1851de8cdf7d0c6469548c2bd8780ba247c2399f8768f)

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