# STC SA4238SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC system 60 two axis flight guidance system, ST-016, with optional autotrim system
- Status date: August 26, 1981
- Data sheets: 3A13, 3A13
- Certificate PDF: https://openairdocs.org/files/sha256/60/0c/600cfec6c8e75343b870a864667c644a3d7d39876ec1edf2cc041e1a7c26fb85
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/65103DFFFD92883B86257DF900595FC6.0001
- Page: https://openairdocs.org/stc/SA4238SW

## ADs that name it

None.

## Approved models (2)

- Cessna Aircraft Company 182Q (TCDS 3A13)
- Cessna Aircraft Company 182R (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 States or amrrica ©tpartment of ^Transportation — federal 2toiation administration Supplemental t:jp Certificate i/le*gbu£a&c>'n&'.

SA4238SW S-TEC Corporation Route 4, Building 946 Wolters Industrial Complex Mineral Wells, Texas 76067 v^fo'fyfaJcteA*:pm^w.&&.fi6buHw^/w>d^^ Civil Air 3A13 Cessna 182R Installation of S-TEC System 60 Two Axis Flight Guidance System, Model ST-016, with Optional Autotrim System according to Bulletin No. 116, Revision 2, dated 7-18-81 and Master Drawing List No. 9217, Revision B, 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. (28 Volt System) See Continuation Sheet, page 2 of this STC.

«^x^ : September 12, 1980 November 20, 1980 6/22/81; 8/26/81 Revision 2 P. Watson Chief, Engineering and Manufacturing Branch (Title)

FAA FO«M 8II0-2 (10-68)

tinted States of amtrica Bcpartmcnt of 'Cransportation— JFcderal 2ttrtation administration Supplemental 'Cgpe Certificate(Continuation 3hcct) « , , iRevision 2 Limitations and Conditions r

1. FAA Approved Supplemental Flight Manual P/N 8915, dated 11/20/80, is required for Cessna Model 182Q, with S-TEC System 60, Two Axis Automatic Flight Control System, Model ST-016.

2. FAA Approved Supplemental Flight Manual P/N 8915-1, dated 6/22/81, is required for Cessna Model 182Q with S-TEC System 60, Two Axis Automatic Flight Control System, Model ST-016, with or without Optional Autotrim System;

or FAA Approved Supplemental Flight Manual P/N 8915-2 dated 8/26/81 is required for Cessna Model 182Q, S/N 18266590 and BELOW with S-TEC System 60, Two Axis Automatic Flight Guidance System, Model fjT-016, with or without Optional Autotrim System;

or Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8974 dated 8/26/81 is required for Cessna Model 182(}, S/N 18266591 and UP with S-TEC System 60, Two Axis Automatic Flight Guidance System Model ST-016, with or without Optional Autotrim System.

3. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement P/N 8965, dated 6/22/81, is required for Cessna Model 182R with S-TEC System 60, Two Axis Automatic Flight Control System, Model ST-016.

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

FAA FORM siio-2-1 (10-69) PAGE 2 OF 2 PAGES

## Every issue (1)

- August 26, 1981: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/60/0c/600cfec6c8e75343b870a864667c644a3d7d39876ec1edf2cc041e1a7c26fb85)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.