# STC SA4661SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 60 single axis automatic flight guidance system, Model ST-091.
- Status date: May 12, 1982
- Data sheets: 3A13, 3A13, 3A13, 3A13, 3A13, 3A13
- Certificate PDF: https://openairdocs.org/files/sha256/bd/6d/bd6dc983007e88a91135ec934d0c6298a2fac8c3e4921bb2fb04c8c2807caded
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/993251DC02C387A585256CC2000E3DE2.0001
- Page: https://openairdocs.org/stc/SA4661SW

## ADs that name it

None.

## Approved models (6)

- Cessna Aircraft Company 182H (TCDS 3A13)
- Cessna Aircraft Company 182J (TCDS 3A13)
- Cessna Aircraft Company 182K (TCDS 3A13)
- Cessna Aircraft Company 182L (TCDS 3A13)
- Cessna Aircraft Company 182M (TCDS 3A13)
- Cessna Aircraft Company 182N (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.

Unittfl gates of amtrica Bepartmcnt of transportation—federal 2toiation administration Supplemental 'Cgpe Certificate <sl£42M>ca&&nA<.

tSbtvrrww SA4661SW Project A5759SW-DSFKP-190 S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 Jfi&Jufi&dc&*jaWjtwJfo^t>£6c>u>^ *aM*^^ 3 Wt^S^Clvil Air

•: 3A13 : Cessna : 182H, 182J, 182K, 182L, 182M, 182N <: installation of S-TEC System 60 Single Axis Automatic Flight Guidance System, Model ST-091 according to Bulletin No. 194, dated 3-18-82 and Master Drawing Ust No. 92104, dated 3-18-82, or later FAA Approved revision. (14 Volt System) FAA Approved Supplemental Flight Manual P/N 89116 dated 5-12-82 is required for Cessna Models 182H, 182J, 182K, 182L, 182M and 182N with S-TEC System 60 Single Axis Automatic Flight Guidance System.

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

S$dmvn4A&<a&>r-JcfJ March 18, 1982 May 12, 1982 vs&Jfae/i SS-J.

(Signature) -Don P. Watson ,/Acting Chief, Aircraft CertificationDtytfiton - Souttwqpt; Bag-ton (Title)

Thii certificate may be transferred in accordance with FAR 21.47.

FAA FotM 81)0-2(10-48)

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name oj transferee) (Address of transferee) (Number and street) (City, State, and £1P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Slate, and <7P code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink): _

## Every issue (1)

- May 12, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/bd/6d/bd6dc983007e88a91135ec934d0c6298a2fac8c3e4921bb2fb04c8c2807caded)

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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.