# STC SA4646SW

- 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-069
- Status date: April 12, 1982
- Data sheets: A16CE, A16CE, A16CE, A16CE
- Certificate PDF: https://openairdocs.org/files/sha256/e4/68/e468041cc5b355c02f04dcdebfe09d61a1587fab653a31ecdbc5fc57bb9e3097
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8A96DACDD84EF33B85256CC2000E3DC7.0001
- Page: https://openairdocs.org/stc/SA4646SW

## ADs that name it

None.

## Approved models (4)

- Cessna Aircraft Company 207 (TCDS A16CE)
- Cessna Aircraft Company 207A (TCDS A16CE)
- Cessna Aircraft Company T207 (TCDS A16CE)
- Cessna Aircraft Company T207A (TCDS A16CE)

## 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 Statu Of amrrica Bepartmcnt of Importation—federal 2toiation administration Supplemental 'Cgpe Certificate tSKivrriv&r' SA4646SW Project A5686SW-DS FKP-190 Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 Federal Aviation Jfas6yfwJeieAjjcjWfW'tn&f& .d^i&xfi^Atvvvw/fri^e&'^^M^tiic^^ 23 <SleMt£a&&n&.

£Jf*ai-naJ Jvvauct —— J/uSw~&:e>rt&tc4i4e'<yu40rdei*-: A16CE Cessna : 207, T207, 207A, T207A Installation of S-TEC System 60 Single Axis Automatic Flight Guidance System Model ST-069 according to Bulletin No. 172, dated 1-13-82 and Master Drawing Ust No. 9289, dated l-lX-82, or later FAA approved revision. (14 Volt System) reltf Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89100 dated 4-12-82, is required with S-TEC System 60 Single Axis Automatic Flight Guidance System for Cessna Models 207A and T207A, S/N 20700483 and Up.

2. FAA Approved Supplemental Flight Manual, P/N 89101 dated 4-12-82, is required with S-TEC System 60 Single Axis Automatic Flight Guidance System for Cessna Models 207, T207, 207A and T207A S/N 20700363 through S/N 20700482.3. Compatibility of this modification with other previously approved modifications must b*^determined by the installer. / / / , * / / // M^</7/j <^W^^^^^Z^l*/l<£^ xl^^^4^W<i?Z^xZ<T^^ January 12, 1982 April 12, 1982 Acting Chief?Division Aircraft Certification (Title) Any alteration o//Ai'f certificate » punishable by ajine of not exceeding $1,000, or imprisonment not exceeding 3yean, or both.

fAA fotM 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, Slate, and £IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Stale, and <7f code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- April 12, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/e4/68/e468041cc5b355c02f04dcdebfe09d61a1587fab653a31ecdbc5fc57bb9e3097)

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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.