# STC SA4647SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 60 two axis automatic flight guidance system, Model ST-070 with optional autotrim system, with optional flight director/ steering horizon
- Status date: April 13, 1982
- Data sheets: A16CE, A16CE, A16CE, A16CE
- Certificate PDF: https://openairdocs.org/files/sha256/8e/8e/8e8efb39f9a9d1d1c536aedf6943dcd4888048990a042fa414724a15ab121e36
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/C2FE2B9CC059522085256CC2000E3DC9.0001
- Page: https://openairdocs.org/stc/SA4647SW

## 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 .Starts of amenta Bepartment of transportation—federal 3toiation administration Supplemental "Cuje Certificate SA4647SW Project A5687SW-DS FKP-190S-TEC Corporation Rt. 4, Bldg. 946 Welters Industrial Complex Mineral Wells, Texas 76067 JifoJ^fie'de&tam.jfwJfafi& Afie4^led^4vv0n/me£&-<£^Ja&r<v(>rJfa 23 Federal Aviation A16CE Cessna 207, T207, 207A, T207A Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-070 with Optional Autotrim System according to Bulletin No. 173, dated 1-04-82 and Master Drawing List No. 9283, dated 1-04-82 with Optional Flight Director/Steering Horizon; or according to later FAA approved revision. (M Volt System)

3.C77.

FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 8992 dated 4-13-82 is required for Cessna Models 207A and T207A, S/N 20700483 and Up with S-TEC System 60 Two Axis Automatic Flight Guidance System installed.

FAA Approved Supplemental Flight Manual P/N 8993 dated 4-13-82 is required for Cessna Models 207, T207, 207A and T207A S/N 20700363 through S/N 20700482 withS-TEC System 60 Two Axis Automatic Flight Guidance System Installed.Cpmea£ibility_of_£h£8 modification with other previously approved modifications ^fw^tfwwwwAna/6/i^n^aAw*m>Jejy!ec£MM<wAuv~ &riritM<a^ £%cwru0itb&<a£>V'd January 7, 1982 April 13, 1982 (Signature) 5on P. WatsonChief, Aircraft Certification DivisionSouthwest Region (Title)

This certificate may be transferred in accordance with FAR 21.17.

**FAA FCMM 8110-2 (10-68)**

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

Signature of grantor (In ink):

## Every issue (1)

- April 13, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/8e/8e/8e8efb39f9a9d1d1c536aedf6943dcd4888048990a042fa414724a15ab121e36)

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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.