# STC SA4734SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 60 pitch stabilization system Model ST-071 with optional autotrim system
- Status date: August 3, 1982
- Data sheets: A16CE, A16CE, A16CE, A16CE
- Certificate PDF: https://openairdocs.org/files/sha256/1b/68/1b688d378416581903c5ea0b01ae15c8f5c72ec289394aac3c59a5eb9a556043
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/BEF8D0C11EAB9A2385256CC2000E3E46.0001
- Page: https://openairdocs.org/stc/SA4734SW

## 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 $tatcs of amrrita Bepartmcnt of Transportation —.federal Situation administration Supplemental Ituje Certificate SA4734SW S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, IX 76067 wJtifa'£ySi&deAMpmf^-&&f<>t£c>t^ Afl£4^MdA^y^v4>w/h^ee&Jfi&^a*wvw 23 <Sl£&Mta£&nA'.

Federal Aviation

••' A16CE : Cessna 207, T207, 207A, T207A . installation of S-TEC System 60 Pitch Stabilization System, Model ST-071, with Optional Autotrim System according to Bulletin No. 174, dated 2-22-82 and Master Drawing List No. 92100, dated 2-22-82, or later FAA approved revision. (14 Volt System) : See Continuation Sheet, page 2, of this STC.

March 24 1982 AUBUSt 3 1982 *\*r /(Signature) Don P. Watson/ Manager, Aircraft Certification Division

FAA FO«M tl 10-7 (10-68)

tinted gtatrs Bcpartment of 'Cransportation—federal aoiation administration Supplemental ICgpe Certificate(Continuation £httt) tSVMWWeW SA4734SW Limitations and Conditions:

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89113, dated 8-3-82, is required for Cessna Models 207A and T207A, S/N 20700483 and UP with S-TEC System 60 Pitch Stabilization System; OR, FAA Approved Supplemental Flight Manual, P/N 89136, dated 8-3-82, is required for Cessna Models 207, T207, 207A, and T207A S/N 20700363 thru S/N 20700482 with S-TEC System 60 Pitch Stabilization System installed.

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

**FAA FORM B110-2-1 (10-69) PAGE 2 OF 2 PAGES**

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

Signature of grantor (In ink):.

## Every issue (1)

- August 3, 1982: Issued, Current. [certificate](https://openairdocs.org/files/sha256/1b/68/1b688d378416581903c5ea0b01ae15c8f5c72ec289394aac3c59a5eb9a556043)

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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.