# STC SA4632SW

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 60 pitch stabilization system, Model ST-068 with optional autotrim system.
- Status date: August 3, 1982
- Data sheets: A16CE, A16CE
- Certificate PDF: https://openairdocs.org/files/sha256/19/64/1964b385e15e2615a2d7616a07d6374eecc9fbbc45a896dae1efd4606a44d7e3
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/D026E2A5E0018D6386257E3000603B92.0001
- Page: https://openairdocs.org/stc/SA4632SW

## ADs that name it

None.

## Approved models (2)

- Cessna Aircraft Company 207A (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.

Baited gtatcs or amtrica Bepartment of transportation—federal Stoiation administration Supplemental t^pe Certificate <-SleaM/a&&nA/.

SA4632SW Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ^^^^•a4l^^^,<^^!&«^^^ o^^^w.^.^w^^^^^i^w^^^^/^K/ 23 y^5^Federal Aviation A16CE Cessna : 207A, T207A , „, p „ ^.Installation of S-TEC System 60 Pitch Stabilization System, Model ST-068 with Optional Autotrim System according to Bulletin No. 171, Revision 1 dated 4-01-82 and Master Drawing List No. 9299, Revision A, dated 4-01-82; or later FAA Approved revision. (28 Volt System) See Continuation Sheet, Page 2, of this STC.

s£ev><^^ S^c^mim^t^a^o^^^e' ™: February 17, 1982 March 22, 1982 August 3, 1982 Revision 1 (ffl Ji- f #^/d/WjKvrecS^&n/sfx/A P. Watson Aircraft Certification DivisionSouthwest Region (Title)

tinted States of amtrira Bcpartment of transportation— federal 2toiation administration Supplemental t;gpe Certificate(Continuation £heet) SA4632SW Revision 1 Limitations and Conditions:

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 89112 dated 3/22/82 is required for Cessna Models 207A and T207A with S-TEC System 60 Pitch Stabilization System; OR, FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual P/N 89112-1 dated 8/3/82 is required for Cessna Modeh 207A and T207A S/N 20700483 and UP with S-TEC System 60 Pitch Stabilization System; OR, FAA Approved Supplemental Flight Manual P/N 89122 dated 8/3/82 is required for Cessna Models 207A and T207A S/N 20790363 through S/N 20700482 with S-TEC System 60 Pitch Stabilization System.

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

**FAA FORM 8110-2-1 (1O-69) PAGE 2OF 2PAGES**

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ^IP 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: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/19/64/1964b385e15e2615a2d7616a07d6374eecc9fbbc45a896dae1efd4606a44d7e3)

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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.