# STC SA5214SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 pitch stabilization system Model ST-071 with optional automatic electric trim system.
- Applied: April 22, 1983
- Status date: October 5, 1983
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A16CE](https://openairdocs.org/tcds/A16CE)
- Certificate PDF: https://openairdocs.org/files/sha256/61/16/61165def869c361dc3e80ff9294111fe3a55e9787c5e3397b817ba2b2b9e9d7b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/77BE88DC41B7ACAF85256CC200122794.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5214SW-D

## ADs that name it (0)

None.

## Approved models (4)

- Cessna Aircraft Company 207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207 ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- Cessna Aircraft Company T207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))

## What the certificate says

This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA52145W-D This certificate issued to: S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Part 23 of the Federal Aviation Hegulations.

Original Product -TypePentificate Numben: AI6CE Make: CESSNA Model: 207, T207, 207A, AND T207A Description of Type Design Change:

Installation of S-TEC System 60 Pitch Stabilization System Model ST-071 with Optional Automatic Electric Trim System, according to Bulletin No. 174, Revision 1, dated 2-28-83 and Master Drawing List No. 92100, Revision A, dated 2-28-83 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89113-1, dated 10-05-83 is required for Cessna Models 207A and T207A, S/N 20700483 and up and/or later FAA Approved revisions of the above supplement.

(See Continuation Sheet, Page 2, a part. of this STC).

Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

47.

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA52145W-D Limitations and Conditions: (cont'd)

2. FAA Approved Supplemental Flight Manual, P/N 89136-1, dated 10-05-83 is required for Cessna Models 207, T207, 207A, and T207A S/N 20700363 thru S/N 20700482, and/or later FAA Approved revisions of the above supplement.

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

**47 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 ZIP code) from (Name of grantor) (Print or type).

(Address of grantor) (Number and street) (City, Stale, and ZIP code ) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE: 1966 OF-205-579

## Every issue (1)

- October 5, 1983: Issued, Current. [certificate](https://openairdocs.org/files/sha256/61/16/61165def869c361dc3e80ff9294111fe3a55e9787c5e3397b817ba2b2b9e9d7b)

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