# STC SA7145SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 two axis automatic flight guidance system, Model ST-067 with optional automatic electric trim system.
- Applied: January 14, 1987
- Status date: April 6, 1987
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A16CE](https://openairdocs.org/tcds/A16CE)
- Certificate PDF: https://openairdocs.org/files/sha256/c5/8c/c58cb3f2cc1bc6af924e2f6a142b850f1b2c88cda50024813195a2437bf1b03b
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/25E4CEB088D66E5885256CC20056A1AB.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA7145SW-D

## ADs that name it (0)

None.

## Approved models (2)

- The Cessna Aircraft Company 207A ([TCDS A16CE](https://openairdocs.org/tcds/A16CE))
- The Cessna Aircraft Company T207A ([TCDS A16CE](https://openairdocs.org/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 or amnica Bepartment of transportation—Jpederal 3toiation administration Supplemental 'Cgpe Certificate tSKwm'VW' SA7145SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Z'.y$^<<^^xz6^ -<^4<s<5^fe<*£/£<57«<?7t'x77t^<!^.^£^.^^^ 23 ^d'^sie' Federal Air tSl&3ttta&&nd/.

£0p&a4ma6 iJiwcutcd' —— dijt/i&~&evdiMca£e'tyutrrive&-: A 1 6C E CESSNA 207A and T207A Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-067, with Optional Automatic Electric Trim System according to Bulletin No.

170, Revision 5, dated 11-06-87 and Master Drawing list No. 9280, Revision E, dated 11-06-87 with Optional Flight Director Steering Horizon and/or later FAA Approved revisions of the above data (28 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 8991-1, dated 4-06-87 is required for Cessna Models 207A and T207A, S/N 20700363 through S/N 20700482 and/or later FAA Approved revisions of the above supplement.

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

SXcwnvnt&foafar'^&'^ 1-14-87 4-06-87 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

**FAA FOIM 8110-2(1 0-68)**

ttnittd £tatt» of SUttrira Bepartment of "Cransportation— Jfederal aoiation administration Certificate(Continuation $heet) SA7145SW-D Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 8989-1, dated 4-06-87 is required for Cessna Models 207A and T207A, S/N 20700483 and Upand/or later FAA Approved revisions of the above supplement.

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

Am alteration of this certificate u punishable by a fine of not exceeding SI,OOP, or imprisonment not exceeding 3 years, or hnth.

• AA FORM 8UO-2-! (1O-68) This certificate may be transferred in accordance with I-'Ali ;'/.-/.7.

**PAGE 2OF 2 RAGES**

INSTRUCTIONS : The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferre and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (9jame of transferee) __ (Address of transferee) (O^umfier arut street) (City, State, amCZlT code) from (y^ame. of grantor) ('Print or type) __ __ ___ (Address of grantor) (O^umter and street) (City, State, andZ'l'P code) Exent of Authority (if licensing agreement) :

Signature of grantor (In i Page 2 of ?.

## Every issue (1)

- April 6, 1987: Issued, Current. [certificate](https://openairdocs.org/files/sha256/c5/8c/c58cb3f2cc1bc6af924e2f6a142b850f1b2c88cda50024813195a2437bf1b03b)

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