# STC SA5145SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 pitch stabilization system Model ST-038 with optional automatic electric trim system.
- Applied: March 11, 1983
- Status date: April 7, 1989
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A4CE](https://openairdocs.org/tcds/A4CE)
- Certificate PDF: https://openairdocs.org/files/sha256/c4/57/c45733761b29b037bac0c02fd8fdffeecd682715b78ba247dad6127bf6b0749a
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/EF5C4F841DE62AA185256CC2001226F9.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5145SW-D

## ADs that name it (0)

None.

## Approved models (2)

- Textron Aviation Inc. TU206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))
- Textron Aviation Inc. U206G ([TCDS A4CE](https://openairdocs.org/tcds/A4CE))

## 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 £tatts of America Bcpartment of transportation ^federal filiation administration Supplemental t^pe Certificate tSleau/a&o-nd'.

tyMvrrww SA5145SW-D S-TEC Corporation Rt. 4, Bldg. 946 Welters Industrial Complex Mineral Wells, Texas 76067 ij<^ % ^.J/if C i V 1 1 Air A4CE Cessna U206G and TU206G Installation of S-TEC System 60 Pitch Stabilization System Model ST-038 with Optional Automatic Electric Trim System according to Bulletin No. 141, Revision 1, dated 2-06-89 and Master Drawing List No. 92175, Revision A, dated 2-06-89 and/or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible when modified per STC SA1513WE (Robertson STOL).

2. Also eligible when modified per STC SA4033SW (Camera Port).

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

e&jS^ da& 4-07-89, Revision 1 ' *#4 3-11-83 O ~ I O ~ O O (Signature) Harold W. Holdeman DAS Staff Coordinator. DAS 5 SW

This certificate may be transferred in accordance with FAR 21 .47.

FAAFoiM 81 10-2 (10-68)

United £tatu of amrrira Department of transportation— federal auiarion administration Supplemental t^pc Certificate(Continuation £heet) SA5145SW-D, Revision 1 Limitations and Conditions (con't.)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89192, dated 3-18-83 is required for Cessna Models U206G and TU2066 and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89192-1, dated 4-07-89 is required for Cessna Models U206G and TU206G and These Models When Modified Per STC SA1513WE (Robertson STOL) or STC SA4033SW (Camera Port) and/or later FAA Approved revisions of the above supplement.

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

/!»!)• altrration of this certificate is punishable by a fine of not exceeding, S1,000, or imprisonment not exceeding 3 years, or hn/h.

FAA FORM 8HO-2-I do-69) This certificate may bt transferred in accordance with FAR I'/./-7 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 ^IP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, State, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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

## Every issue (1)

- April 7, 1989: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/c4/57/c45733761b29b037bac0c02fd8fdffeecd682715b78ba247dad6127bf6b0749a)

---
OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.