# STC SA5162SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC yaw damper system Model ST-135.
- Applied: May 5, 1983
- Status date: January 13, 1987
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A15](https://openairdocs.org/tcds/3A15)
- Certificate PDF: https://openairdocs.org/files/sha256/8b/47/8b477ad178345e6c866b925a7ea20f60ed268117ea78d425567f866e6032d6b1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/F5C6C9EC5D066D9685256CC200122721.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5162SW-D

## ADs that name it (0)

None.

## Approved models (6)

- Beechcraft Corporation H35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation J35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation K35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation M35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation N35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))
- Beechcraft Corporation P35 ([TCDS 3A15](https://openairdocs.org/tcds/3A15))

## 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.

ttititrd Statu of amrrica Btparrmcnt of Transportation —federal atriation administration Supplemental "Cgpe Certificate SA5162SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 n&* Civil Air f .'l£&t&£ii&{* fj*€a*-mu d&vciuc/ 3A1 5 BEECH H35, J35, K35, M35, N35 AND P35 &£' :

Installation of S-TEC Yaw Damper System, Model ST-135, according to Bulletin No. 235, Revision 2, dated 10-28-86 and Master Drawing List No. 92191, Revision B, dated 10-28-86 and/or later FAA Approved revisions of the above data (14 VoltSystem) .

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89206, dated 5-16-83 is required and/or later FAA Approved revisions of the above supplement.

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

5-05-83 5-16-83 JJA^Jh^^ SX</mtvi4&lra£f>r-*fjA« 1-13-87, Revision 1 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW

This certificate may bt trarufrmJ in accorJanet with FAR 21.17.

FAA fox • 119-2 (10-«t)

United #tatu of amain Bepartmtnt of ^transportation— Jp eflcral aoiation administration Supplemental t^pe Certificate(Continuation £htet) SA5162SW-D, Revision 1 Limitations and Conditions (con't)

2. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89206-1, dated 1-13-87 is required and/or later FAA Approved revisions of the above supplement.

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

alteration of this certificate is punishable by a fine of not exceeding SI,OOP, or imprisonment not exceeding 3 years, or both.

FORM 8tto-2-i (10-6?) This certificate may be transferred in accordance with l-'AR i'l.1~ 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, State, and <7P code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

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

## Every issue (1)

- January 13, 1987: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/8b/47/8b477ad178345e6c866b925a7ea20f60ed268117ea78d425567f866e6032d6b1)

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