# STC SA5193SW-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-093, with optional automatic electric trim system.
- Applied: May 20, 1983
- Status date: October 15, 1984
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/d1/fa/d1fa2b75e11c1ff9bc013a47e56eb0c5891c9916833a8534a227fdab07f94d9f
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/9436EA56D92018DF85256CC200122764.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5193SW-D

## ADs that name it (0)

None.

## Approved models (9)

- Textron Aviation Inc. 182E ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182F ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182G ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182H ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182J ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182K ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182L ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182M ([TCDS 3A13](https://openairdocs.org/tcds/3A13))
- Textron Aviation Inc. 182N ([TCDS 3A13](https://openairdocs.org/tcds/3A13))

## 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: SA51935W-D This certificate issued to: 1e S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 Part 3 of the CiVil Air Hegulations.

Original Product - Type Bertificate Number: 3A13 Model: 182E, 182F, 182G, 182H, 182J, 182K, 182L, 182M and 182N Description of Type Design Change:

Installation of S-TEC System 60 Pitch Stabilization System, Model ST-093, with Optional Automatic Electric Trim System according to Bulletin No. 196, Revision 2, dated 9-28-84 and Master Drawing List No. 92105, Revision B, dated 9-28-84 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89117-1, dated 8-11-83 is required for Cessna Models 182H, 182J, 182K, 182L, 182M and 182N and/or later FAA Approved revisions of the above supplement.

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

Date of Application: 5-20-83 Date Reissued: 10-15-34, Revision 1 Date of Issuance: . 8-11-83 Date Amended:

FEDERAL AVIATIO By Direction of the Administrator Feberld it still enas (Signature ) Harold W. Holdeman OMINISTRANO DAS Staff Coordinator, DAS 5 SW (Title)

47.

**FAA FORM 3110-2 (10-59)**

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA51935W-D, Revision 1 Limitations and Conditions: (con't)

2. FAA Approved Supplemental Flight Manual, P/N 89527, dated 10-15-84 is required for Cessna Models 182E, 182F and 182G 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.

A TA Cing 81,000, ! not exceeding & vears

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) trom (Name of grantor) (Print or type).

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

Signature of grantor (In ink):

U.S. GOVERNMENT PRINTING OFFICE : 1906 OF -105-97:

## Every issue (1)

- October 15, 1984: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/d1/fa/d1fa2b75e11c1ff9bc013a47e56eb0c5891c9916833a8534a227fdab07f94d9f)

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