# STC SA6051SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC system 60 pitch stabilization system, ST-292, with optional automatic electric trim system.
- Applied: December 4, 1985
- Status date: September 27, 1988
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS 3A13](https://openairdocs.org/tcds/3A13)
- Certificate PDF: https://openairdocs.org/files/sha256/95/55/9555555eac115e3fe494a6c7f947b164e1284e9c962172717776dbd4301fbced
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/4A48C2A74FC23B5685256CC200569E2E.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA6051SW-D

## ADs that name it (0)

None.

## Approved models (6)

- 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))

## 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: SA605154-0 This certificate issued to: S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 Part 3 of the Civil Air Regulations:

Original Product -Typetertificate Number: 3A13 Make: Cessna Model: 182G, 182H, 182J, 182K, 182L and 182M Description of Type Design Change:

Installation of S-TEC System 60 Pitch Stabilization System, ST-292, with Optional automatic Llectric Trim System according to Bulletin No. 392, Revision 1, dated 9-01-88 and Master Drawing List No. 92344, Revision A, dated 9-01-88 is required and/or later FAA Approved revisions of the above data (14 Volt System).

1. Only eligible on Model 182G When Modified Per STC SA403SW (WREN 460).

2. Only eligible on Models 182H, 182J, 182K, 182L and 182M When Modified Per STC SA485SW (WREN 460H, 460J, 460K, 460L and 460M).

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

Date of Application: 12-04-85 Date Reissued: 9-27-88, Revision 1 Date of Issuance: 1-08-86 Date Amended:

FEDERAL AVIATION By Direction of the Administrator Sente I Hopelera ( Signature ) T MINISTRATIO Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate (Continuation Sheet) Number: SA60515W-D, Revision 1 Limitations and Conditions: (con't.)

3. FAA Approved Supplemental Flight Manual, P/N 89631, dated 1-08-86 is required for Cessna Models 182H, 182J, 182K, 182L and 182M When Modified Per STC SA485SW (WREN Models 460H, 460J, 460K, 460L and 460M) and/or later FAA Approved revisions of the above supplement.

4. FAR Approved Supplemental Flight Manual, P/N 89798, dated 9-27-88 is required for Cessna Model 182G When Modified Per STC SA485SW (WREN Model

460) 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.

17.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) _ (Address of transferee) (Number and streel) (City, Stake, and 21P code) from (Name of grantor) (Print or type) (Address of grantor) (Number and sireel;

(City, Stake, and ZIP code, Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- September 27, 1988: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/95/55/9555555eac115e3fe494a6c7f947b164e1284e9c962172717776dbd4301fbced)

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