# STC SA4444SW

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC system 60 pitch stabilization system, Model ST-048 with optional autotrim system.
- Status date: August 13, 1981
- Data sheets: 3A13, 3A13
- Certificate PDF: https://openairdocs.org/files/sha256/7f/6e/7f6e5310553e52f5b24edac60d37a26c2d04f2c2ff09db7ed3137e287e320963
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/042F1EA4DF05560385256CC2000E3C81.0001
- Page: https://openairdocs.org/stc/SA4444SW

## ADs that name it

None.

## Approved models (2)

- Cessna Aircraft Company 182Q (TCDS 3A13)
- Cessna Aircraft Company 182R (TCDS 3A13)

## 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 States of America Bepartment of tonsportation— federal 2toiation administration Supplemental Ttgpe Certificate SA4444SW Project A5373SW-DS FKP-213S-TEC Corporation Rt. 3, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 ^J'W^fte'dedjicvwfw^fo^c&oivvi^fiM^^ .<yk*^<«^^^ Civil Air 3A13 Cessna 182Q, 182R . Installation of S-TEC System 60 Pitch Stabilization System, Model ST-048 with Optional Autotrim System according to Bulletin No. 151, dated 7-27-81 and Master Drawing List No. 9263, dated 7-27-81, or later FAA approved revision. (28 Volt System) See Continuation Sheet, page 2 of this STC.

July 27, 1981 August 13, 1981 . Watson (Sismture) Chief, Engineering and Manufacturing Branch (Title) ~~~~~~

**FAA FORM 81 10-2(10-68)**

United States of America Bcpartmcnt of Transportation— federal atriation autministtation Supplemental ¥j)pe Certificate(Continuation 3hect) SAA444SW Limitations and Conditions:

1. Supplemental Flight Manual FAA Approved P/N 8964 dated August 13, 1981, is required for Cessna Models 1820, S/N 18266590 and Below with S-TEC System 60 Pitch Stabilization System (28 Volt System).

2. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement FAA Approved P/N 8976 dated August 13, 1981, is required for Cessna Model 1820, S/N 18266591 and up with S-TEC System 60 Pitch Stabilization System (28 Volt System).

3. Pilot's Operating Handbook and FAA Approved Airplane Flight Manual Supplement FAA Approved P/N 8967 dated August 13, 1981, is required for Cessna Hodal 182R with S-TEC System 60 Pitch Stabilization System (28 Volt System).

i. Compatibility of this modification with other previously approved modifications mist be determined by the installer.

**FAA FORM 8HO-2-1 (10-69) PAGE 2 OF 2 PAGES**

## Every issue (1)

- August 13, 1981: Issued, Current. [certificate](https://openairdocs.org/files/sha256/7f/6e/7f6e5310553e52f5b24edac60d37a26c2d04f2c2ff09db7ed3137e287e320963)

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From OpenAirDocs.org, an independent open copy of FAA data. Only the Federal Register edition on govinfo.gov is the official legal text of an AD.