# STC SA5264SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 60 two axis automatic flight guidance system Model ST-011 with optional automatic electric trim system
- Applied: November 4, 1983
- Status date: August 12, 1986
- Product: Aircraft, Small Airplane
- Certification basis: Part 21
- Data sheets: [TCDS A42EU](https://openairdocs.org/tcds/A42EU)
- Certificate PDF: https://openairdocs.org/files/sha256/93/4d/934df2e4ff59e0b374317e8518dc3296aefc24589e88411c4af8e0851ebd8d33
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/1A14D5D34697937E86257ECB004F66B9.0001
- DRS record last changed: December 5, 2025
- Page: https://openairdocs.org/stc/SA5264SW-D

## ADs that name it (0)

None.

## Approved models (2)

- Cessna Aircraft Company F182P ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))
- Cessna Aircraft Company F182Q ([TCDS A42EU](https://openairdocs.org/tcds/A42EU))

## 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.

ttmtri gtatti of antnta

•Department of transportation — Jftdcral atnation administration Supplemental 'Cgpe Certificate SA5264SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 no* fati /i*&AtJ^n A-42EU

REIMS-CESSNA F182P AND F182Q ClVll Air jy-1/yfit _/ -eAtgn ~(:2sia-nja4< .' Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-011, with Optional Automatic Electric Trim System, according to Bulletin No.

Ill, Revision 8, dated 6-10-86 and Master Drawing List No. 9216, Revision H, dated 6-10-86 and/or later FAA Approved revisions of the above data (14 Volt System)

1. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89360, dated 1-20-84 is required for Reims-Cessna Models F182P and F182Q and/or later FAA Approved revisions of the above supplement.

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

Sxdmi>n*&6r<i<£(*r-jid>4n& 11-04-83 1-20-84 8-12-86, Revision 1 ( Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Tttu)————————

Tkii arttjuate may bt Iraiufmtd in accordant with FAR 21.17.

FAA FCMM »110-2 (1O-««)

United $tatts of America Bepartment of ^Transportation— federal aoiation administration Supplemental l^pe Certificate(Continuation &heet) SA5264SW-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 89360-1, dated 8-12-86 is required for Reims-Cessna Models F182P and F182Q 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.

Am alteration of this certificate is punishable by a fine of not exceeding Si,000, or imprisonment not exceeding 3 years, or holh FAA FORM 8110-2-1 (10-69) This certificate may be transferred in accordance with 1'AK »/.•// PAGE2 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, Stale, and <?/> code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

## Every issue (1)

- August 12, 1986: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/93/4d/934df2e4ff59e0b374317e8518dc3296aefc24589e88411c4af8e0851ebd8d33)

---
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.