# STC SA5334SW-D

- Type: Supplemental type certificate
- Status: Current, Reissued
- Holder: S-TEC Corporation
- Description: Installation of S-TEC System 60 two axis flight guidance system Model ST-241, with optional automatic electric trim system.
- Status date: March 10, 1989
- Data sheets: A20CE
- Certificate PDF: https://openairdocs.org/files/sha256/5f/21/5f21569fb06e03378272befee5426c07e6693e8fb35207150c4a519e440a9ac1
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/E8D27EB5E2B0A6D385256CC200122873.0001
- Page: https://openairdocs.org/stc/SA5334SW-D

## ADs that name it

None.

## Approved models (1)

- Cessna Aircraft Company 177RG (TCDS A20CE)

## 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.

Starts or arnica Bcpartmtnt of Itonsportation—Jpcdcral 2toiation administration Supplemental 'Cgpe Certificate tSbU'mvW' SA5334SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 J^Jfafe -<iifi^yi^^<>*&n'jrnee&^fo^aiv'^^ 23 -<«^£E- Federal Air ^sleoMCa&<mA/.

A20CE Cessna 177RG Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System, Model ST-241, with Optional Automatic Electric Trim System, according to Bulletin No. 341, Revision 1, dated 2-15-89 and Master Drawing List No. 92286, Revision A, dated 2-15-89 and/or later FAA Approved revisions of the above data (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89512, dated 9-04-84 is required for Cessna Model 177RG, S/N 177RG0787 and Below and/or later FAA Approved revisions of the above supplement.

2. FAA Approved Supplemental Flight Manual, P/N 89512-1, dated 3-10-89 is required for Cessna Model 177RG, S/N 177RG0787 and Below and/or later FAA Approved revisions of the above supplement.

XSee Continuation Sheet, Page 2, a part of this STC.)i£^x*^<<^&<z<^z*t^i<(^i<^4^^«>7««!^^ &VLintMs^ S$£vmvrwJi-foa&>r'^> &i& 8-29-84 L^^^u^/. 3-10-89, Revision 1 9-04-84 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (TitU)

FAA FO«M 8110-2 (10-68)

tinted Skua of amenta Btparrmcnt of ^transportation— Jfderal atriation administration Supplemental HDgpc Certificate(Continuation £heet) SA5334SW-D, Revision 1 Limitations and Conditions (con't.)

3. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89513, dated 9-04-84 is required for Cessna Model 177RG, S/N 177RG0788 through S/N 177RG1266 and/or later FAA Approved revisions of the above supplement.

4. FAA Approved Supplement to Pilot's Operating Handbook and/or FAA Approved Airplane Flight Manual, P/N 89513-1, dated 3-10-89 is required for Cessna Model 177RG, S/N 177RG0788 through S/N 177RG1266 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.

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

FAA FORM 8110-2-1 (10-69) This certificate may be transferred in accordance with FAR i'1.47 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, Stale, and ZJP code) from (Name of grantor) (Print or type) (Address of grantor) (Number and street) (City, Stale, and ^IP code) Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

US. GOVERNMENT PRINTING OFFICE : 1966 OF —205-579

## Every issue (1)

- March 10, 1989: Reissued, Current. [certificate](https://openairdocs.org/files/sha256/5f/21/5f21569fb06e03378272befee5426c07e6693e8fb35207150c4a519e440a9ac1)

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