# STC SA5319SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC System 40/50 single and two axis automatic flight guidance systems, model ST-243-40/50.
- Applied: May 4, 1984
- Status date: May 10, 1984
- Product: Aircraft, Single-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A26EU](https://openairdocs.org/tcds/A26EU)
- Certificate PDF: https://openairdocs.org/files/sha256/63/d1/63d1fae29698b7d0b6f974fee316f0a21c92bc6a1513731d2093ad236bbee285
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/8F9D09969EAE369885256CC200122858.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA5319SW-D

## ADs that name it (0)

None.

## Approved models (1)

- Cessna Aircraft Company F177RG ([TCDS A26EU](https://openairdocs.org/tcds/A26EU))

## 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.

fiatd £otn of Bcpartmmt rf Transportation— Jfataal atriation administration Supplemental 'Cgpe Certificate SA5319SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, TX 76067 ^^JA&fe'ttcwvn&fitvctt^^ *A*aAt*r*tin4m/frJ&ctai*£ 23 ^of^£n^ Federal <SltaM£a- A26EU

REIMS-CESSNA F177RG Installation of S-TEC System 40/50 Single and Two Axis Automatic Flight Guidance Systems, Model ST-243-40/50, according to Bulletin No. 343, dated 5-01-84 and Master Drawing List No. 92275, dated 5-01-84 and/or later FAA Approved revisions of the above data, (14 Volt System).

1. FAA Approved Supplemental Flight Manual, P/N 89451, dated 5-10-84 is required for Reims-Cessna Model F177RG for S-TEC System 40, and/or later FAA Approved revisions of the above supplement.

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

'&^&0^aA^fc^^&tyM*>va6AA4i&j*€frui4W4rv;ejfl!e^MM&VA &^&e<puMa**dZa0it&A&cv&U'&e' SXdrru*uA/ra£?r-4f.t 5-04-84 5-10-84 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW (Title)

This artijualt may ft* transferrtd in accordance with FAR 21.47.

FJUkfcxM (110-2(10-6*)

finfcti goto of 3atrica Btpartmott rf transportation— jfdcral atriation administration Certificate(Continuation SA5319SW-D Limitations and Conditions (con't)

2. FAA Approved Supplemental Flight Manual, P/N 89456, dated 5-10-84 is required for Reims-Cessna Model F177RG for S-TEC System 50, and/or later FAA Approved revisions of the above supplement.

3. Compatability of this modification with other previously approved modifi cations must be determined by the installer.

Any al!:ration of this certificate is punishable by a fine of not exceeding $1,000, or imprisonment not exceeding 3 years, o; both.

FAA FORM 8110-2-1 (10-69) This certificate may bt transferred in accordance with FAR 21.47.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number .

to (Name of transferee).

(Address of transferee). (Number and street) (City, State, and <JP code) from (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 : 1966 OF —205-579

## Every issue (1)

- May 10, 1984: Issued, Current. [certificate](https://openairdocs.org/files/sha256/63/d1/63d1fae29698b7d0b6f974fee316f0a21c92bc6a1513731d2093ad236bbee285)

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