# STC SA7208SW-D

- Type: Supplemental type certificate
- Status: Current, Issued
- Holder: S-TEC Corporation, United States
- Description: Installation of S-TEC system 65 two axis automatic flight guidance system, Model ST-313.
- Applied: February 7, 1990
- Status date: February 27, 1990
- Product: Aircraft, Small Multi-Engine
- Certification basis: Part 21
- Data sheets: [TCDS A6CE](https://openairdocs.org/tcds/A6CE), [TCDS A23EU](https://openairdocs.org/tcds/A23EU)
- Certificate PDF: https://openairdocs.org/files/sha256/18/3d/183dc9c48e8b2912337be37afb32e673f2a24febe4a1083d9789adfd135d54b0
- FAA DRS: https://drs.faa.gov/browse/excelExternalWindow/ED075D292C21442085256CC20056A209.0001
- DRS record last changed: December 6, 2025
- Page: https://openairdocs.org/stc/SA7208SW-D

## ADs that name it (0)

None.

## Approved models (11)

- Reims Aviation S.A. F337E ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- Reims Aviation S.A. F337F ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- Reims Aviation S.A. F337G ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- Reims Aviation S.A. F337H ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- Reims Aviation S.A. FT337E ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- Reims Aviation S.A. FT337F ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- Reims Aviation S.A. FT337GP ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- Reims Aviation S.A. FT337HP ([TCDS A23EU](https://openairdocs.org/tcds/A23EU))
- The Cessna Aircraft Company 337F ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- The Cessna Aircraft Company 337G ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))
- The Cessna Aircraft Company 337H ([TCDS A6CE](https://openairdocs.org/tcds/A6CE))

## 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.

Corrected Copy Uritri gtatn rf arnica Btpartmtnt of Transportation —jfttoal attation administration Supplemental t^pc Certificate SA7208SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 >*'u£i*^£'i^«z£it^ «^A^^^<^^~t^A^^>^^ 23 j/J&*< Federal Aviation A23EU Reims Aviation S.A.

F337E, FT337E, F337F, FT337F, F337G, FT337GP, Installation of S-TEC System 65 Two Axis Automatic Flight Guidance System, Model ST-313, according to Bulletin No. 413, Revision 1, dated 2-06-90 and Master Drawing List No. 92497, Revision A, dated 2-06-90 and/or later FAA Approved revisions of the above data (28 Volt System).

1. Also eligible on the above models when modified per STC SA937CE (Norton STOL Craft Conversion) .

2. Also eligible on the above models when modified per STC SA1627WE (Robertson STOL Conversion) .

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

*?& JSa 2-07-90 2-27-90 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SM

This tertificatt ma) bf tramferrtJ in ttitirilana with FAR 21.17.

fAA Pow II10-1 (I0-*»|

Corrected Copy ttnitrd £tatts of 3mtnra Bepartmcnt of transportation— federal a&iation administration Supplemental H$$t Certificate(Continuation £hett) SA7208SW-D Limitations and Conditions (con't.)

3. FAA/DAS Approved Supplemental Flight Manual, P/N 89843, dated 2-27-90 is required for Reims Aviation S.A. Models F337E, FT337E, F337F, FT337F, F337G, FT337GP, F337H and FT337HP When Modified Per STC SA1627WE (Rpbertson STOL Conversion) and/or later FAA Approved revisions of the above supplement.

4. FAA/DAS Approved Supplemental Flight Manual, P/N 89844, dated 2-27-90 is required for Reims Aviation S.A. Models F337E, FT337E, F337F, FT337F, F337G, FT337GP, F337H and FT337HP And The Above Models When Modified Per STC SA937CE (Horton STOL Craft Conversion) 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.

A ni alteration nf this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or hii/h.

FAA FORM aiio-2-1 do-69) This ctrtijicate may be liamjerrtd in accordance with I-'AR .'!.->' PAGE 2 OF 2 PAGES

INSTRUCTIONS : The transfer endorsement below may be used to notify the appropriate FAA Regional Office of the transfer of this Supplemental Type Certificate.

The FAA will reissue the certificate in the name of the transferre and forward it to him.

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (%(ame of transferee) (Address of transferee) CXymber and strut) (City, State, atufZlf codt) from (9{ame. of grantor) ('Print or type) (Address of grantor) (yJumBer ami street) (City, State, andZlT code.)

Exent of Authority (if licensing agreement) :

Signature of grantor (In infy : _ __ _ Page 2 of 2

## Every issue (1)

- February 27, 1990: Issued, Current. [certificate](https://openairdocs.org/files/sha256/18/3d/183dc9c48e8b2912337be37afb32e673f2a24febe4a1083d9789adfd135d54b0)

---
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.