STC SA7809SW-D

Supplemental type certificate · S-TEC Corporation

Holder
S-TEC Corporation · United States
Status
Current · Issued
Status date
December 10, 1991
Applied
November 25, 1991
Product
Aircraft · Small Multi-Engine
Certification basis
Part 21
Data sheet
TCDSA23EU

From FAA DRS, with our copy of the certificate PDF. DRS record last changed December 5, 2025.

What it approves

Installation of S-TEC System 60 pitch stabilization system, Model ST-478, with optional automatic electric trim system.

What the certificate says

From the PDF’s text layer, without the form’s printed wording. Layout and order may differ; the PDF is the record.

Btpartrarnt of transportation—Jfotaal atnation administration Supplemental "Cgpe Certificate i/u4rrwe>*' SA7809SW-D S-TEC Corporation 946 Pegram Wolters Industrial Park Mineral Wells, Texas 76067 *AA.*«f<,.»~n~*fA*fzz*i«[ 23 V^ Federal Aviation A23EU REIMS AVIATION S.A.

F337E, FT337E, F337F, FT337F, F337G, FT337GP, Installation of S-TEC System 60 Pitch Stabilization System, Model ST-478, with Optional Automatic Electric Trim System, according to Bulletin No. 578, dated 11-21-91 and Master Drawing List No. 92553, dated 11-21-91 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 (Horton 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.)<«i>£^^W-^»^ f^s William J. Thomas DAS Staff Coordinator. DAS 5 SW (THU)

nit tertijieate may Ar troiufmid in ucatdanu until FAR 21.17.

ttrarni Scam of antnra Bcpartmcnt of Transportation— Jfedtral 3Wation Administration Certificate (Continuation Sheet) SA7809SW-D Limitations and Conditions (con't.)

3. FAA/DAS Approved Supplemental Flight Manual, P/N 89952, dated 12-10-91 is required for Reims Aviation S.A. Models F337E, FT337E, F337F, FT337F, F3376, FT337GP, F337H, and FT337HP And The Above Models When Modified Per STC SA937CE (Norton STOL Craft Conversion) and/or later FAA Approved revisions of the above supplement.

4. FAA/DAS Approved Supplemental Flight Manual, P/N 89953, dated 12-10-91 is required for Reims Aviation S.A. Models F337E, FT337E, F337F, FT337F, F337G, FT337GP, F337H, and FT337HP When Modified Per STC SA1627WE (Robertson STOL Conversion) and/or later FAA Approved revisions of the above supplement.

5. Compatibility of this modification with other previously approved modifications must be determined by the installer.

alteration of thu certificate is punishable by a fine of not exceeding 11,000, or imprisonment not exceeding 3 years, or hnth.

FORM siiu-2-1 (to.a» Thu etrttfeatt may hi trant/errtd m oaorJanti with 1~.\H .'/.V* PAGE 2 Of 2 PAGES

INSTRUCTIONS: The transfer endorsemeni 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 Ihc name of the transferee and forward it to him

TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and £1P code) from (Name of grantor) (Print or type) (Address of grantor) itntkfr ami street) ( ('.lit. Slnle. and ^1T rode I Extent of Authority (if licensing agreement):

Signature of grantor (In ink):

ADs that name this STC · 0

An AD can apply because an STC is installed, or mention one in its text.

No AD in this release names this STC

Approved models · 8

MakeModelData sheet
Reims Aviation S.A.F337EA23EU
Reims Aviation S.A.F337FA23EU
Reims Aviation S.A.F337GA23EU
Reims Aviation S.A.F337HA23EU
Reims Aviation S.A.FT337EA23EU
Reims Aviation S.A.FT337FA23EU
Reims Aviation S.A.FT337GPA23EU
Reims Aviation S.A.FT337HPA23EU