What it approves
Installation of S-TEC system 60 two axis automatic flight guidance system w/optional autotrim system, Model ST-314.
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.
Btpartmcnt of transportation—Jfcdoral SlDiadon administration Supplemental 'Cgpe Certificate tSUvmwt" SA7210SW-D S-TEC Corporation Rt. 4, Bldg. 946 Wolters Industrial Complex Mineral Wells, Texas 76067 J^^^.^^ K>T&^ 23 y^ Federal Aviation rat A23EU Reims Aviation S.A.
F337E, FT337E, F337F, FT337F, F337G, FT337GP, F337H, FT337HP Installation of S-TEC System 60 Two Axis Automatic Flight Guidance System w/Optional Autotrim System, Model ST-314, according to Bulletin No. 414, dated 3-14-90 and Master Drawing List No. 92503, dated 3-14-90 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 (Horton STOL Craft Conversion).
2. Also eligible on the above models when modified per STC SA1627WE (Robertson STOL Conversion).
£.a^.^i!ii^ 3-16-90 4-06-90 (Signature) Harold W. Holdeman DAS Staff Coordinator, DAS 5 SW ——————(Tit(e)
TAu certificate may tt traraferrtd in accvrdana with FAR 21.17.
»AA re** ino-j (io-»»)
Hmtrd £tatra of amtrira Bepartment of transportation— federal aviation administration Supplemental lEgpe Certificate(Continuation £hcet) SA7210SW-D Limitations and Conditions (con't.)
3. FAA/DAS Approved Supplemental Flight Manual, P/N 89847, dated 4-06-90 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.
4. FAA/DAS Approved Supplemental Flight Manual, P/N 89848, dated 4-06-90 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 (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.
Atir nitfratiim of this certificate is punishable by a fine of not exceeding SI,000, or imprisonment not exceeding 3 years, or both.
<-AA FORM 8HO-2-I (10-69) This ccrtiftatt may ki iransjrrrtd in accordance with FAR -7.-/7 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 Ctymt of transferee) (Address of transferee) _ (y&anier and street) (City, State, andZlf code) of grantor) (Print or type) (Adifress of grantor) (J&anBer and street) (City, State, andZlf code) Exent of Authority (if licensing agreement) :
Signature of grantor (In inQ : _ Page 2 of 2
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.