What it approves
Installation of S-TEC System 55 Two Axis Automatic Flight Guidance System, Model ST-603
What the certificate saysOCR
This is OCR from the scanned FAA certificate. OCR can misread letters and numbers.
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA09121AC-D I his Certifiente isned te S-TEC Corporation One S-TEC Way Mineral Wells Municipal Airport Mineral Wells, TX 76067-9236 9 at 23 of the Federal & viation Regulutions.
Original Product F ype Certifieute A umber: A23EU Al ate : Reims Aviation S.A.
Model: F337E, FT337E, F337F, FT337F, F337G, FT337GP, F337H, FT337HP Description of Type Design Change:
Installation of S-TEC System 55/55X Two Axis Automatic Flight Guidance System, Model ST-603, according to Bulletin No. 703, Revision 2, dated 4-19-01 and Master Drawing List No. 92806, Revision B, dated 4-19-01 or later FAA Approved revisions of the above data (28 Volt System).
(See Continuation Sheet, Page 2, a part of this STC.)
If the holder agrees to permit another person to use this certificate to alter the product, the holder shall give the other person written evidence of that permission.
Date of Application: 9-21-95 Late wissued:
Date of Issuance: 9-29-95 Date Amended: 4-19-01 By chinction of the iS deinstrator FEDERAL AVIATION milk (Signature) TOMINSTRATO Michael Keirnan DAS Staff Coordinator, DAS 5 SW (Title)
FAA Porm 8110-2 (10-68) Page 1 of 2
TRANSFER ENDORSEMENT Transfer the ownership of Supplemental Type Certificate Number to (Name of transferee) (Address of transferee) (Number and street) (City, State, and ZIP code) from (Name of grantor) (Print or type) (Address of grantor) (Number & street) (City, State, and ZIP code) Extent of Authority (if licensing agreement):
Signature of grantor (In ink):
United States of America Department of Transportation Federal Aviation Administration Supplemental Type Certificate Number: SA09121AC-D Limitations and Conditions: (con't.)
1. Also eligible on The Above Models When Modified Per STC SA937CE (Horton STOL Craft Conversion).
Also eligible on The Above Models When Modified Per STC SA1627WE (Robertson STOL Conversion).
FAA/DAS Approved Supplemental Flight Manual, P/N 891200, dated 9-29-95 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) or later FAA Approved revisions of the above supplement.
4. FAA/DAS Approved Supplemental Flight Manual, P/N 891201, dated 9-29-95 is required for Reims Aviation S.A. Models F337E, FT337E, F337F, FT337F, F337G, FT337G, F337H, and FT337HP And The Above Models When Modified Per STC SA937CE (Horton STOL Craft Conversion) or later FAA Approved revisions of the above supplement.
5. FAA/DAS Approved Supplemental Flight Manual, P/N 891200, Revision 1, dated 4-19-01 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) for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.
6. FAA/DAS Approved Supplemental Flight Manual, P/N 891201, Revision 1, dated 4-19-01 is required for Reims Aviation S.A. models F337E, FT337E, F337F, FT337F, F337G, FT337G, F337H, and FT337HP and the above models when modified per STC SA937CE (Horton STOL Craft Conversion) for S-TEC System 55/55X or later FAA Approved revisions of the above supplement.
Compatibility of this modification with other previously approved modifications must be determined by the installer.
ADs that name this STC · 0
An AD can apply because an STC is installed, or mention one in its text.