04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
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<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10029937 S-TEC CORPORATION FAA STC SA09140AC-D 210, 210A, 210B, 210C Installation of S-TEC System 55/55X Two Axis None The installation of this modification by <strong>04</strong>.05.2<strong>01</strong>0<br />
Automatic Flight GuidanceSystem, Model ST-<br />
third persons is subject towritten<br />
621 (14 Volt System)<br />
permission of the approval holder and<br />
disposal of the approvedappropriate<br />
documentation. Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
10032286 S-TEC CORPORATION FAA STC SA8910SW-D BEECH S35, V35, V35A AND Installation of S-TEC System 55/55X Two Axis This STC is also eligible on Beech models The installation of this modification by 22.10.2<strong>01</strong>0<br />
V35B<br />
Automatic Flight GuidanceSystem, Model ST- S35, V35, V35A, and V35B whenmodified by third persons is subject towritten<br />
577 (14 Volt System)<br />
STC SA1035WE (turbocharged engine) or permission of the approval holder and<br />
STC SA5223NM (turbonormalizing system) disposal of the approvedappropriate<br />
and any combination of the following STCs: documentation.Prior to installation of this<br />
STCSA09074SC (vortex generators), STC modification it must be determined<br />
SA4-1629 (tip<br />
thatthe interrelationship b<br />
10032336 S-TEC CORPORATION FAA STC SA09320AC-D CESSNA F182P, F182Q Installation of S-TEC System 20/30 Single and This STC is also eligible on Cessna models The installation of this modification by 28.10.2<strong>01</strong>0<br />
Two Axis Automatic FlightGuidance Systems, F182P and F182Q when modifiedby: 1. STC third persons is subject towritten<br />
Model ST-762-20/30 (14 Volt System) SA485SW (Wren conversion) and STC permission of the approval holder and<br />
SA3825SW (260 H.P. engineconversion) or 2. disposal of the approvedappropriate<br />
STC SA950CE (Horton STOL) and/or STC documentation.Prior to installation of this<br />
SA2285CE (Hortonflap gap seals) and STC modification it must be determined<br />
SA3825SW (260 H.P.<br />
thatthe interrelationship b<br />
10032443 S-TEC CORPORATION FAA STC SA7818SW-D 35-C33, F33C Installation of S-TEC System 40/50 Single and none Compatibility of this modification with 08.11.2<strong>01</strong>0<br />
Two Axis Automatic FlightGuidance Systems,<br />
other previously approvedmodifications<br />
Model ST-492-40/50 (28 Volt System)<br />
must be determined by the installer.Prior<br />
to installation of this modification it must<br />
be determined thatthe interrelationship<br />
between this modification and any other<br />
previously<br />
10032444 S-TEC CORPORATION FAA STC SA7819SW-D 35-C33, F33C Installation of S-TEC Manual Electric Trim none Compatibility of this modification with 08.11.2<strong>01</strong>0<br />
System, Model ST-493 (28 VoltSystem)<br />
other previously approvedmodifications<br />
must be determined by the installer.Prior<br />
to installation of this modification it must<br />
be determined thatthe interrelationship<br />
between this modification and any other<br />
previously<br />
10033463 S-TEC CORPORATION FAA STC SA84<strong>01</strong>SW-D TB9, TB10, TB20, TB21, TB200 Installation of S-TEC System 55/55X Two Axis Optional Autotrim System not eligible on If the holder agrees to permit another 24.<strong>01</strong>.2<strong>01</strong>1<br />
Automatic Flight GuidanceSystem, Model ST- Socata model TB 9, TB 10, andTB 200 (Group person to use this certificate toalter the<br />
547 (28 Volt System)<br />
Aerospatiale)<br />
product, the holder shall give the other<br />
person writtenevidence of that<br />
permission. Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship<br />
10033582 S-TEC CORPORATION FAA STC SA5210SW-D H35, J35, K35, M35, N35, P35 Installation of S-TEC 40/50 Single and Two None The installation of this modification by 28.<strong>01</strong>.2<strong>01</strong>1<br />
Axis Automatic FlightGuidance Systems, Model<br />
third persons is subject towritten<br />
ST-188-40/50 (14V - System)<br />
permission of the approval holder and<br />
disposal of the approvedappropriate<br />
documentation.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship b<br />
10033820 S-TEC CORPORATION FAA STC SA09285AC-D PA-31-350<br />
Installation of S-TEC 20/30 Single and Two This STC is also eligible on models PA-31 and The installation of this modification by 10.02.2<strong>01</strong>1<br />
PA-31, PA-31-300, PA-31-325 Axis Automatic FlightGuidance Systems, Model PA-31-300 when modifiedper FAA STC third persons is subject towritten<br />
ST-727-20/30 (28V - System)<br />
SA970SO (350 H.P. Colemill Conversion) This permission of the approval holder and<br />
STC is also eligible on model PA-31-325 when disposal of the approvedappropriate<br />
modified per FAA STCSA00<strong>04</strong>8SE (Vortex documentation. Prior to installation of this<br />
Generator System) This STC is also eligible on modification it must be determined<br />
m<br />
thatthe interrelationship<br />
10038328 S-TEC CORPORATION FAA STC SA8392SW-D PA-32-3<strong>01</strong>, PA-32-3<strong>01</strong>T<br />
Installation of S-TEC system 55/55X Two Axis Installer must check availability of <strong>EASA</strong>- The installation of this modification by 07.02.2<strong>01</strong>2<br />
PA-32R-3<strong>01</strong>, PA-32R-3<strong>01</strong>T Automatic Flight GuidanceSystems, Model ST- approval for one or morereferenced STC when third persons is subject towritten<br />
534 (14V - System).<br />
airplane is modified per that / those STC(s) permission of the approval holder and<br />
disposal of the approvedappropriate<br />
documentation.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship b<br />
10038425 S-TEC CORPORATION FAA STC SA09307AC-D 4<strong>01</strong>/4<strong>01</strong>A/4<strong>01</strong>B/402A/402B/402C Installation of S-TEC system 20/30 single and Installer must check availability of <strong>EASA</strong>- The installation of this modification by 15.02.2<strong>01</strong>2<br />
two axis Automatic FlightGuidance Systems. approval for one or morereferenced STC when third persons is subject towritten<br />
Installation Model ST-743 (28V - System) airplane is modified per that / those STC(s) permission of the approval holder and<br />
according tobulletin N. 843.<br />
disposal of the approvedappropriate<br />
documentation.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship b<br />
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