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 />
10<strong>01</strong>5928 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02064 REV. 1 FAA STC SA7198W-D BEECH 100<br />
Installation of S-TEC Systems 65 Two Axis 1. Also eligible on Models 100, A100 and<br />
17.10.2006<br />
BEECH A100<br />
Automatic Flight Guidance System, Model ST- B1000 when modified per STC SA3828NM<br />
BEECH B100<br />
3<strong>01</strong><br />
(Lower Aft Fuselage Strakes).2. Also eligible<br />
on Model A100 when modified per STC<br />
SA1679SO (750 S.H.P. Engines).3. Airplane<br />
Flight Manual Supplement, P/N 89827S, dated<br />
9-29-89 is<br />
10<strong>01</strong>5996 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02152 FAA STC SA09124AC-D PIPER PA-60-6<strong>01</strong>P<br />
Installation of S-TEC 55/55X two axis 1. According to AFMS, Section 2 Operating<br />
29.08.2006<br />
PIPER PA-60-602P<br />
automatic flight control system in Aerostar Limitation2. Instructions for continued<br />
models<br />
airworthiness acc. Doc. P/N 81319 Rev. 23.<br />
Maintenance Instructions 2.-4. must be<br />
performed every 100 flight hours or once every<br />
calender year, whichever comes first<br />
10<strong>01</strong>6052 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02224 FAA STC SA09262AC-D CESSNA 182Q<br />
CESSNA 182R<br />
CESSNA 182T<br />
Installation of S-TEC System 20/30 Single and<br />
Two Axis Automatic Flight Guidance System,<br />
Model ST-718-20/30 in Cessna 182Q, 182R<br />
and T182, also when modified per STC<br />
SA1382WE (Robertson STOL)<br />
For 182Q the maximum aft c.g. is limited to<br />
46.0 inches aft of datum when autopilot is<br />
installedInstaller must check availability of<br />
<strong>EASA</strong>-approval for Robertson STOL STC No.<br />
when aeroplane is modified per that STC<br />
10<strong>01</strong>6053 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02225 FAA STC SA09218AC-D GRUMMAN GA-7 Installation of S-TEC System 55/55X Two Axis --<br />
Automatic Flight Guidance System, Model ST-<br />
661 in Grumman American GA-7<br />
14.12.2006<br />
10<strong>01</strong>6054 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02226 FAA STC SA09316AC-D CESSNA R182<br />
Installation of S-TEC System 20/30 Single and This STC is approved only for the product<br />
18.12.2006<br />
CESSNA TR182<br />
Two Axis Automatic Flight Guidance System, configuration as defined in the approved design<br />
Model ST-759-20/30 in Cessna R182, and data referred to in the paragraph "Description".<br />
TR182.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
10<strong>01</strong>6080 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02264 FAA STC SA092<strong>01</strong>AC-D CESSNA 172R<br />
Installation of S-TEC System 55/55X Two Axis This STC is approved only for the product<br />
16.<strong>01</strong>.2007<br />
CESSNA 172S<br />
Automatic Flight Guidance System, Model ST- configuration as defined in the approved design<br />
563 in Cessna 172R and 172S<br />
data referred to in the paragraphs "Description"<br />
and “Associated Technical Documentation”.<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined<br />
10<strong>01</strong>6103 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02293 FAA STC SA09160AC-D PIPER PA-32-260<br />
PIPER PA-32-300<br />
PIPER PA-32R-300<br />
10<strong>01</strong>6146 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02347 FAA STC SA09397CA-D PIPER PA-31<br />
PIPER PA-31-300<br />
PIPER PA-31-325<br />
PIPER PA-31-350<br />
Installation of S-TEC System 55/55X Two Axis<br />
Automatic Flight Guidance System, Model ST-<br />
640<br />
Installation of S-TEC System 65 Two Axis<br />
Automatic Flight Guidance System with<br />
Autotrim, Model ST-849, and with Optional<br />
Flight Director/Steering Horizon.<br />
10<strong>01</strong>6175 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02403 FAA STC SA09139AC-D PIPER PA-44-180 Installation of S-TEC Manual Electric Trim<br />
System, Model ST-619, in above mentioned<br />
airplane Type / Variant<br />
10<strong>01</strong>6194 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.02431 FAA STC SA8886SW-D CESSNA 206<br />
CESSNA P206<br />
CESSNA P206A<br />
CESSNA P206D<br />
CESSNA P206E<br />
CESSNA TP206C<br />
CESSNA TP206D<br />
CESSNA TU206B<br />
CESSNA TU206C<br />
CESSNA TU206D<br />
CESSNA TU206E<br />
CESSNA TU206G<br />
CESSNA U206<br />
CESSNA U206B<br />
CESSNA U206C<br />
CESSNA U206D<br />
CESSNA U206E<br />
CESSNA U206F<br />
CESSNA U206G<br />
This STC is also eligible on:- PA-31 and PA-<br />
31-300 when modified per STC SA970SO,-<br />
PA-31-325 when modified per STC<br />
SA00<strong>04</strong>8SE,- PA-31-350 when modified per<br />
STC SA1151SO and / or any of STC<br />
SA5796NW, STC SA0<strong>01</strong>92SE, STC<br />
SA00039SE, STC SA0<strong>01</strong>26SE.I<br />
Prior to installation of this modification the<br />
installer must determine that the<br />
interrelationship between this modification and<br />
any other previously installed modification will<br />
introduce no adverse effect upon the<br />
airworthiness of the product.The installa<br />
Installation of S-TEC System 55/55X Two Axis This STC is also eligible on variants 206, P206,<br />
Automatic Flight Guidance System, Model ST- U206, P206A, TP206A, U206A, TU206A,<br />
556 in above mentioned airplane Types / P206B, TP206B, U206B, TU206B, P206C,<br />
Variants, also when modified per STC as listed TP206C, U206C, TU206C, P206D, TP206D,<br />
in 3.5 (Limitations and Conditions)<br />
U206D, TU206D, P206E, TP206E, U206E,<br />
TU206E, U206F, and TU206F when converted<br />
to 28 Volt electri<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 430/<strong>462</strong><br />
14.12.2006<br />
28.02.2007<br />
23.02.2007<br />
15.06.2007<br />
05.07.2007