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>5557 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>454 REV. 1 FAA STC SA5302SW-D CESSNA 210 Installation of S-TEC System 40/50 Single and 1. As defined in the Limitations and Conditions<br />
09.09.2008<br />
Two Axis Automatic Flight Guidance System, section of FAA STC SA5302SW-D, latest<br />
Model ST-212-40/50, according to Bulletin No approved revision2. Prior to installation of this<br />
312, dated 3-21-88 or later approved revisions modification the installer must determine that<br />
the interrelationship between this modification<br />
andany other previously i<br />
10<strong>01</strong>5558 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>455 REV 1 FAA STC SA09628AC TWIN COMMANDER AIRCRAFT<br />
690C<br />
TWIN COMMANDER AIRCRAFT<br />
690D<br />
TWIN COMMANDER AIRCRAFT<br />
695<br />
TWIN COMMANDER AIRCRAFT<br />
10<strong>01</strong>5559 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>456 FAA STC SA5242SW-D<br />
695A<br />
AERMACCHI F 260 B<br />
AERMACCHI F 260 C<br />
AERMACCHI F 260 D<br />
Installation of S-TEC/Meggitt MAGIC <strong>01</strong>298-07-<br />
<strong>01</strong>-005 Digital Flight Control SystemFAA STC<br />
SA09628AC<br />
10<strong>01</strong>5588 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>499 FAA STC SA09239AC-D CESSNA F172-N Installation of S-TEC System 20/30 Single and<br />
tow Axis Automatic Flight Guidance Systems<br />
10<strong>01</strong>56<strong>04</strong> S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>540 REV. 1 FAA STC SA7209SW-D CESSNA 337D<br />
CESSNA 337E<br />
CESSNA 337F<br />
CESSNA 337G<br />
CESSNA 337H<br />
CESSNA P337H<br />
CESSNA T337D<br />
CESSNA T337E<br />
CESSNA T337F<br />
CESSNA T337G<br />
CESSNA T337H<br />
CESSNA T337H-SP<br />
10<strong>01</strong>5606 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>541 REV. 1 FAA STC SA7210SW-D REIMS AVIATION F-337E<br />
REIMS AVIATION F-337F<br />
REIMS AVIATION F-337G<br />
REIMS AVIATION F-337H<br />
REIMS AVIATION FT-337E<br />
REIMS AVIATION FT-337F<br />
REIMS AVIATION FT-337GP<br />
REIMS AVIATION FT-337HP<br />
10<strong>01</strong>5633 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>589 FAA STC SA7805SW-D PIPER PA-28R-180<br />
PIPER PA-28R-200<br />
PIPER PA-28R-2<strong>01</strong><br />
PIPER PA-28R-2<strong>01</strong>T<br />
10<strong>01</strong>5634 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>590 FAA STC SA7815SW-D PIPER PA-23<br />
PIPER PA-23-160<br />
10<strong>01</strong>5669 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>645 REV 1 FAA STC SA09214AC-D CESSNA 172R<br />
CESSNA 172S<br />
10<strong>01</strong>5783 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.<strong>01</strong>839 FAA STC SA09522AC-D BEECH 95<br />
BEECH B95A<br />
BEECH D95A<br />
BEECH E95<br />
Airplane with S-TEC/Meggit <strong>01</strong>298-07-<strong>01</strong>-005<br />
Digital Flight Control System is prohibited from<br />
flight into known icing condition. STC<br />
SA<strong>01</strong>627CH, Meggit EFIS installation is<br />
required for this modification. Compatibility of<br />
this design with previously approved<br />
Installation of S-TEC System 40/50, Single and 1. Only eligible on model F260B when<br />
Two Axis Automatic Flight Guidance Systems equipped with Aileron Assemblies P/N SF260-<br />
Model ST-235-40/50FAA STC SA5242SW-D 02-05-<strong>01</strong> (L.H.) and P/N SF260-02-05-02<br />
(R.H.)2. This STC is approved only for the<br />
product configuration as defined in the<br />
approved design data referred to in the<br />
paragrap<br />
Installation of S-TEC System 60 Two Axis<br />
Automatic Flight Guidance System with<br />
Optional Autotrim System, Model ST-314,<br />
according toBulletin No 414, dated 3-14-90 or<br />
later approved revision<br />
Installation of S-TEC System 60 Two Axis<br />
Automatic Flight Guidance System with<br />
Optional Autotrim System, Model ST-314,<br />
according toBulletin No 414, dated 3-14-90 or<br />
later approved revisions.<br />
Installation of S-TEC Manual Trim System<br />
(field installation) i.a.w. MDL 92549 Rev A<br />
STC SA7815SW-D, Installation of S-TEC<br />
System 60 Two Axis Automatic Flight<br />
Guidance System, Model ST-486<br />
Installation of S-TEC System 30 ALT Altitude<br />
Hold Sytem, Model ST-673, according to<br />
Bulletin No 773, Revision 4 dated 9-22-98 or<br />
later approved revision<br />
Also eligible on the above models when<br />
modified by 180 HP Engine conversion. <strong>EASA</strong><br />
approval of this STC must be ckecked.This<br />
STC is issued as result of the validation of the<br />
S-TEC Corporation STC No SA09239AC-D<br />
approved by the FAA on June 26, 1997.<br />
1. Eligble when above models are modified per<br />
FAA STC SA1627WE (Robertson STOL<br />
Conversion)2. Eligible when the above models<br />
are modified per FAA STC SA937CE (Horton<br />
STOL Craft Conversion)3. It is the operator's<br />
responsibility to ensure the above mentioned<br />
1. Eligible when the above models are<br />
modified per FAA STC SA1627WE<br />
(Robertson STOL Conversion).2. Eligible<br />
when the above models are modified per FAA<br />
STC SA937CE (Horten STOL Craft<br />
Conversion).3. It is the operators<br />
responsibility to ensure the a<br />
Limited to Installations without the trim monitor<br />
system<br />
1. Eligible on models modified per STC<br />
SA5<strong>04</strong>WE and/or STC SA824WE.2. Eligible<br />
on models modified per STC SA461SW,<br />
SA636SW, SA671SW and 899SW3.<br />
Instructions for continued airworthiness acc.<br />
Doc. P/n 81431 5. Maintenance Instructions 2.-<br />
4. must be performed<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
Installation of S-TEC System 55/55X Two Axis FAA/DAS Approved Pilot’s Operating<br />
Automatic Flight Guidance System, Model ST- Handbook and / or FAA Approved Airplane<br />
898.<br />
Flight Manual Supplement P/N 892113 dated 2-<br />
18-02 or later approved revision, is required for<br />
Beech models 95 and B95.FAA/DAS<br />
Approved Pilot’s Operating Handbook and / or<br />
FAA Approv<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 428/<strong>462</strong><br />
17.10.2006<br />
13.03.2006<br />
<strong>04</strong>.08.2005<br />
12.09.2008<br />
09.09.2008<br />
30.<strong>01</strong>.2006<br />
17.02.2006<br />
10.09.2008<br />
17.10.2006