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>04</strong><strong>04</strong>93 STC TWENTY ONE LIMITED CL-600-2A12 Introduction of Swift Broadband none Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
06.07.2<strong>01</strong>2<br />
10<strong>04</strong>0691 STC TWENTY ONE LIMITED PA-31 Provisions for the installation of a Sensor Turret With a sensor turret installed, flight into known<br />
or forecast icingconditions is<br />
prohibited.Limitations as defined in AFMS<br />
S21.FMS-0091 Issue 1The installation and<br />
subsequent operation of a sensor turret<br />
requires aseparate approval.<br />
Prior to installation of this modification it 19.07.2<strong>01</strong>2<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>04</strong>1363 STC TWENTY ONE LIMITED B757-200/-200PF/-300 Introduction of Antenna Mounting Provision None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
11.09.2<strong>01</strong>2<br />
10<strong>04</strong>1598 STC TWENTY ONE LIMITED BOEING 767-200/-300 Introduction of Iridium Antenna. None. Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
<strong>01</strong>.10.2<strong>01</strong>2<br />
10<strong>01</strong>5317 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.00244 FAA STC SA5321SW-D BOEING 767-300ER Reconfiguration of passenger cabin interior 1. Subject to compliance with the provisions<br />
from 2<strong>04</strong> passengers to 250 passengers in of Part 21 Subpart E, this STC and associated<br />
accordance with DER Services Inc. Master data shall remain valid until surrendered,<br />
Document List (MDL) Report No. MDL-A20<strong>04</strong>- withdrawn or otherwise terminated.2. If<br />
026-1 dated 15 June 20<strong>04</strong>, or later <strong>EASA</strong> transfer of this Certificate is requested under<br />
approved revisions<br />
Part 21A.116, the STC will<br />
10<strong>01</strong>5320 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.00268 REV. 1 FAA STC SA09290AC-D PIPER PA-32-260<br />
PIPER PA-32-300<br />
10<strong>01</strong>5321 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.00269 REV. 2 FAA STC SA8906SW-D PA-28-151, PA-28-161<br />
PA-28-181, PA-28-2<strong>01</strong>T<br />
PA-28-236<br />
10<strong>01</strong>5326 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.00281 REV. 1 FAA STC SA09386AC-D GRUMMAN AA-5<br />
GRUMMAN AA-5A<br />
GRUMMAN AA-5B<br />
Installation of S-TEC System 20/30 Single Axis 1. Subject to compliance with the provisions<br />
and Two Axis Automatic Flight Guidance of Part 21 Subpart E, this STC and associated<br />
Systems Model ST-733-20/30 SA09290AC-D. data shall remain valid until surrended,<br />
withdrawn or otherwise terminated2. If<br />
transfer of this Certificate is requested under<br />
Part 21A.116 the STC will be re<br />
Installation of S-TEC System 55/55X Two Axis<br />
Automatic Flight GuidanceSystem Model ST-<br />
568.<br />
Installation of S-TEC System 30 Single and<br />
Two Axis Automatic Flight Guidance System,<br />
Model ST-840-30, FAA STC SA09386AC-D<br />
14.10.20<strong>04</strong><br />
10.09.2008<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
interrelationship between this modification<br />
and any other previouslyinstalled<br />
modification and/ or repair will introduce<br />
no adverse effectupon the airworthiness<br />
of the product<br />
14.09.2<strong>01</strong>0<br />
1. Subject to compliance with the provisions of<br />
Part 21 Subpart E, this STC and associated<br />
data shall remain valid until surrendered,<br />
withdrawn or otherwise terminated.2. If transfer<br />
of this certificate is requested under Part<br />
21A.116, the STC will be reis<br />
10<strong>01</strong>5327 S-TEC CORPORATION <strong>EASA</strong>.IM.A.S.00289 FAA STC SA09264AC-D CESSNA F182-Q Installation of S-TEC System 30 Two Axis 1. <strong>EASA</strong> Approved Pilot's Operating<br />
Automatic Flight Guidance System, Model ST- Handbook and/or Airplane Flight Manual<br />
718/30, according to Bulletin No. 818, dated Supplement, dated October 21, 20<strong>04</strong> is<br />
July 30, 1997 and Master Drawing List No. required for Reims-Cessna Model F182Q for S-<br />
921<strong>01</strong>6, dated July 30, 1997 or later FAA TEC System 30 or later <strong>EASA</strong> approved<br />
approved revisions of the above data (28 Vol revisions of the above supplement.2.<br />
Compatibility of<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 426/<strong>462</strong><br />
11.09.2008<br />
28.10.20<strong>04</strong>
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