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>5202 SCHERDEL ENGINEERING Ltd. <strong>EASA</strong>.A.S.03599 SCHEMPP CIRRUS Standard Cirrus: Weight of nonlifting parts Prior to installation of this modification the<br />
02.10.2008<br />
increase with winglets.Doc. No. 07-278-005, installer must determine that the<br />
rev. 2.Doc. No. 07-278-006, rev. 3<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 install<br />
1003<strong>04</strong>20 SCHERDEL ENGINEERING Ltd. ASK 21, ASK 21 MI ASK 21 Front Instrument Panel Modification -<br />
Modification of the ASK 21front seat instrument<br />
panel to allow more leg space for the pilot<br />
None None 15.06.2<strong>01</strong>0<br />
10038786 SCHERDEL ENGINEERING Ltd. 1. DUO DISCUS, 2. DISCUS A<br />
3. DISCUS BT, 4. DUO DISCUS T<br />
5. NIMBUS 4M, 6. VENTUS A<br />
7. STANDARD CIRRUS<br />
8. VENTUS BT, 9. CIRRUS<br />
10<strong>01</strong>5763 SEAPLANES WEST INC. <strong>EASA</strong>.IM.A.S.<strong>01</strong>799 TCCA STC SA<strong>04</strong>-63 CESSNA 182E<br />
CESSNA 182F<br />
CESSNA 182G<br />
CESSNA 182H<br />
CESSNA 182J<br />
CESSNA 182K<br />
CESSNA 182L<br />
CESSNA 182M<br />
CESSNA 182N<br />
CESSNA 182P<br />
CESSNA 182Q<br />
CESSNA 182R<br />
10027470 SECURAPLANE TECHNOLOGIES, Inc. P-<br />
<strong>EASA</strong>.IM.A.S.03268<br />
FAA STC ST<strong>01</strong>809LA SEE APPROVED MODEL LIST<br />
(AML)<br />
10038222 SECURAPLANE TECHNOLOGIES, INC. FAA STC SA<strong>01</strong>696LA SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
Cockpit Ventilation Modification 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 />
14.03.2<strong>01</strong>2<br />
Installation of Aerocet 3400 Amphibious Float<br />
Conversion.<br />
Installation of Hawker 975W0640 Sealed Lead<br />
Acid Battery<br />
1. This STC confers no Operational<br />
Approval, that must be sought from the<br />
National Airworthiness Authority of the country<br />
of registration.2. This STC is approved only<br />
for the product configuration as defined in the<br />
approved design data referred to in<br />
17.07.2006<br />
This approval is limited to those aircraft listed in 1) Prior to installation of this modification 05.10.2009<br />
the AML andequipped with lead acid battery. the installer mustdetermine that the<br />
interrelationship between this modification<br />
and anyother previously installed<br />
modification will introduce no adverse<br />
effectupon the airworthiness of the<br />
product. 2) The inst<br />
Installation of Hawker Part Number<br />
None Prior to installation of this modification it 30.<strong>01</strong>.2<strong>01</strong>2<br />
9750W0370 or 9750W0370-8 Series24Volt 43<br />
must be determined thatthe<br />
Ah Sealed Lead Acid Battery.<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>01</strong>3938 SEFA <strong>EASA</strong>.A.S.00352 REV. 1 BEECH B200 - Installation of calibration workbench ref. 1. Applicable only for F-GJFA s/n BB-1270, F-<br />
STNA "Margouillat1" according to the 02-11<strong>04</strong>- GJFC s/n BB-1347 and F-GJFE s/n BB1399<br />
DIR document.- Installation of calibration aircraft.2. Prior to installation of this<br />
workbench ref. STNA "Margouillat1".Revision modification the installer must determine that<br />
1: Extension of STC <strong>EASA</strong>.A.S.00352 with a the interrelationship between this modification<br />
minor change to another aircraf<br />
and any other previously inst<br />
10<strong>01</strong>4362 SEGELFLUGGRUPPE SIEMENS<br />
MUENCHEN<br />
<strong>EASA</strong>.A.S.<strong>01</strong>629 DIAMOND HK 36 TC Optional operation with skis instead of wheels<br />
in winterOne piece for serial-number 36730<br />
10039286 SEGINUS Inc. FAA STC ST02954CH BN2A-8/-9/-20/-21/-26/-27<br />
BN2B-20/-21/-26/-27<br />
BN2T/-4R/-4S<br />
Installation of a replacement pitot static probe<br />
P/N DU130-24 inaccordance with FAA STC<br />
ST02954CH.<br />
10<strong>01</strong>4058 SELL GmbH <strong>EASA</strong>.A.S.<strong>01</strong>142 BOEING 767-300 Replacement of galley G3A P/N1<strong>01</strong>60F23-<br />
00000with a new galley P/N 1<strong>01</strong>60F23A00000<br />
designed by Sell GmbHaccording to Sell<br />
Engineering Order Doc. No. EO WA 151<strong>04</strong>3,<br />
Issue May 7 20<strong>04</strong><br />
10<strong>01</strong>4575 SELL GmbH <strong>EASA</strong>.A.S.02679 BOEING 777-200<br />
BOEING 777-300<br />
Interior Re-configuration of Forward Galley<br />
Complex for Emirates airline.<br />
16.02.2009<br />
31.07.2006<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 />
23.<strong>04</strong>.2<strong>01</strong>2<br />
Limited to B777-200/300 models serial<br />
numbers 29324 and 29325.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 4<strong>01</strong>/<strong>462</strong><br />
11.02.2005<br />
18.<strong>01</strong>.2007
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