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>0380 AIRCAD AIRCRAFT CABIN DESIGN F900EX Partial Cabin Entertainment and Galley Falcon 900EX S/N 054 Prior to installation of this modification it 28.06.2<strong>01</strong>2<br />
equipment upgrade<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>0624 AIRCAD AIRCRAFT CABIN DESIGN REV. 1 F2000 Installation of a sliding door, main entryway<br />
door removableworkshelves, installation or<br />
replacement of galleys equipment and<br />
IFEequipment, RH and annex RH galleys<br />
shelves rearrangement.<br />
10038356 AIRCRAFT CABIN MAINTENANCE GmbH A318, A319, A320, A321 Installation of refurbished Passenger Seat Belt<br />
P/N EPA20511-2-<strong>01</strong>-33 on16g seats<br />
10039575 AIRCRAFT CABIN MAINTENANCE GmbH REV. 1 1. A330<br />
2. B737<br />
3. B767<br />
10<strong>04</strong>2194 AIRCRAFT CABIN MAINTENANCE GmbH SEE APPROVED MODEL LIST Installation of refurbished Passenger Seat Belt<br />
P/N EPA 6488-2-<strong>01</strong>-40 on16g seats<br />
10033896 AIRCRAFT DESIGN & CERTIFICATION<br />
Ltd<br />
10035295 AIRCRAFT DESIGN & CERTIFICATION<br />
Ltd<br />
100365<strong>01</strong> AIRCRAFT DESIGN & CERTIFICATION<br />
Ltd<br />
Falcon 2000 S/N 111. 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 />
19.07.2<strong>01</strong>2<br />
As per Service Bulletin No. 62-146169 SEB 06<br />
00, latest revision.<br />
The installation of this modification by<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation.Prior to<br />
installation of this modification it must be<br />
Installation of refurbished Passenger Seat Belt As per Service Bulletin No. 82-1000845 SEB<br />
determined thatthe interre<br />
The installation of this modification by 21.05.2<strong>01</strong>2<br />
P/N EPA20511-2-<strong>01</strong>-20 on16g seats 06 00, latest revision<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation. Prior to<br />
installation of this modification it must be<br />
determined thatthe interr<br />
As per Service Bulletin No. 1<strong>04</strong>-10<strong>01</strong>541 SEB The installation of this modification by 14.11.2<strong>01</strong>2<br />
06 00, latest revision<br />
third persons is subject towritten<br />
permission of the approval holder and<br />
holding and disposal ofthe approved<br />
appropriate documentation.Prior to<br />
installation of this modification it must be<br />
determined thatthe interre<br />
VENTUS CM Steerable Tail Wheel Ventus cM with Schempp-Hirth technical Note None.<br />
825-6.<br />
17.02.2<strong>01</strong>1<br />
REV. 1 L-13 "BLANÍK" Modification and inspection program for According to the applicable AFM Supplement. Prior to installation of this modification it 28.02.2<strong>01</strong>2<br />
compliance with <strong>EASA</strong>AD-2<strong>01</strong>0-<strong>01</strong>85-E.<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 />
EA 300, EA 300/S<br />
EA 300/L, EA 300/LC<br />
Multi glider towing capacity up to 1000kg total<br />
tow mass<br />
10<strong>01</strong>6510 AIRCRAFT ENGINEERING & <strong>EASA</strong>.IM.A.S.02877 FAA STC ST02974AT BOEING 767 Installation of the KANNAD 406 ATP<br />
Emergency Locator Transmitter<br />
10<strong>01</strong>4852 AIRCRAFT INDUSTRIES, A.S. <strong>EASA</strong>.A.S.03076 CAA CZ STC--<strong>01</strong>0 LETECKE ZAVODY L 410 UVP-<br />
E20<br />
Completion recorded parameters FDR BUR 1-<br />
2G for compliance with Brazilian regulation<br />
RBHA 135.152.<br />
10<strong>01</strong>4896 AIRCRAFT INDUSTRIES, A.S. <strong>EASA</strong>.A.S.03126 Implementation of VFR-NIGHT kind of<br />
operation - installation of additionalm<br />
equipment ensuring the extension of currently<br />
approved kinds of operation to VFR-NIGHT<br />
kind of operation.<br />
08.02.2<strong>01</strong>2<br />
Aircraft conforming to <strong>EASA</strong> TCDS.A.362 and Prior to installation of this modification it 14.09.2<strong>01</strong>1<br />
being equipped accordingUA-300-4-95 Air-tow- must be determined thatthe<br />
release.<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 />
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<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.<br />
This STC is approved only for the product<br />
configuration as defined in the approved design<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 />
03.06.2008<br />
22.03.2007<br />
Applicable for s/n 23-08 only. 23.07.2007<br />
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