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>5830 DECA AVIATION ENGINEERING <strong>EASA</strong>.IM.A.S.<strong>01</strong>919 REV 2 TCCA LSTC O-LSA06-056/D ISS1 DHC-6-300 Installation of an ASIRAS Radar System in a 1. DECA Aviation Flight Manual Supplement<br />
18.07.2007<br />
LIMITED<br />
DHC-6-300 aircraft in accordance with<br />
Modification Summary for ASIRIS Radar<br />
System Installation, DECA Aviation<br />
Engineering Limited document DCP 05259,<br />
Revision 2, dated 14/12/05 or later <strong>EASA</strong><br />
approved revision<br />
FMS05259, Revision 1, is required<br />
10<strong>01</strong>6112 DECA AVIATION ENGINEERING <strong>EASA</strong>.IM.A.S.02302 TCCA STC O-LSA02-397/D ISS 2 A320-214 Installation Of 180 Passenger - All Economy 1. As per Transport Canada STC O-LSA02-<br />
10.05.2007<br />
LIMITED<br />
Class Seating Arrangement, in accordance 397/D Issue 2.2. This STC is approved only<br />
with Transport Canada STC O LSA02-397/D for the product configuration as defined in the<br />
Issue 2<br />
approved design data referred to in the<br />
paragraphs "Description" and “Associated<br />
Technical Documentation”. Compatibility<br />
10<strong>01</strong>6342 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10<strong>01</strong>6431 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10<strong>01</strong>6482 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10027141 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10029659 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10029922 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10030614 DECA AVIATION ENGINEERING<br />
LIMITED<br />
10032064 DECA AVIATION ENGINEERING<br />
LIMITED<br />
<strong>EASA</strong>.IM.A.S.02656 REV. 1 TCCA SA00-98 ISSUE 4 BD-700-1A10 Baggage Door Locking System Modification. 23.<strong>04</strong>.2008<br />
<strong>EASA</strong>.IM.A.S.02771 REV 1 TCCA STC O-LSA07-260/D ISSUE 2 BOMBARDIER BD-700-1A10 Cabin Interior Reconfiguration. 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 install<br />
<strong>EASA</strong>.IM.A.S.02836 TC STC O-LSA08-069/D BOMBARDIER DHC-6-300 Radar System Installation. 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 install<br />
REV. 1 TCCA SA00-126; CAA NL SA0<strong>01</strong>4NL DHC-8-102, -103, -106<br />
DHC-8-2<strong>01</strong>, -202<br />
DHC-8-3<strong>01</strong>, -311, -314, -315<br />
QAR/ASAP Monitoring SystemTCCA SA00-<br />
126, Is. 4<br />
TCCA LSTC O-LSA09-37/D B737-800 Interior Reconfiguration & miscelaneous Cabin<br />
Alterations /Modification and relocation of the<br />
passenger seats along<br />
withrelocation/installation of emergency<br />
equipments.<br />
TCCA LSTC O-LSA09-<strong>04</strong>0/D B737-800 Sliding Carpet Loading System Removal/<br />
Deactivation<br />
TCCA STC O-LSA06-007/D B737-800 Passenger Seating Arrangement - Installation /<br />
Relocation of passengerSeats in 186-189 Pax<br />
Configuration and installation of<br />
EmergencyEquipments<br />
TCCA STC O-LSA10-43 DHC-6-300 Radar Antenna Installation - Structural<br />
Provisions i.a.w. TCCA STCO-LSA10-<strong>04</strong>3/D<br />
The QAR system configurations are<br />
compatible with each of the<br />
followingFDR/FDAU combinations: For Model<br />
DHC -8- 102, -103, -106, -2<strong>01</strong>, -202L3 FDR<br />
No: 2100-4<strong>04</strong>3-00 with Plessey FDAU No:<br />
612/1/49780/102 (ModelPA3810Bl/Post Mod<br />
8/1876). For Model DHC -8 -3<strong>01</strong>,<br />
12.11.2008<br />
12.11.2008<br />
1. Prior to installation of this modification <strong>04</strong>.<strong>01</strong>.2<strong>01</strong>0<br />
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 insta<br />
Valid for MSN 30292 only None 09.<strong>04</strong>.2<strong>01</strong>0<br />
Valid for MSN30292 and 33029 only 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 />
03.05.2<strong>01</strong>0<br />
Only valid for MSN 28373, 28375, 29351,<br />
29642, 29883, 30637, 30671,33003, 33029,<br />
33699, 347<strong>04</strong>, 35093<br />
a) For serial number 235 only.b) Flight in kwon<br />
icing conditions are not approved.<br />
Prior to installation of this modification it 25.06.2<strong>01</strong>0<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 />
Prior to installation of this modification it 06.10.2<strong>01</strong>0<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>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 180/<strong>462</strong>
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