04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
You also want an ePaper? Increase the reach of your titles
YUMPU automatically turns print PDFs into web optimized ePapers that Google loves.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10038867 CONCORDE BATTERY CORPORATION FAA STC 03930AT ATR 42-200 /-300 /-320 /-500 Installation of a Lead Acid BatteryThis STC None. Prior to installation of this modification it 20.03.2<strong>01</strong>2<br />
ATR 72-1<strong>01</strong> / -102<br />
installs a Lead Acid battery in replacement of<br />
must be determined thatthe<br />
ATR 72-2<strong>01</strong> / -202 / -211 the existingNickel-Cadmium battery.<br />
interrelationship between this modification<br />
ATR 72-212 / -212A<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>0738 CONCORDE BATTERY CORPORATION FAA STC NO. SA<strong>01</strong>633WI EMB 500 Installation of Concorde RG-390E VRSLA<br />
Batteries in the Embraer 500 inaccordance<br />
with Concorde Battery Corporation Master<br />
Drawing List, DWGNo. 5-0359, Revision NC,<br />
dated August 25, 2<strong>01</strong>0 or later FAA<br />
approvedrevisions.<br />
10<strong>04</strong>0781 CONCORDE BATTERY CORPORATION FAA STC ST<strong>01</strong>643WI DHC-8-102, -103, -106<br />
DHC-8-2<strong>01</strong>, -202<br />
DHC-8-3<strong>01</strong>, -311, -314, -315<br />
10<strong>04</strong>2099 CONCORDE BATTERY CORPORATION FAA STC SA<strong>01</strong>118WI SEE <strong>EASA</strong> APPROVED MODEL<br />
LIST<br />
Installation of Concorde RG-380E/44 (42AH)<br />
or RG-380E/60L (48AH) SeriesValve<br />
Regulated Sealed Lead-Acid (VRSLA)<br />
batteries as replacement of OEMbatteries.FAA<br />
STC ST<strong>01</strong>643WI<br />
Installation of the Concorde FLA or VRSLA RG<br />
series batteries in CessnaSingle Engine<br />
Airplanes listed on the attached Approved<br />
Model List (AML)in accordance with Concorde<br />
Battery Corporation, Master Drawing ListDwg.<br />
No. 5-<strong>01</strong>48, Revision A, dated August 16,<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 />
24.07.2<strong>01</strong>2<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 />
26.07.2<strong>01</strong>2<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 />
08.11.2<strong>01</strong>2<br />
10<strong>01</strong>4097 CONTOUR AEROSPACE LIMITED <strong>EASA</strong>.A.S.<strong>01</strong>195 REV 1 BOEING 767-300 SERIES Introduction G3 Wardrobe to British Airways<br />
aircraft as defined in the modification definition<br />
document and Declaration of Design and<br />
Performance (DDP)<br />
As defined in the DDP. 20.05.2005<br />
10<strong>01</strong>6274 CORPORATION LOGIC AIR Inc. <strong>EASA</strong>.IM.A.S.02560 REV 1 TC STC C-LSA07-205/D ISSUE 2 BOEING 767-300 Installation of In-Flight Entertainment System. 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 />
10<strong>01</strong>6283 CORPORATION LOGIC AIR Inc. <strong>EASA</strong>.IM.A.S.02578 TCCA SA07-210/D ISSUE 1 BOEING 767-300 Installation of 270 Pax Interior Configuration. 02.11.2007<br />
10<strong>01</strong>6284 CORPORATION LOGIC AIR Inc. <strong>EASA</strong>.IM.A.S.02579 REV 1 TCCA STC SA07-12 ISSUE 2 BOEING 767 Tire pressure Indication System De-activation,<br />
Boeing 767-300.<br />
10<strong>01</strong>6285 CORPORATION LOGIC AIR Inc. <strong>EASA</strong>.IM.A.S.02580 TCCA STC C-LSA07-091/D BOEING 767-300 installation of Mode S ATC Transponder with<br />
Elementary and Enhanced Surveillance Modes.<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 will<br />
introduce no adverse effect upon the<br />
airworthiness of the product. The install<br />
10<strong>01</strong>6290 CORPORATION LOGIC AIR Inc. <strong>EASA</strong>.IM.A.S.02585 C-LSA03-498/D BOEING 767-300 Changes to Altitude Callout Configuration,<br />
Honeywell Mark V EGPWS.<br />
02.11.2007<br />
10033973 CRANE AEROSPACE & ELECTRONICS FAA STC ST02316LA LEARJET 60 Installation of Tire Pressure Sensor FAA STC None Prior to installation of this modification it 23.02.2<strong>01</strong>1<br />
ST02316LA (Date of issuance: September 28,<br />
must be determined thatthe<br />
2<strong>01</strong>0)<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>4384 CRANFIELD AEROSPACE LTD <strong>EASA</strong>.A.S.<strong>01</strong>669 Installation of a Honeywell Global GNS-XLS 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 />
20.02.2006<br />
10027822 CRANFIELD AEROSPACE LTD P-<strong>EASA</strong>.A.S.03734 BAE JETSTREAM 3100 Installation of Satcom System None None 09.11.2009<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 158/<strong>462</strong><br />
10.<strong>04</strong>.2008<br />
07.08.2008<br />
02.11.2007
Change language