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 />
10027108 LEARJET INC. P-<br />
FAA STC ST<strong>01</strong>716LA-D BD-100-1A10 (CHALLEGER 300) - Installation of a Passenger Seat Upgrade- None - Prior to installation of this modification 07.09.2009<br />
<strong>EASA</strong>.IM.A.S.03188<br />
Validation of FAA STC ST<strong>01</strong>716LA-D<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- The installa<br />
10028342 LEARJET INC. P-<br />
<strong>EASA</strong>.IM.A.S.03206<br />
REV. 1 FAA STC ST<strong>01</strong>255LA-D BD-100-1A10 (CHALLENGER<br />
300)<br />
Installation of a Baseline Executive<br />
Interior.Validation of FAA STC ST<strong>01</strong>255LA-D (-<br />
2 Configuration)Revision of the <strong>EASA</strong> STC<br />
10028342 to include -2 Configuration<br />
Not Applicable Prerequisite for the installation of this<br />
STC as per FAA STCST<strong>01</strong>255LA-D:<br />
Bruce Industries Inc. STC ST<strong>01</strong>569LA -<br />
Installation of FloorProximity Emergency<br />
Escape Path Marking System Prior to<br />
installation of this modification it must be<br />
determined thatthe inte<br />
10031271 LEARJET Inc. FAA STC SA8117NM-D CL-600-2B16 Installation of the RH Forward Lavatory 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 />
06.08.2<strong>01</strong>0<br />
10031299 LEARJET Inc. FAA STC SA8118NM-D CL-600-2B16 Installation of the RH Forward Galley 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 />
09.08.2<strong>01</strong>0<br />
10035643 LEARJET INC. P-<br />
<strong>EASA</strong>.IM.A.S.02343<br />
10036055 LEARJET INC. P.<strong>EASA</strong>.IM.A.S.0325<br />
3<br />
FAA STC ST<strong>01</strong>239LA-D CL-600-2B16 FAA STC ST<strong>01</strong>239LA-D, Complete Custom<br />
Aircraft Interior<br />
BOMBARDIER CL-600-1A11<br />
BOMBARDIER CL-600-2A12<br />
BOMBARDIER CL-600-2B16<br />
FAA STC ST<strong>01</strong>735LA-D, Installation of a<br />
Kidde Aerospace Smoke Detector inthe Aft<br />
Baggage Compartment, as a replacement for<br />
Walter Kidde PIN473052.<br />
10037572 LEARJET INC. REV. 1 FAA STC ST00288BO BD100-1A10 (CHALLENGER 300) Installation of Honeywell EGPWS with<br />
windshear and Terrain Display (MDL-1<br />
configuration), Runway Awareness and<br />
Advisory System (RAAS) (MDL -<br />
2configuration) or Runway Awareness and<br />
Advisory System (RAAS) inhibit(MDL -3<br />
configuration) in accordance with Bomb<br />
10038287 LEARJET INC. FAA STC ST00299BO BD-700-1A10, BD-700-1A11 Installation of Honeywell Cockpit Displays<br />
Upgrade<br />
10<strong>04</strong><strong>04</strong>05 LEARJET INC. FAA STC SA8192NM-D BD-700-1A10 Installation of a Sextant Integrated Electronic<br />
Standby InstrumentSystem<br />
Restricted to ASN 5541.A concurrent<br />
requirement to this STC is the installation of<br />
BruceAerospace <strong>EASA</strong> STC No. 10035636<br />
(FAA STC SA6<strong>01</strong>1NM) (ref. <strong>EASA</strong><br />
PN0<strong>01</strong>0<strong>01</strong>1393) Floor Proximity Emergency<br />
Escape Path Marking System.<br />
An <strong>EASA</strong> approved Walter Kidde Smoke<br />
Detector System for PIN 473052 is<br />
aprerequisite I concurrent requirement for the<br />
installation of this STC.<br />
15.03.2<strong>01</strong>0<br />
Prior to installation of this modification it 06.07.2<strong>01</strong>1<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 the<br />
installer must determinethat the<br />
interrelationship between this modification<br />
and any otherpreviously installed<br />
modification will introduce no adverse<br />
effect uponthe airworthiness of the<br />
02.07.2009<br />
- Instructions for Continued Airworthiness ref.<br />
product. The installati<br />
Prior to installation of this modification it 19.03.2<strong>01</strong>2<br />
BAS68<strong>01</strong>70<strong>01</strong>-ICA-1 rev Adated January 14, must be determined thatthe<br />
2<strong>01</strong>1 must be made available to the operator interrelationship between this modification<br />
at thetime of installation for MDL-1<br />
and any other previouslyinstalled<br />
configuration, EGPWS with Windshear modification and/ or repair will introduce<br />
andTerrain Display. - Instructions for Continued no adverse effectupon the airworthiness<br />
A<br />
of the product.<br />
The Honeywell DU-875 Multifunction Display<br />
(MFD) Expansion Applicationsinclude 'MFD<br />
charts' (date sensitive charts with ownship<br />
position) and'MFD Uplink Graphical Weather<br />
Map' (XM Weather). Any other<br />
intendedfunction of this equipment will require<br />
a re-exa<br />
Prior to installation of this modification it 03.02.2<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 />
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 />
02.07.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 310/<strong>462</strong>
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