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>5295 JET AVIATION FLUGZEUGWARTUNG <strong>EASA</strong>.A.S.03840 CESSNA 650 Installation of dual Honeywell GNS-XLS 1) Prior to installation of this modification the<br />
27.05.2009<br />
GmbH<br />
PRNAV FMS<br />
installer must determine that the<br />
interrelationship between this modification<br />
andany other previously installed modification<br />
will introduce no adverse effect upon the<br />
airworthiness of the product.2) The ins<br />
10027115 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10027116 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10027199 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10027391 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10027933 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10028549 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10028945 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10035941 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
10038721 JET AVIATION FLUGZEUGWARTUNG<br />
GmbH<br />
P-<strong>EASA</strong>.A.S.03705 500, 550, S550, 560 Installation of a TAWS System Honeywell Mark Restricted to aircraft which already have<br />
VIII EGPWS<br />
installed a suitablemultifunction display.<br />
P-<strong>EASA</strong>.A.S.03730 500, 550, S550, 560 Installation of an FMS System Universal UNS-<br />
1M<br />
P-<strong>EASA</strong>.A.S.03743 P.180 AVANTI II Installation of Garmin GPS-400 / 400W<br />
System<br />
1) Prior to installation of this modification 08.09.2009<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 inst<br />
None The installation of Air Data Computer<br />
B&D ADC900<strong>04</strong> is optional. Prior<br />
to installation of this modification it must<br />
be determined thatthe interrelationship<br />
between this modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will in<br />
08.09.2009<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. The in<br />
14.09.2009<br />
P-<strong>EASA</strong>.A.S.03654 500, 550, 560 Installation of Honeywell KLN-94-GPS The installation is limited to Cessna models Prior to installation of this modification it 28.09.2009<br />
500, 550 and 560 equippedwith Honeywell must be determined thatthe<br />
SPZ 500 Auto Pilot /Flight Director system and interrelationship between this modification<br />
RD600 /RD44 Horizontal Situation Indicator and any other previouslyinstalled<br />
525A Upgrade of existing Dual Garmin GTX 330D<br />
Transponder System for EHS<br />
system Limitations according to AFMS 2008-8-<br />
8<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<br />
modification and any otherpreviously<br />
installed modification and/ or repair will<br />
introduce noadverse effect upon the<br />
airworthiness of the product. The<br />
<strong>EASA</strong>.A.S.03911 BEECH 1900 15.07.2009<br />
P.180 AVANTI, AVANTI II Installation of In-Flight Entertainment System in<br />
accordance withEngineering Order, Doc. No.<br />
2009-9<br />
None Prior to installation of this modification it<br />
must be determined thatthe<br />
,,interrelationship between this<br />
modification and any otherpreviously<br />
installed modification and/ or repair will<br />
introduce noadverse effect upon the<br />
airworthiness of the product. The<br />
17.11.2009<br />
22.02.2<strong>01</strong>0<br />
BD-700-1A11 Cabin Reconfiguration Restricted to ASN 9166A prerequisite for this Prior to installation of this modification it 29.07.2<strong>01</strong>1<br />
approval is Transport Canada STC No. SA05- must be determined thatthe<br />
60(FAA STC No ST02140NY) as applicable to interrelationship between this modification<br />
ASN 9166. However <strong>EASA</strong> has notapproved and any other previouslyinstalled<br />
this STC for ASN9166 and if this aircraft is to modification and/ or repair will introduce<br />
be entered onan EU register then the ST no adverse effectupon the airworthiness<br />
of the product.<br />
EMB-135BJ Installation of 4 Place Ambulance Stretcher<br />
System/ VIP interior.Description as per:Master<br />
Data List reference 2<strong>01</strong>1-8-16, Revision A,<br />
dated 26th February2<strong>01</strong>2. Engineer Order<br />
reference 2<strong>01</strong>1-8, Revision A, dated 26th<br />
February 2<strong>01</strong>2.AFM Supplement, reference 2<br />
None. None. 09.03.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 295/<strong>462</strong>
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