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 />
10027985 DANSK FLY ELEKTRONIK ApS F172D, F172E, F172F, F172H, ASPEN EFD1000 Installation Not Applicable Prior to installation of this modification it 23.11.2009<br />
F172K, F172L, F172M, F172N,<br />
must be determined thatthe<br />
F172P<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 />
10031092 DANSK FLY ELEKTRONIK ApS PA-42, PA-42-720, PA-42-1000 Installation of Avidyne EX500 MFD 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 />
27.07.2<strong>01</strong>0<br />
10031093 DANSK FLY ELEKTRONIK ApS PA-42, PA-42-720, PA-42-1000 Installation of one or two Garmin GTX 330D<br />
Mode-S transponder<br />
10031129 DANSK FLY ELEKTRONIK ApS P-<strong>EASA</strong>.A.S.03981 PA-42, PA-42-1000, PA-42-720 Installation of dual Garmin GNS 430AW, dual<br />
Garmin GNS 530AW or GarminGNS 430AW<br />
and GNS 530AW<br />
100314<strong>04</strong> DANSK FLY ELEKTRONIK ApS B200, B200C Installation of L-3 Skywatch HP Traffic Alert &<br />
Collision AvoidanceSystem, Model SKY899A.<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 />
27.07.2<strong>01</strong>0<br />
For PA-42 with Bendix King EFIS only Prior to installation of this modification the 28.07.2<strong>01</strong>0<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 />
product. The installati<br />
Garmin G1000 retrofit STC must be installed in<br />
aircraft prior toinstalling this STC.<br />
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 />
10034209 DANSK FLY ELEKTRONIK ApS B200 KING AIR Installation of Garmin DUAL GPS 400. GPS# 1 None Prior to installation of this modification it 16.03.2<strong>01</strong>1<br />
is linked to the autopilotsystem. Ref. DFE-DO-<br />
must be determined thatthe<br />
<strong>04</strong><strong>01</strong>-PS-00 Product Specification.<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 />
10034210 DANSK FLY ELEKTRONIK ApS B200 KING AIR Installation of Bendix/Kings KGP 560 EGPWS None Prior to installation of this modification it 16.03.2<strong>01</strong>1<br />
system with Avidyne EX500display. Ref. DFE-<br />
must be determined thatthe<br />
DO-<strong>04</strong>00-PS-00 Product Specification.<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 />
10035243 DANSK FLY ELEKTRONIK ApS CESSNA 414, 414A Installation of Garmin GTX330D Transponder 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 />
07.06.2<strong>01</strong>1<br />
10<strong>01</strong>4207 DAO AVIATION A/S <strong>EASA</strong>.A.S.<strong>01</strong>358 PIPER PA-24<br />
PIPER PA-24-250<br />
PIPER PA-24-260<br />
PIPER PA-24-400<br />
Installation of Garmin GNS 430<br />
COM/NAV/GPS. Approval for B-RNAV, en<br />
route IFR and Terminal flights<br />
10<strong>01</strong>4324 DAO AVIATION A/S <strong>EASA</strong>.A.S.<strong>01</strong>577 BEECH 200, SUPER KING AIR Installation of Honeywell ACAS II system<br />
comprising CAS 67A processor, 2 IVA-81D<br />
VSIs and 2 ANT-67A antennas.<br />
13.08.2<strong>01</strong>0<br />
29.06.2005<br />
MSN BB-309 only. 27.10.2006<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 160/<strong>462</strong>
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