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>6286 ROCKY MOUNTAIN AIRCRAFT <strong>EASA</strong>.IM.A.S.02581<br />
TCCA STC SA02-119; <strong>EASA</strong> STC.IM VIKING AIR LIMITED (DCH) DHC- Dual or Single Garmin GNS530 or GNS430 Prior to installation of this modification the<br />
21.11.2008<br />
REVISION 1<br />
6<br />
installation.<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>6400 ROCKY MOUNTAIN AIRCRAFT <strong>EASA</strong>.IM.A.S.02729 REV. 1 TCCA STC SA07-131 DHC-6-100, DHC-6-200,DHC-6-<br />
300<br />
10<strong>01</strong>6511 ROCKY MOUNTAIN AIRCRAFT <strong>EASA</strong>.IM.A.S.02878 REV. 1 TCCA STC SA08-38 BOMBARDIER DHC-6 SERIES<br />
200<br />
BOMBARDIER DHC-6-100<br />
BOMBARDIER DHC-6-300<br />
Installation of single or dual Sandel SN4500<br />
primary navigationdisplay(s) (EHSI) with<br />
optional SA4550 primary attitude<br />
display(s)(EADI)<br />
10037908 ROCKY MOUNTAIN AIRCRAFT TCCA STC SA11-72 DHC-6 SERIES 100, 200, 300 Installation of chip detectors on both left hand<br />
and right hand enginewith caution indication in<br />
DHC-6 series 100, 200, and 300 Twin<br />
Otteraircraft based on Engineering Data<br />
Summary E1<strong>04</strong>600 in accordance<br />
withTransport Canada STC SA11-72, Issue 1<br />
Installation of Pitot Heat Indication 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 instal<br />
None 1) Prior to installation of this modification 03.08.2<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 inst<br />
11.11.2008<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 />
05.<strong>01</strong>.2<strong>01</strong>2<br />
10038966 ROCKY MOUNTAIN AIRCRAFT DHC-6-100/-200/-300 Installation of Dual or Single Garmin GTN 650 None<br />
or GTN 750 in DHC-6 series100, 200, and 300<br />
Twin Otter aircraft based on Engineering Data<br />
SummaryE102910 & E102911 in accordance<br />
with Transport Canada STC SA11-79, Issue1<br />
None 27.03.2<strong>01</strong>2<br />
10<strong>04</strong>0247 ROCKY MOUNTAIN AIRCRAFT TCCA STC NO. SA11-80 DHC-6 SERIES 100<br />
DHC-6 SERIES 200<br />
DHC-6 SERIES 300<br />
10<strong>04</strong>2836 ROCKY MOUNTAIN AIRCRAFT TCCA STC SA05-54 DHC-6 SERIES 100<br />
DHC-6 SERIES 200<br />
DHC-6 SERIES 300<br />
10<strong>01</strong>5218 ROEDER PRAEZISION GMBH <strong>EASA</strong>.A.S.03633 CIRRUS SR20<br />
CIRRUS SR22<br />
Installation of either Universal Avionics CVR-<br />
120A or CVR-120R inaccordance with<br />
Transport Canada STC SA11-80, Issue 1<br />
Installation of a L-3 Skywatch HP TCAS 1<br />
System in accordance with TCCASTC SA05-<br />
54<br />
Installation of Avidyne Iridium MLX770 Two<br />
Way Datalink.<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 />
19.06.2<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 />
20.12.2<strong>01</strong>2<br />
1. 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.2.<br />
100292<strong>01</strong> ROEDER PRAEZISION GMBH CESSNA P210N Ferry Tank Provisioning Limited to Aircraft S/N P210 00629 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 />
11.03.2<strong>01</strong>0<br />
10030847 ROEDER PRAEZISION GMBH REV. 1 206H, T206H Provisioning for implementation and operation<br />
with a "Turtle Pac160-ferry tank"<br />
Installation of the ferry tank is not subject of<br />
this STC.<br />
03.12.2008<br />
Prior to installation of this modification it 14.07.2<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> 373/<strong>462</strong>
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