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 />
10039339 FIELD AVIATION COMPANY Inc. REV. 1 TCCA STC SA11-27 DHC-8-102, -103, -106,<br />
Universal EFI-890R EFIS Cockpit<br />
The Installation of the DHC-8-314 MPA Prior to installation of this modification it 03.05.2<strong>01</strong>2<br />
DHC-8-2<strong>01</strong>, -202<br />
UpgradeTCCA STC SA11-27, Issue 3 configuration is limited to Serialnumber must be determined thatthe<br />
DHC-8-3<strong>01</strong>, -311, -314, -315<br />
0660.The installation of dual, Universal UNS- interrelationship between this modification<br />
1E, or UNS-1E(w) or UNS-1F orUNS-1F(w) and any other previouslyinstalled<br />
Flight Management Systems are a prerequisite modification and/ or repair will introduce<br />
to theinstallation of the EFI 890R Electronic Fl no adverse effectupon the airworthiness<br />
of the product.<br />
10039340 FIELD AVIATION COMPANY Inc. REV. 1 TCCA STC C-LSA12-<strong>01</strong>4/D DHC-8-202 Installation of upgraded Cabin Floor<br />
PanelsTCCA STC C-LSA12-<strong>01</strong>4/D, Issue 1<br />
10039731 FIELD AVIATION COMPANY Inc. TCCA STC C-LSA12-<strong>01</strong>7/D DHC-8-202 Fleet Standardization ModificationTCCA STC<br />
C-LSA12-<strong>01</strong>7/D, Issue 1<br />
10039983 FIELD AVIATION COMPANY Inc. TCCA STC C-LSA12-006/D DHC-8-202 RH Rear Facing Seat Installation.TCCA STC<br />
C-LSA12-006/D, Issue 1.<br />
The modification is limited to Serial numbers<br />
445, 446 with post-1990Hunting interiors<br />
only.Floor loads of 75 lbs/ft(s) only in<br />
conjunction with underfloor supportstructure<br />
modified per Bombardier CR 853CH2003 or<br />
equivalent.<br />
The modification is limited to Serial numbers<br />
435, 440 and 441.<br />
The modification is limited to Serial numbers<br />
435, 440 and 441 withpost-1990 Hunting or<br />
C&D interiors only.,,<br />
10<strong>04</strong>1560 FIELD AVIATION COMPANY Inc. TCCA STC C-LSA12-128/D DHC-8-202 Auxiliary Ground Heater System TCCA STC C- Installation is limited to Serial Numbers 435,<br />
LSA12-128/D, Issue 1<br />
440, 441, 445 and 446<br />
10<strong>04</strong>1590 FIELD AVIATION COMPANY Inc. REV. 1 TCCA STC SA-12-57 DHC-8-102, DHC-8-103,<br />
DHC-8-106.<br />
10<strong>01</strong>5754 FIELD AVIATION EAST, LTD. <strong>EASA</strong>.IM.A.S.<strong>01</strong>787 REV 2 SA<strong>04</strong>-125 ISSUE 1 BOMBARDIER DHC-8-102<br />
BOMBARDIER DHC-8-103<br />
BOMBARDIER DHC-8-311<br />
BOMBARDIER DHC-8-315<br />
10<strong>01</strong>5755 FIELD AVIATION EAST, LTD. <strong>EASA</strong>.IM.A.S.<strong>01</strong>788 REV 1 SA05-67 ISSUE 1 BOMBARDIER DHC-8-102<br />
BOMBARDIER DHC-8-103<br />
BOMBARDIER DHC-8-311<br />
BOMBARDIER DHC-8-315<br />
10<strong>01</strong>5849 FIELD AVIATION EAST, LTD. <strong>EASA</strong>.IM.A.S.<strong>01</strong>949 REV. 2 TCCA STC SA05-42 DHC-8-102, -103, -106<br />
DHC-8-2<strong>01</strong>/-202<br />
10027122 FIELD AVIATION EAST, LTD. P-<br />
<strong>EASA</strong>.IM.A.S.03183<br />
REV. 2 TCCA STC SA02-48 DHC-8-102, -103, -106<br />
DHC-8-2<strong>01</strong>/-202<br />
DHC-8-3<strong>01</strong>, -311, -314, -315<br />
Installation of Protective Breathing Equipment<br />
(PBE)TCCA STC SA 12-57, Issue 1<br />
Collins CTL-94E Controller for Elementary<br />
Surveillance<br />
Installation of ICARUS Sky Connect Tracker<br />
SOP and Satellite Communication System<br />
Installation of Dual Universal GLS-1250 DGPS<br />
Receivers (SCAT-1)TCCA STC SA05-42,<br />
Issue 3<br />
Retrofit Installation of Universal Avionics<br />
Systems Corp. UNS-1F FMS forSoftware<br />
versions SCN 8<strong>01</strong>/802 and 803Ref. TCCA<br />
SA02-48, Issue 5<br />
Prior to installation of this modification it 03.05.2<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 />
Prior to installation of this modification it 21.05.2<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 />
Prior to installation of this modification it 05.06.2<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 />
Prior to installation of this modification it 26.09.2<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 />
15.10.2<strong>01</strong>2<br />
Thi sapproval is only applicable to the<br />
type/model of aeronautical product specified<br />
therein. Prior to incorporating thi smodification,<br />
the installer shall establish that the<br />
interrelationship between this change and any<br />
other modification(s) incorporated<br />
FAEL (Dual UNS-1F FMS for Software<br />
versions 8<strong>01</strong>/802 and 803)<br />
STC<strong>EASA</strong>.IM.AS.3183, Issue1 or later <strong>EASA</strong><br />
approved revision must beinstalled as a<br />
prerequisite to the installation of the Dual GLS-<br />
1250DGPS (SCAT-1) modification.<br />
Configuration B Single UNS-1F with Software<br />
Version SCN 8<strong>01</strong>, EFISEquipped AircraftdeHavilland<br />
factory installed single UNS-1B or<br />
UNS-1B+ FlightManagement System Electrical<br />
and Structural provisions are aprerequisite to<br />
the Universal UNS-1F Flight Manageme<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 />
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 />
product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 217/<strong>462</strong><br />
26.02.2007<br />
<strong>04</strong>.08.2006<br />
20.<strong>01</strong>.2<strong>01</strong>2<br />
31.<strong>01</strong>.2<strong>01</strong>2
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