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 />
10032965 FIELD AVIATION COMPANY INC. TCCA LSTC C-LSA09-212/D DHC-8-311 Installation of Aft Baggage Bay Divider The modification is applicable only when the Prior to installation of this modification it 10.12.2<strong>01</strong>0<br />
NetsTCCA LSTC C-LSA09-212/D<br />
necessary structuralprovisions are pre-existing. 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 />
10035887 FIELD AVIATION COMPANY Inc. REV. 1 DHC-8--2<strong>01</strong>/-202<br />
DHC-8-102/-103/-106<br />
DHC-8-3<strong>01</strong>/-302<br />
Auxilliary Power Unit (APU) RemovalTCCA<br />
STC SA98-30, Issue 3<br />
10035939 FIELD AVIATION COMPANY Inc. DHC-8-102/-103/-106 Installation of Right Hand Ground Air<br />
ConnectionTCCA STC C-LSA11-<strong>04</strong>3/D, Issue<br />
1<br />
10036488 FIELD AVIATION COMPANY Inc. TCCA STC NO. SA11-37 DHC-8-4<strong>01</strong>, -402 Temporary Removal of Auxilliary Power Unit<br />
(APU)TCCA STC SA11-37, Issue 1<br />
10038098 FIELD AVIATION COMPANY Inc. REV. 1 TCCA STC O-LSA06-139/D DHC-8-106<br />
DHC-8-202<br />
TCCA STC O-LSA06-139/D, Issue 2Retrofit<br />
installation of a Honeywell KHF-950 HF Radio<br />
System.<br />
100381<strong>04</strong> FIELD AVIATION COMPANY Inc. TCCA STC O-LSA06-111/D DHC-8-202 TCCA STC O-LSA06-111/D, Issue 2Retrofit of<br />
AirCell ST3100 Satellite Telephone and<br />
Tracking System.<br />
The modification is applicable only when the<br />
necessary structuralprovisions are pre-existing<br />
OEM installed APU must be removed in<br />
accordance with <strong>EASA</strong> STC 10035887or<br />
TCCA STC SA98-30, Issue 3.<br />
The modification is applicable only when the<br />
necessary structuralprovisions are pre-existing<br />
The modification is limited to Serial numbers<br />
335, 337, 445, 446.<br />
The modification is limited to Serial numbers<br />
445, 446.<br />
10038661 FIELD AVIATION COMPANY Inc. TCCA STC O-LSA11-232/D DHC-8-103 Honeywell Mark VII EGPWS Annunciator This modification is limited to Serial number<br />
Relocation and UpgradeTCCA STC O-LSA11- 310 with <strong>EASA</strong> STC No.MOT.21NE2.138<br />
232/D, Issue 1<br />
installed.<br />
10038932 FIELD AVIATION COMPANY Inc. DHC-8-102/-103/-106/-2<strong>01</strong>/-202<br />
DHC-8-3<strong>01</strong>/-311/-314/315<br />
10038999 FIELD AVIATION COMPANY Inc. JAA STC<br />
ACG.21.NE.050<br />
TCCA STC SA<strong>01</strong>-50 DHC-8-102/-103/-106<br />
DHC-8-2<strong>01</strong>/-202<br />
DHC-8-3<strong>01</strong>/-311/-314/-315<br />
Prior to installation of this modification it 28.07.2<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 it 29.07.2<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 it 13.09.2<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 it 19.<strong>01</strong>.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 19.<strong>01</strong>.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 06.03.2<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 />
Auxiliary Wing Fuel Tank InstallationTCCA STC None Prior to installation of this modification it 23.03.2<strong>01</strong>2<br />
SA11-64, Issue 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 />
Installation of Variable Position Cabin Class<br />
DividerTCCA STC SA<strong>01</strong>-50, Issue 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 />
29.03.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 216/<strong>462</strong>
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