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 />
10037710 ACS-NAI Ltd. TCCA STC C-LSA10-169/D CL-600-2B19 Installation, Complete Custom Aircraft Interior. Restricted to ASN 81<strong>01</strong>. 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 />
16.12.2<strong>01</strong>1<br />
10037711 ACS-NAI Ltd. TCCA STC C-LSA11-165/D CL-600-2B19 Installation, Complete Custom Aircraft Interior. Restricted to ASN 8107. 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 />
16.12.2<strong>01</strong>1<br />
10038022 ACS-NAI Ltd. TCCA STC NO. C-LSA11-009/D CL-600-2B19 Installation, Complete Custom Aircraft Interior. Restricted to ASN 81051.The Wireless Local Prior to installation of this modification it 12.<strong>01</strong>.2<strong>01</strong>2<br />
Area Network (WLAN) system installed as part must be determined thatthe<br />
of theinterior completion is intended to provide interrelationship between this modification<br />
cached internet content andemail services to and any other previouslyinstalled<br />
Portable Electronic Devices. Any other use of modification and/ or repair will introduce<br />
thisequipment will require a<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10038149 ACS-NAI Ltd. TCCA STC NO. C-LSA11-179/D BD-700-1A10 Modifications to Existing Interior Completions -<br />
ASN 9393.<br />
10039631 ACS-NAI Ltd. TCCA STC C-LSA05-318/D CL-600-2B16 Aircraft Completion ASN 5618, 12 Passenger<br />
Interior Configuration.<br />
10039703 ACS-NAI Ltd. TCCA STC NO. C-<br />
LSA12-038/D<br />
10<strong>04</strong>0686 ACS-NAI Ltd. JAA STC<br />
ACG.21NE2.084<br />
TCCA SA<strong>01</strong>-77/JAA ACG.21NE2.084 DHC-8-102,-103,-106<br />
DHC-8-2<strong>01</strong>,-202,<br />
DHC-8-3<strong>01</strong>,-311,-314,-315<br />
10<strong>04</strong>1474 ACS-NAI Ltd. REV. 1 TCCA STC SA12-17 PC-6/B2-H2<br />
PC-6/B2-H4<br />
10<strong>04</strong>2346 ACS-NAI Ltd. ACG.21NE2.108 TCCA SA02-127 / ACG.21NE2.108 DHC-8-102,-103,-106<br />
DHC-8-2<strong>01</strong>,-202<br />
DHC-8-3<strong>01</strong>,-311,-314,-315<br />
Restricted to ASN 9393 andThe Installation of Prior to installation of this modification it 24.<strong>01</strong>.2<strong>01</strong>2<br />
<strong>EASA</strong> STC No. 10036060 is a prerequisite for must be determined thatthe<br />
theapproval of this STC.<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 />
Restricted to ASN 5618 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 />
15.05.2<strong>01</strong>2<br />
BD-700-1A10 Installation of Complete Custom Aircraft Interior Restricted to ASN 9434.The Wireless Local Prior to installation of this modification it 18.05.2<strong>01</strong>2<br />
- ASN 9434<br />
Area Network (WLAN) system is intended to must be determined thatthe<br />
provideinternet connectivity and email services interrelationship between this modification<br />
to the airplane's cabin usingportable devices and any other previouslyinstalled<br />
(PEDs). Any other intended function of this modification and/ or repair will introduce<br />
equipmentwill require a re-examina<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
Installation of an improved Aft Jet Pipe Support None. Prior to installation of this modification it 19.07.2<strong>01</strong>2<br />
TCCA STC N° SA<strong>01</strong>-77, Issue 3<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 Vapour Cycle Air Conditioner<br />
System.<br />
Installation of an Improved Gound Power<br />
Current Limiter(ACS-NAI Ltd. Modification<br />
Data Summary D 11900) TCCA STC SA02-<br />
127, Issue 1<br />
Refer to the Airworthiness Limitations Prior to installation of this modification it <strong>04</strong>.10.2<strong>01</strong>2<br />
contained in Airplane FlightManual Supplement must be determined thatthe<br />
H4<strong>04</strong>091 Revision N/C.<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 />
26.11.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 5/<strong>462</strong>
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