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 />
10026840 AERO CONSULTING SERVICES LTD. TCCA LSTC C-LSA09-028/D CL-600 2B19 Installation, Complete Custom Aircraft Restricted to ASN 8070The applicant must 1) Prior to installation of this modification 14.08.2009<br />
submit the final EWIS ICA, if applicable, to the installer mustdetermine that the<br />
theAgency by 07 June 2<strong>01</strong>0.<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 />
100269<strong>04</strong> AERO CONSULTING SERVICES LTD. P-<br />
<strong>EASA</strong>.IM.A.S.03136<br />
10027086 AERO CONSULTING SERVICES LTD. P-<br />
<strong>EASA</strong>.IM.A.S.03165<br />
10027216 AERO CONSULTING SERVICES LTD. P-<br />
<strong>EASA</strong>.IM.A.S.03160<br />
TCCA LSTC C-LSA09-032/D CL-600-2B19 Installation, Complete Custom Aircraft Interior Restricted to ASN 8089 The applicant must submit the final EWIS<br />
ICA, if applicable, to theAgency by 07<br />
June 2<strong>01</strong>0. Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification a<br />
REV. 1 TCCA STC C-LSA09-33/D CL-600-2B19 Installation, Complete Custom Aircraft Interior -<br />
ASN 8085<br />
21.08.2009<br />
Restricted to ASN 8085 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 />
22.10.2<strong>01</strong>0<br />
TCCA STC C-LSA09-079/D BD-700-1A11 Installation 16G Side Facing Divan Restricted to: ASN 9289 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 />
14.09.2009<br />
10027715 AERO CONSULTING SERVICES LTD. TCCA LSTC C-LSA09-099/D BD-700-1A10 Installation, 16 G Side Facing Divan. None. Prior to installation of this modification the 26.10.2009<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 />
10028465 AERO CONSULTING SERVICES LTD. TCCA LSTC C-LSA08-007/D LEARJET 60 Installation of Chelton HSD Satcom System. Approval is valid for s/n 60-328 only. None. 13.<strong>01</strong>.2<strong>01</strong>0<br />
10028761 AERO CONSULTING SERVICES LTD. P-<br />
<strong>EASA</strong>.IM.A.S.03154<br />
10028762 AERO CONSULTING SERVICES LTD. P-<br />
<strong>EASA</strong>.IM.A.S.03131<br />
10028763 AERO CONSULTING SERVICES LTD. P-<br />
<strong>EASA</strong>.IM.A.S.03134<br />
10028799 AERO CONSULTING SERVICES LTD. TCCA STC C-LSA10-006/D 900XP Installation of Dual Lifeport Patient Loading and<br />
Utility System (PLUS)<br />
10029239 AERO CONSULTING SERVICES LTD. TCCA LSTC C-LSA10-<strong>01</strong>0/D PC-12/47E Installation, Lifeport PLUS Units in Tandem<br />
Configuration<br />
10029773 AERO CONSULTING SERVICES LTD. REV. 1 TCCA PROJECT # C-09-784 PC-12/47E Main battery No. 2 relocation.Validation of the<br />
TCCA STC SA10-4 Issue 1: Relocation of the<br />
mainbattery No 2 from the tail section to the<br />
engine compartment.<br />
10029833 AERO CONSULTING SERVICES LTD. TCCA STC SA10-9 CL600-1A11, CL600-2A12,<br />
CL600-2B16<br />
BOMBARDIER CL-600-2B19 31.07.2009<br />
BOMBARDIER CL-600-2B19 16.07.2009<br />
BOMBARDIER CL-600-2B19 27.07.2009<br />
Transport Canada STC No. SA10-9 Issue 1<br />
dated 08 February 2<strong>01</strong>0.ACS-NAI Ltd.<br />
Modification Data Summary Number G373000<br />
Revision N/C orlater approved<br />
revision.Instructions for Continued<br />
Airworthiness G373071 Revision A and<br />
G373072Revision N/C, or later approv<br />
Aircraft Serial Number HA-<strong>01</strong>14 Only - Prior to installation of this modification<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- The installa<br />
10.02.2<strong>01</strong>0<br />
The applicability of the present STC is limited<br />
to Aircraft S/N: 1165Refer to the Limitations<br />
section in the TCCA-approved Airplane<br />
FlightManual Supplement listed in associated<br />
technical documentation<br />
Prior to installation of this modification it 15.03.2<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 />
None. None. 02.11.2<strong>01</strong>0<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 />
23.<strong>04</strong>.2<strong>01</strong>0<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 11/<strong>462</strong>
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