04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
04/01/2013 Page 1/462 - EASA
Create successful ePaper yourself
Turn your PDF publications into a flip-book with our unique Google optimized e-Paper software.
<strong>EASA</strong> STC no. STC holder Old STC ref. Revision Level Foreign/NAA STC ref. Model Description Limitations Conditions Date of issue<br />
10029931 EUROCOPTER UK Ltd. REV. 1 MBB-BK117 C-2 Cabin Configuration - Installation of Police or None Prior to installation of this modification it 11.06.2<strong>01</strong>0<br />
Emergency Medical SystemRole Equipment<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 />
10030287 EUROCOPTER UK Ltd. MBB-BK 117 C-2 Wescam HDi FLIR camera system.Installation<br />
of Wescam HDi FLIR camera system with<br />
build standards foralternate installation of MX-<br />
15 Analogue system in accordance with EC<br />
UKchange no. MHL/145/1211, Master<br />
Drawings A3/1451211-100-1&-2.<br />
Theinstallation is inc<br />
1. Following items must be installed on the<br />
aircraft prior toincorporation of this<br />
change:ACS/MEEKER Utility step on the right<br />
hand side, p/n AFM/SM117A-11 andrelated<br />
Arm p/n AF-SM117-C10 installed i.a.w. STC<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>489 2. This approval does not<br />
inc<br />
Prior to installation of this modification it 09.06.2<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 />
10030343 EUROCOPTER UK Ltd. BK117 C-2 (EC145) Dual Martin Baker Swivelling Passenger Seats As identified in RFMS 19 None 11.06.2<strong>01</strong>0<br />
10031371 EUROCOPTER UK Ltd. AS350B3 Coupling of the existing Sagem/SFIM Autopilot<br />
installation with theGarmin GNS530<br />
10031633 EUROCOPTER UK Ltd. MBB-BK 117C2 Skyshout SystemInstallation of a Skyshout<br />
System. With internal cabin control andexternal<br />
loudspeaker array, installed on aircraft RHS<br />
and configuredwith low skid landing gear<br />
10032268 EUROCOPTER UK Ltd. REV. 1 EC135 T2+ NVIS Certification for EC135 T2+REV. 1 is<br />
implementing administrative changes<br />
10033580 EUROCOPTER UK Ltd. EC 135 T1(CDS)<br />
EC 135 T1(CPDS)<br />
EC 135 T2(CPDS)<br />
EC 135 T2+<br />
Installation of Spectrolab Nightsun XP on<br />
EC135 equipped with ECUKequipment pod.<br />
Equipment inspection and re-certification to<br />
close therequirement for AD No. 2<strong>01</strong>0-<br />
<strong>01</strong>83R1. Note: Identical to STC with ref.<br />
10032575, re-issued for<br />
administrativepurposes.<br />
10034086 EUROCOPTER UK Ltd. REV. 1 EC 130 B4 Installation of Sagem Cockpit Display System<br />
MHL/130/1245 and revisionto Eurocopter UK<br />
EC130B4 Supplement No. 1<br />
10039454 EUROCOPTER UK Ltd. EC135 P1 Installation of Kelvin 275 Camera per Drawing<br />
List DL/1352<strong>04</strong>4-0<strong>01</strong>, IssueA<br />
100397<strong>04</strong> EUROCOPTER UK Ltd. EC 135 P1 Cabin ConfigurationInstallation of equipment<br />
rack and pedestal mounted LCD monitor in<br />
theforward cabin, as per ECD design change<br />
EC UK/135/2<strong>04</strong>3<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 />
12.08.2<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 />
<strong>01</strong>.09.2<strong>01</strong>0<br />
None The first installation of this STC must be<br />
performed with the assistanceof the STC<br />
holder.This rotorcraft employs Night<br />
Vision Imaging System lighting,<br />
commonlynamed NVIS lighting, that has<br />
been certified to ensure the aircraft<br />
iscompatible with night visi<br />
11.02.2<strong>01</strong>1<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 />
16.11.2<strong>01</strong>0<br />
Prerequisite<br />
Prior to installation of this modification it <strong>04</strong>.03.2<strong>01</strong>1<br />
changes:MHL/130/1246,,,,,,TWX670 Weather must be determined thatthe<br />
detection systemMHL/130/1070,,,,,,KRA405B interrelationship between this modification<br />
Radio AltimeterMHL/130//1069,,,,,,Avidyne and any other previouslyinstalled<br />
TAS620 Traffic Advisory<br />
modification and/ or repair will introduce<br />
SystemMHL/130/952,,,,,,Replacement of no adverse effectupon the airworthiness<br />
GNS430 with GNS530WSTC<br />
<strong>EASA</strong>.IM.R.S.<strong>01</strong>061,,Installation o<br />
of the product<br />
-Day/Night VFR operation only-Operation of<br />
the Kelvin 275 camera approved under this<br />
STC (EC UKmodification EC UK/135/2<strong>04</strong>4)<br />
has to be done, in conjunction with EC<br />
UKmodifications EC UK/135/2<strong>04</strong>5 and EC<br />
UK/135/2<strong>04</strong>3<br />
Prior to installation of this modification it <strong>04</strong>.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 />
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 />
18.05.2<strong>01</strong>2<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 213/<strong>462</strong>
Change language