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 />
10029836 BOURNEMOUTH AVIATION<br />
BOEING 737-800 164 Passenger Layout. None. Prior to installation of this modification it 23.<strong>04</strong>.2<strong>01</strong>0<br />
(CONSULTANTS)<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 />
10038818 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
100389<strong>04</strong> BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10038905 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10038906 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10038907 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10038986 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>04</strong>1170 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>04</strong>1983 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
REV. 1 AS332 L2 Installation of Seat Rail Mounted Fuel Tank. 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 />
20.03.2<strong>01</strong>2<br />
0<strong>01</strong>0<strong>01</strong>2414-0<strong>01</strong> CAA UK STC AAN 27329 A109E OBSERVER MOVING MAP SYSTEM The approval holder shall fulfill the obligations<br />
INSTALLATIONThe system is manufactured of Part 21, Paragraph 21A.118A.Prior to<br />
by Skyforce and consists of a 5"Display/Control installation of this modification it must be<br />
Head, a Processor Unit, and a Control Panel. determined thatthe interrelationship between<br />
Theequipment is CAA approved under this modification and any other<br />
miscellaneous approvals No. MIS0<strong>01</strong>83.The<br />
installation is ident<br />
previouslyinstalled modification and/ or rep<br />
0<strong>01</strong>0<strong>01</strong>2415-0<strong>01</strong> CAA UK STC AAN 27645 A109E OXYGEN SYSTEM MODIFICATIONReplace<br />
(before) P/N 127<strong>01</strong>52-3 Oxygen cylinder with<br />
(now) "BritishOxygen Company" (BOC),<br />
Medical Gases AF size cylinder.The installation<br />
is identified and defined by the "Sloane<br />
HelicoptersLtd. Modification document No.<br />
P023/109/M<br />
0<strong>01</strong>0<strong>01</strong>2416-0<strong>01</strong> CAA UK STC AAN 27764 A109E Installation of Bendix/King RDR 2000 Weather<br />
Radar System(Bendix/King RDR 200 is CAA<br />
approved Ref. VC <strong>01</strong><strong>04</strong>8).The installation<br />
consists of an antenna-receiver-transmitter<br />
(ART) unit,the Configuration Module, and the<br />
Control Panel. The (ART) radar unit isfi<br />
0<strong>01</strong>0<strong>01</strong>2417-0<strong>01</strong> CAA UK STC AAN 27763 A109E Trimble 21<strong>01</strong> (IO) Approach Plus GPS(CAA<br />
approved Ref. VC<strong>01</strong><strong>04</strong>8)The installation<br />
consists of a Jeppesen data base slot card,<br />
aReceiver/Display Unit (RDU) interfaced to the<br />
EFIS via ARINC 429 andfitted on the top<br />
centre of the instrument panel. A GPS antenna<br />
BOEING 757-200 Installation of 21 Horse Stalls and a 10<br />
Passenger Pallet.<br />
CAA-UK AAN28344 REV. 1 A109A II AVIONICS UPGRADE FOR A109A<br />
IIInstallation of 2 x Garmin GNS430<br />
Nav/Com/GPS, 1 x Garmin<br />
GTX327Transponder, 1 x Garmin GMA340<br />
Audio Panel, Skymap KMD150 and Kannad<br />
406AF-H ELT. Also King KNI 582-<strong>01</strong>. Removal<br />
of 2 x Collins Comms, 2 xCollins Navs, Collins<br />
None The approval holder shall fulfill the<br />
obligations of Part 21,Paragraph<br />
21.A109.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
None The approval holder shall fulfill the<br />
obligations of Part 21, Paragraph<br />
21A.118A.interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
repair will introduce no adverse<br />
effectupon the airworthiness of the<br />
product<br />
A Placard is placed in clear view of the pilot<br />
and reads:GPS SYSTEM. USE ONLY<br />
DURING VFR OPERATIONAs specified in the<br />
Sloane Flight Manual Supplement No 8:1. The<br />
GPS systems to be used in VFR conditions<br />
only, for use as asupplemental navigation<br />
system.2. T<br />
The approval holder shall fulfill the<br />
obligations of Part 21, Paragraph<br />
21A.118A.Prior to installation of this<br />
modification it must be determined<br />
thatthe interrelationship between this<br />
modification and any other<br />
previouslyinstalled modification and/ or<br />
22.03.2<strong>01</strong>2<br />
22.03.2<strong>01</strong>2<br />
22.03.2<strong>01</strong>2<br />
22.03.2<strong>01</strong>2<br />
This <strong>EASA</strong> STC does not approve the<br />
rep<br />
Prior to installation of this modification it 28.03.2<strong>01</strong>2<br />
installation of Horse Boxes. The following BAC must be determined thatthe<br />
Minor Modifications must be installed as interrelationship between this modification<br />
aprerequisite for this approval:- Mod BAC- and any other previouslyinstalled<br />
820MOD<strong>01</strong>- Mod BAC-820MOD02- Mod BAC- modification and/ or repair will introduce<br />
820MOD03- Mod BAC-820MOD<strong>04</strong>- Mod BAC- no adverse effectupon the airworthiness<br />
820MOD06<br />
of the product.<br />
ONE PLACARD WITH THE WORDS "GPS<br />
LIMITED TO VFR ONLY" POSITIONED ON<br />
THEINSTRUMENT PANEL NEAR THE KMD<br />
150<br />
Prior to installation of this modification it 03.09.2<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 />
767-300<br />
Tran<br />
Installation y 276 PAX LOPA on B767-300. The following BAC minor modifications are Prior to installation of this modification it 29.10.2<strong>01</strong>2<br />
prerequisites for thismodification:(1) Mod BAC- must be determined thatthe<br />
784MOD12 Revision of Emergency safety interrelationship between this modification<br />
Equipment Layout;(2) Mod BAC-784MOD06 and any other previouslyinstalled<br />
Revision of Emergency Floor Path Lighting;(3) modification and/ or repair will introduce<br />
Mod BAC-784MOD18 Revision of the PSU no adverse effectupon the airworthiness<br />
(overhea<br />
of the product.<br />
<strong>04</strong>/<strong>01</strong>/2<strong>01</strong>3 <strong>Page</strong> 142/<strong>462</strong>
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