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 />
10039850 BOND HELICOPTERS EUROPE Ltd. EC 135 P1<br />
BOND/MOD/060 "Martin- Baker Rotating Seat None. Prior to installation of this modification it 29.05.2<strong>01</strong>2<br />
EC 135 P2<br />
Installation, EC 135"<br />
must be determined thatthe<br />
EC 135 P2+<br />
interrelationship between this modification<br />
EC 135 T1<br />
and any other previouslyinstalled<br />
EC 135 T2<br />
modification and/ or repair will introduce<br />
EC 135 T2+<br />
no adverse effectupon the airworthiness<br />
EC 635 P2+<br />
EC 635 T1<br />
EC 635 T2+<br />
of the product.<br />
10<strong>04</strong>2728 BOND HELICOPTERS EUROPE Ltd. EC135 T1,-T2,-T2+,-P1,-P2,-P2+ "East Anglia Air Ambulance Role Equipment, Limited to Aircraft with CPDS and FCDS Prior to installation of this modification it 14.12.2<strong>01</strong>2<br />
EC 135" for installation ofNVIS equipment installed.- This STC applies only to the models must be determined thatthe<br />
based on modification BOND/MOD/063 as listed above. This rotorcraftemploys Night interrelationship between this modification<br />
defined inDL/063-099.<br />
Vision Imaging System lighting, commonly and any other previouslyinstalled<br />
named NVISlighting, that has been certified to modification and/ or repair will introduce<br />
ensure the aircraft is compatiblewith<br />
no adverse effectupon the airworthiness<br />
of the product.<br />
10<strong>01</strong>4082 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4083 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4277 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4310 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4331 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4352 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4437 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4438 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4467 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4473 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4478 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4532 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4533 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4534 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4535 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4536 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4588 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4596 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
10<strong>01</strong>4636 BOURNEMOUTH AVIATION<br />
(CONSULTANTS)<br />
<strong>EASA</strong>.A.S.<strong>01</strong>174 BOEING 737-200 Revised Seating Layout of 124 Seats and 130<br />
Seats using BAC 1288 Series Seats<br />
17.03.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>175 BOEING 737-200 Deactivation of Type III Exits & Installation of a<br />
60 Seat VIP Passenger configuration.<br />
03.03.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>513 REV 2 BAE 146<br />
Installation of PRNAV Compliant UNS-1E FMS This STC is approved only for the product<br />
08.12.2006<br />
BAE 146/AVRO 146 SERIES<br />
configuration as defined in the approved design<br />
BAE 146/RJ SERIES<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.<br />
<strong>EASA</strong>.A.S.<strong>01</strong>555 BAE 146 Change EGPWS Altitude Callouts 16.03.2006<br />
<strong>EASA</strong>.A.S.<strong>01</strong>585 BOEING 737-200 Installation of Cargo Hold Smoke Detection &<br />
Fire Suppression System<br />
<strong>01</strong>.12.2005<br />
<strong>EASA</strong>.A.S.<strong>01</strong>617 BAE 146/AVRO 146 SERIES Installation of BRNAV Compliant GPS 12.12.2005<br />
<strong>EASA</strong>.A.S.02487 BAE 146-200 Layout of Passenger Accomodation (LOPA) for<br />
84, 93, 95 & 96<br />
19.<strong>04</strong>.2006<br />
<strong>EASA</strong>.A.S.02488 BOEING 737-400 Installation of 136 (16/120) PAX LOPA 07.<strong>04</strong>.2006<br />
<strong>EASA</strong>.A.S.02528 B757-200 Layout of Passenger Accommodation, C2C<br />
Seats with new audio IFE & Seat Covers.<br />
20.03.2006<br />
<strong>EASA</strong>.A.S.02534 BOEING 757-200 Layout of Passenger Accommodation - 92<br />
Business & 8 Economy/Crew<br />
20.03.2006<br />
<strong>EASA</strong>.A.S.02540 CESSNA 441 SERIES Installation of Two L Band Antennae Installation of Aircraft Registered within <strong>EASA</strong><br />
Member State only<br />
17.05.2006<br />
<strong>EASA</strong>.A.S.02618 BOMBARDIER DHC-8-100 ACS Change 7 Upgrade & Elementary -- <strong>04</strong>.08.2006<br />
SERIES<br />
Surveillance Upgrade<br />
<strong>EASA</strong>.A.S.02620 BOMBARDIER DHC-8-100<br />
SERIES<br />
Installation of HF System -- <strong>04</strong>.08.2006<br />
<strong>EASA</strong>.A.S.02621 REV 1 BOMBARDIER DHC-8-102 Installation of Dual UNS-1E Flight Management 1. This STC is approved only for the product<br />
26.<strong>01</strong>.2009<br />
BOMBARDIER DHC-8-103 System.Note: Rev.1 to STC <strong>EASA</strong>.A.S.02621 configuration as defined in the approved design<br />
adds RNP Approach Capability.<br />
data referred to in the paragraph "Description".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by the<br />
installer.2. Prior to ins<br />
<strong>EASA</strong>.A.S.02622 BOMBARDIER DHC-8-100 Installation of Aircell ST3100 Satellite -- <strong>04</strong>.08.2006<br />
SERIES<br />
Telephone System (SATCOM)<br />
<strong>EASA</strong>.A.S.02623 BOMBARDIER DHC-8-100 Installation of Universal Terrain Awareness -- <strong>04</strong>.08.2006<br />
SERIES<br />
Warning System (TAWS)<br />
<strong>EASA</strong>.A.S.02695 BOEING 737-200 Installation of 106 Seat LOPA 31.07.2006<br />
<strong>EASA</strong>.A.S.02713 BOMBARDIER CL-600-2B16 (6<strong>04</strong>) Omnibus Modification to Support Aircraft<br />
Importation.<br />
Restricted to ASN 5383. 28.11.2006<br />
<strong>EASA</strong>.A.S.02782 AIRBUS A330 Installation of Quick Access Recorder. This STC is approved only for the product<br />
configuration as defined in the approved design<br />
data referred to in the paragraph "Description<br />
& Associated Technical Documentation".<br />
Compatibility with other aircraft/engine<br />
configurations shall be determined by t<br />
02.<strong>01</strong>.2007<br />
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