Easa ad 2002-365 b pdf South Cotabato

EASA Safety Information Bulletin

One-stop support for ADS-B implementation. Revision: This AD revises EASA AD 2010-0188 dated 20 September 2010, including the B Within 3 000 EH since the last inspection accomplished before 04 October 2010 [the effective date of the original issue of this AD] in accordance with RR NMSB RB211-73-D685 Revision 3 C, Rulemaking proposal. Any person or organisation may propose the development of a new rule or an amendment thereto. More information via Rulemaking proposals..

Safety Information Bulletin

Lufttüchtigkeitsanweisung (AD). Revision: This AD revises EASA AD 2010-0188 dated 20 September 2010, including the B Within 3 000 EH since the last inspection accomplished before 04 October 2010 [the effective date of the original issue of this AD] in accordance with RR NMSB RB211-73-D685 Revision 3 C, “ADS-B OUT” is the transmission of ADS-B information out from an aircraft to other aircraft or to the ground. ADS-B OUT has been made mandatory for IFR aircraft over an extended transition period. Compliance dates for ADS-B OUT depend on whether the aircraft flies in upper or lower airspace, is newly registered or existing,.

Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS–B) Out Doc No.: WHTP-2013-14-05 Revised, August 2016 EUROCONTROL/EASA AMC 20-24 mandates ADS–B Out in production in June 8, 2016 and for entire European airspace (retrofit) by January 7, 2020. Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation.

Rulemaking proposal. Any person or organisation may propose the development of a new rule or an amendment thereto. More information via Rulemaking proposals. vom 24.12.2018 bis zum 11.01.2019 bleibt unser Betrieb geschlossen. Ab dem 14.01.2019 sind wir wieder fГјr Sie da. Wir wГјnschen ein frohes Fest und einen guten Start ins Neue Jahr 2019.

EASA AD 2016-0062 Emergency Parachute Harness – Inspection..... 21 EASA AD 2016-0044 Engine and APU Automatic Fire Extinguisher s FAA AD 2017-18-12 B/E Aerospace Protective Breathing Equipment – Inspection.. 22 * FAA AD 2017-19-05 Siemens Smoke Detectors – Inspection European third countries that participate in the activities of EASA under Article 66 of that Regulation. This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs.

ADS-B OUT (AMC 20-24): EASA Experience ¾Various applications ¾In general, EASA considers the classification of a change that introduces ADS-B is a MAJOR change. ¾However, the change may be classified as a minor change if certain conditions are met,,g e.g. • Transponder is ETSO-2C112b approved and complies with European third countries that participate in the activities of EASA under Article 66 of that Regulation. This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs.

[effective date of EASA AD 2009-0184] but no later than 30 June 2010 [original compliance date of EASA AD 2009-0184] A292 73 2830 version B Group 2 Within 750 EFH after 28 October 2010 [ the effective date of the original issue of EASA AD 2010-0215] , but no later than 14 months after 28 October 2010 [ the effective date of the of your participation to the EASA workshops is by sending an e-mail to STC_news@easa. europa.eu. In This Edition For this edition of the newsletter, we have chosen the following topics: 1. STC Workshop information 2. Technical subjects – Installation of large antennas and ADS-B 3. New regulations- New Basic Regulation 4.

FAA: F27 marks 050, 100, 200, 300, 400, 500, 600, 700 Type Certificate. Download (PDF) Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of

ADS-B SITF/11 and adopted by APANPIRG/23 Included sample template on harmonization framework 6.0 June 2013 Proposed by ADS-B SITF/12 and adopted by APANPIRG/24 Revamped to include the latest ADS-B developments and references to guidance materials on ADS-B implementation 7.0 September 2014 Proposed by ADS-B SITF/13 and adopted by APANPIRG/25 GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page nВ° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied.

This AD supersedes DGAC France AD 1999-263-134(B) dated 30 June 1999. Publication(s) and related information: Airbus SB A320-24-1092 Revision 04. Any later approved revision is acceptable. Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS–B) Out Doc No.: WHTP-2013-14-05 Revised, August 2016 EUROCONTROL/EASA AMC 20-24 mandates ADS–B Out in production in June 8, 2016 and for entire European airspace (retrofit) by January 7, 2020.

375 kb - EASA ADs - Europa.eu. Oct 28, 2016 Leonardo AW189 helicopters, serial numbers 49007 to 49021 determined that the affected windows were incorrectly installed during Rulemaking proposal. Any person or organisation may propose the development of a new rule or an amendment thereto. More information via Rulemaking proposals.

2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Executive Directorate, EASA. E-mail: ADs@easa.europa.eu. 4. Info-USA (PDF) Produkte: Übersicht Minor Changes: Minor Changes (PDF) Produkte: Wartungsanforderungen: Wartungsanforderungen (PDF) AGB: Allgemeine Geschäftsbedingungen: FAV AGB (PDF) ISO 9001:2015: ISO-Zertifikat: FAV ISO 9001:2015 (PDF) EASA APDOA: Design Organisation: EASA APDOA (PDF) EASA Part 21G: Herstellungsbetrieb: EASA Part 21G (PDF

LufttГјchtigkeitsanweisung (AD)

Global Surveillance through Space-Based ADS-B. 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Executive Directorate, EASA. E-mail: ADs@easa.europa.eu. 4., Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS-B) Out Doc No.: WHTP-2013-14-05 ADS-B Equipage Eurocontrol/EASA AMC 20-24 mandates ADS-B Out in production in January 2015 and for entire European air-space (retrofit) by December 2017..

Automatic Dependent Surveillance – Wikipedia. Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS-B) Out Doc No.: WHTP-2013-14-05 ADS-B Equipage Eurocontrol/EASA AMC 20-24 mandates ADS-B Out in production in January 2015 and for entire European air-space (retrofit) by December 2017., EASA beschlossen, eine Endfassung der LTA heraus zu geben und fordert zu Kommentaren durch die Verschiebung des öffentlichen Kommentierungsverfahrens auf den Zeitpunkt nach der Herausgabe der LTA auf. 3. Anfragen zu dieser AD sollen an die EASA Safety Information Section, Certification Directorate, gesandt werden. E-Mail: Ads@easa.europa.eu 4..

Part-145 / AMC / GM EASA

Understanding Compliance with Automatic Dependent. of your participation to the EASA workshops is by sending an e-mail to STC_news@easa. europa.eu. In This Edition For this edition of the newsletter, we have chosen the following topics: 1. STC Workshop information 2. Technical subjects – Installation of large antennas and ADS-B 3. New regulations- New Basic Regulation 4. Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation..

Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of . Rulemaking Cooperation Guidelines for the Federal Aviation Administration and the European Aviation Safety Agency . harmonisation of their rules within the scope of Articles 2.B and 6 of the Agreement. The Participants understand that harmonisation can best be achieved through effective

EASA AD 2018-0259R1: EFB USB Receptacle - Modification. With reference to EASA AD 2018-0259R1, Fokker Services issued a list of Engineering Bulletins to modify the USB receptacle LS03-05050A that are installed as part of Fokker Services provisions for an Electronic Flight Bag (EFB) solution. Rulemaking Cooperation Guidelines for the Federal Aviation Administration and the European Aviation Safety Agency . harmonisation of their rules within the scope of Articles 2.B and 6 of the Agreement. The Participants understand that harmonisation can best be achieved through effective

375 kb - EASA ADs - Europa.eu. Oct 28, 2016 Leonardo AW189 helicopters, serial numbers 49007 to 49021 determined that the affected windows were incorrectly installed during GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page nВ° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied.

2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs@easa.europa.eu. 4. This AD supersedes DGAC France AD 97-360-111(B)R1 dated 12 August 1998. Publication(s) and related information: AIRBUS INDUSTRIE SB A320-24В·1092 Revision 3 (or any further approved revision). Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA;

Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of . 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs@easa.europa.eu. 4.

Rulemaking Cooperation Guidelines for the Federal Aviation Administration and the European Aviation Safety Agency . harmonisation of their rules within the scope of Articles 2.B and 6 of the Agreement. The Participants understand that harmonisation can best be achieved through effective Jeder Iridium-NEXT-Satellit wird mit einem ADS-B-Empfänger ausgestattet. Satellitengestütztes ADS-B ermöglicht die Flugverkehrskontrolle in Regionen, die heute nicht durch ein Flugsicherungsradar abgedeckt werden. Durch die ADS-B-Empfänger auf den Iridium-NEXT-Satelliten ist der weltweite, lückenlose Empfang von ADS-B-Signalen möglich.

designated ADS-B airspaces Supported fleets • A320 family • 737NG • 777 • 767 • MD-11 … others on request The ADS-B mandate ADS-B Out is mandated by the FAA and the EASA for their respective airspace until 2020. Canada and Asia also have active ADS-B programs in effect and other countries are preparing for their ADS-B regulations. GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page n° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied.

Airworthiness Directives (ADs) and Safety Information Bulletins (SIBs) An Airworthiness Directive means a document issued or adopted by EASA which mandates actions to be performed on an aircraft to restore an acceptable level of safety, when evidence shows that … 375 kb - EASA ADs - Europa.eu. Oct 28, 2016 Leonardo AW189 helicopters, serial numbers 49007 to 49021 determined that the affected windows were incorrectly installed during

ADS-B OUT (AMC 20-24): EASA Experience ¾Various applications ¾In general, EASA considers the classification of a change that introduces ADS-B is a MAJOR change. ¾However, the change may be classified as a minor change if certain conditions are met,,g e.g. • Transponder is ETSO-2C112b approved and complies with Rulemaking proposal. Any person or organisation may propose the development of a new rule or an amendment thereto. More information via Rulemaking proposals.

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation. Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of .

This AD supersedes DGAC France AD 97-360-111(B)R1 dated 12 August 1998. Publication(s) and related information: AIRBUS INDUSTRIE SB A320-24В·1092 Revision 3 (or any further approved revision). Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; This can be an indicator dedicated to an ADS-B failure, however a single transponder failure indicator may be acceptable if the crew are able to distinguish between ADS-B device or function failures and other transponder failures using suitable troubleshooting procedures. AMC 20-24 does not contain an equivalent requirement.

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One-stop support for ADS-B implementation

Automatic Dependent Surveillance – Wikipedia. This AD supersedes DGAC France AD 97-360-111(B)R1 dated 12 August 1998. Publication(s) and related information: AIRBUS INDUSTRIE SB A320-24·1092 Revision 3 (or any further approved revision). Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA;, EASA EMERGENCY AIRWORTHINESS DIRECTIVE AD No : 2006-0105-E Date: 28. April 2006 No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with the.

Understanding Compliance with Automatic Dependent

ADS-B Operations Manual. Working Arrangement between the Hong Kong Civil Aviation Department and the European Aviation Safety Agency on validation of certificates for under 5.2.b). d) The HKCAD will assist EASA in understanding and applying its additional technical conditions., Jeder Iridium-NEXT-Satellit wird mit einem ADS-B-Empfänger ausgestattet. Satellitengestütztes ADS-B ermöglicht die Flugverkehrskontrolle in Regionen, die heute nicht durch ein Flugsicherungsradar abgedeckt werden. Durch die ADS-B-Empfänger auf den Iridium-NEXT-Satelliten ist der weltweite, lückenlose Empfang von ADS-B-Signalen möglich..

This AD supersedes DGAC France AD 1999-263-134(B) dated 30 June 1999. Publication(s) and related information: Airbus SB A320-24-1092 Revision 04. Any later approved revision is acceptable. Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; “ADS-B OUT” is the transmission of ADS-B information out from an aircraft to other aircraft or to the ground. ADS-B OUT has been made mandatory for IFR aircraft over an extended transition period. Compliance dates for ADS-B OUT depend on whether the aircraft flies in upper or lower airspace, is newly registered or existing,

Info-USA (PDF) Produkte: Übersicht Minor Changes: Minor Changes (PDF) Produkte: Wartungsanforderungen: Wartungsanforderungen (PDF) AGB: Allgemeine Geschäftsbedingungen: FAV AGB (PDF) ISO 9001:2015: ISO-Zertifikat: FAV ISO 9001:2015 (PDF) EASA APDOA: Design Organisation: EASA APDOA (PDF) EASA Part 21G: Herstellungsbetrieb: EASA Part 21G (PDF ADS-B OUT (AMC 20-24): EASA Experience ¾Various applications ¾In general, EASA considers the classification of a change that introduces ADS-B is a MAJOR change. ¾However, the change may be classified as a minor change if certain conditions are met,,g e.g. • Transponder is ETSO-2C112b approved and complies with

Rulemaking proposal. Any person or organisation may propose the development of a new rule or an amendment thereto. More information via Rulemaking proposals. Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation.

Global Surveillance through Space-Based ADS-B . 2 AIREON LLC PROPRIETARY INFORMATION Agenda Of Surveillance Through Space-Based ADS-B EASA Certification Safety is part of developing the system and maintaining operations for the life of the European third countries that participate in the activities of EASA under Article 66 of that Regulation. This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs.

EASA SIB No: 2009-33 This is information only. Recommendations are not mandatory. EASA Form 117 Page 2/2 (b) An operator shall establish a check-list system to be used by crew members for all phases of operation of the aeroplane under normal, abnormal and emergency conditions as … This AD supersedes DGAC France AD 97-360-111(B)R1 dated 12 August 1998. Publication(s) and related information: AIRBUS INDUSTRIE SB A320-24·1092 Revision 3 (or any further approved revision). Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA;

Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of . “ADS-B OUT” is the transmission of ADS-B information out from an aircraft to other aircraft or to the ground. ADS-B OUT has been made mandatory for IFR aircraft over an extended transition period. Compliance dates for ADS-B OUT depend on whether the aircraft flies in upper or lower airspace, is newly registered or existing,

Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of . unsicherer Zustand angesehen, der die Herausgabe einer Lufttüchtigkeitsanweisung (AD) entsprechend der VO(EU) 748/2012, Teil 21A.3B rechtfertigen würde. Das SIB wurde geändert, um einen Verweis auf Transpondersysteme Mode C aufzunehmen und wird gleichzeitig mit der Streichung der EASA AD 2006-0265 verbunden.

European third countries that participate in the activities of EASA under Article 66 of that Regulation. This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page nВ° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied.

Review of Aviation Mandates White Paper Introduction With commercial airspace becoming increasingly crowded, safety and EASA Forward Fit FAA ADS-B Out Forward Fit and Retrofit EASA ADS-B Out Retrofit ADS-B In DO-260A or later DO-260 or later DO-260 or later DO-260 or later GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page nВ° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied.

designated ADS-B airspaces Supported fleets • A320 family • 737NG • 777 • 767 • MD-11 … others on request The ADS-B mandate ADS-B Out is mandated by the FAA and the EASA for their respective airspace until 2020. Canada and Asia also have active ADS-B programs in effect and other countries are preparing for their ADS-B regulations. EASA AD 2018-0259R1: EFB USB Receptacle - Modification. With reference to EASA AD 2018-0259R1, Fokker Services issued a list of Engineering Bulletins to modify the USB receptacle LS03-05050A that are installed as part of Fokker Services provisions for an Electronic Flight Bag (EFB) solution.

AIRWORTHINESS DIRECTIVE. EASA AD 2018-0259R1: EFB USB Receptacle - Modification. With reference to EASA AD 2018-0259R1, Fokker Services issued a list of Engineering Bulletins to modify the USB receptacle LS03-05050A that are installed as part of Fokker Services provisions for an Electronic Flight Bag (EFB) solution., 375 kb - EASA ADs - Europa.eu. Oct 28, 2016 Leonardo AW189 helicopters, serial numbers 49007 to 49021 determined that the affected windows were incorrectly installed during.

ADS-B Aircraft Electronics Association

Lufttüchtigkeitsanweisung (AD). Supersedure: This AD supersedes EASA AD 2014-0275R1 dated 19 January 2015. compliance with the requirements of this AD. B/E Aerospace SIL D1019-01 Revision 1, dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator., ADS-B OUT (AMC 20-24): EASA Experience ¾Various applications ¾In general, EASA considers the classification of a change that introduces ADS-B is a MAJOR change. ¾However, the change may be classified as a minor change if certain conditions are met,,g e.g. • Transponder is ETSO-2C112b approved and complies with.

LufttГјchtigkeitsanweisung (AD). 375 kb - EASA ADs - Europa.eu. Oct 28, 2016 Leonardo AW189 helicopters, serial numbers 49007 to 49021 determined that the affected windows were incorrectly installed during, EASA EMERGENCY AIRWORTHINESS DIRECTIVE AD No : 2006-0105-E Date: 28. April 2006 No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with the.

Safety Information Bulletin

Lufttüchtigkeitsanweisung (AD). ADS-B SITF/11 and adopted by APANPIRG/23 Included sample template on harmonization framework 6.0 June 2013 Proposed by ADS-B SITF/12 and adopted by APANPIRG/24 Revamped to include the latest ADS-B developments and references to guidance materials on ADS-B implementation 7.0 September 2014 Proposed by ADS-B SITF/13 and adopted by APANPIRG/25 EASA AD 2016-0062 Emergency Parachute Harness – Inspection..... 21 EASA AD 2016-0044 Engine and APU Automatic Fire Extinguisher s FAA AD 2017-18-12 B/E Aerospace Protective Breathing Equipment – Inspection.. 22 * FAA AD 2017-19-05 Siemens Smoke Detectors – Inspection.

EASA SIB No: 2009-33 This is information only. Recommendations are not mandatory. EASA Form 117 Page 2/2 (b) An operator shall establish a check-list system to be used by crew members for all phases of operation of the aeroplane under normal, abnormal and emergency conditions as … Jeder Iridium-NEXT-Satellit wird mit einem ADS-B-Empfänger ausgestattet. Satellitengestütztes ADS-B ermöglicht die Flugverkehrskontrolle in Regionen, die heute nicht durch ein Flugsicherungsradar abgedeckt werden. Durch die ADS-B-Empfänger auf den Iridium-NEXT-Satelliten ist der weltweite, lückenlose Empfang von ADS-B-Signalen möglich.

EASA beschlossen, eine Endfassung der LTA heraus zu geben und fordert zu Kommentaren durch die Verschiebung des öffentlichen Kommentierungsverfahrens auf den Zeitpunkt nach der Herausgabe der LTA auf. 3. Anfragen zu dieser AD sollen an die EASA Safety Information Section, Certification Directorate, gesandt werden. E-Mail: Ads@easa.europa.eu 4. EASA AD 2016-0062 Emergency Parachute Harness – Inspection..... 21 EASA AD 2016-0044 Engine and APU Automatic Fire Extinguisher s FAA AD 2017-18-12 B/E Aerospace Protective Breathing Equipment – Inspection.. 22 * FAA AD 2017-19-05 Siemens Smoke Detectors – Inspection

Rulemaking Cooperation Guidelines for the Federal Aviation Administration and the European Aviation Safety Agency . harmonisation of their rules within the scope of Articles 2.B and 6 of the Agreement. The Participants understand that harmonisation can best be achieved through effective 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs@easa.europa.eu. 4.

Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS-B) Out Doc No.: WHTP-2013-14-05 ADS-B Equipage Eurocontrol/EASA AMC 20-24 mandates ADS-B Out in production in January 2015 and for entire European air-space (retrofit) by December 2017. Revision: This AD revises EASA AD 2010-0188 dated 20 September 2010, including the B Within 3 000 EH since the last inspection accomplished before 04 October 2010 [the effective date of the original issue of this AD] in accordance with RR NMSB RB211-73-D685 Revision 3 C

“ADS-B OUT” is the transmission of ADS-B information out from an aircraft to other aircraft or to the ground. ADS-B OUT has been made mandatory for IFR aircraft over an extended transition period. Compliance dates for ADS-B OUT depend on whether the aircraft flies in upper or lower airspace, is newly registered or existing, [effective date of EASA AD 2009-0184] but no later than 30 June 2010 [original compliance date of EASA AD 2009-0184] A292 73 2830 version B Group 2 Within 750 EFH after 28 October 2010 [ the effective date of the original issue of EASA AD 2010-0215] , but no later than 14 months after 28 October 2010 [ the effective date of the

designated ADS-B airspaces Supported fleets • A320 family • 737NG • 777 • 767 • MD-11 … others on request The ADS-B mandate ADS-B Out is mandated by the FAA and the EASA for their respective airspace until 2020. Canada and Asia also have active ADS-B programs in effect and other countries are preparing for their ADS-B regulations. [effective date of EASA AD 2009-0184] but no later than 30 June 2010 [original compliance date of EASA AD 2009-0184] A292 73 2830 version B Group 2 Within 750 EFH after 28 October 2010 [ the effective date of the original issue of EASA AD 2010-0215] , but no later than 14 months after 28 October 2010 [ the effective date of the

unsicherer Zustand angesehen, der die Herausgabe einer Lufttüchtigkeitsanweisung (AD) entsprechend der VO(EU) 748/2012, Teil 21A.3B rechtfertigen würde. Das SIB wurde geändert, um einen Verweis auf Transpondersysteme Mode C aufzunehmen und wird gleichzeitig mit der Streichung der EASA AD 2006-0265 verbunden. European third countries that participate in the activities of EASA under Article 66 of that Regulation. This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with EC 2042/2003 Annex I, Part M.A.301, the continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs.

This can be an indicator dedicated to an ADS-B failure, however a single transponder failure indicator may be acceptable if the crew are able to distinguish between ADS-B device or function failures and other transponder failures using suitable troubleshooting procedures. AMC 20-24 does not contain an equivalent requirement. GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page nВ° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied.

EASA AD 2016-0062 Emergency Parachute Harness – Inspection..... 21 EASA AD 2016-0044 Engine and APU Automatic Fire Extinguisher s FAA AD 2017-18-12 B/E Aerospace Protective Breathing Equipment – Inspection.. 22 * FAA AD 2017-19-05 Siemens Smoke Detectors – Inspection Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS-B) Out Doc No.: WHTP-2013-14-05 ADS-B Equipage Eurocontrol/EASA AMC 20-24 mandates ADS-B Out in production in January 2015 and for entire European air-space (retrofit) by December 2017.

FAA: F27 marks 050, 100, 200, 300, 400, 500, 600, 700 Type Certificate. Download (PDF) Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS-B) Out Doc No.: WHTP-2013-14-05 ADS-B Equipage Eurocontrol/EASA AMC 20-24 mandates ADS-B Out in production in January 2015 and for entire European air-space (retrofit) by December 2017.

GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page nВ° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied. Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of .

TE Emergency Airworthiness Directive

Airworthiness Directive. Review of Aviation Mandates White Paper Introduction With commercial airspace becoming increasingly crowded, safety and EASA Forward Fit FAA ADS-B Out Forward Fit and Retrofit EASA ADS-B Out Retrofit ADS-B In DO-260A or later DO-260 or later DO-260 or later DO-260 or later, 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Executive Directorate, EASA. E-mail: ADs@easa.europa.eu. 4..

EASA Safety Information Bulletin

Neuigkeiten KORFF LUFTFAHRT GMBH. designated ADS-B airspaces Supported fleets • A320 family • 737NG • 777 • 767 • MD-11 … others on request The ADS-B mandate ADS-B Out is mandated by the FAA and the EASA for their respective airspace until 2020. Canada and Asia also have active ADS-B programs in effect and other countries are preparing for their ADS-B regulations., ADS-B SITF/11 and adopted by APANPIRG/23 Included sample template on harmonization framework 6.0 June 2013 Proposed by ADS-B SITF/12 and adopted by APANPIRG/24 Revamped to include the latest ADS-B developments and references to guidance materials on ADS-B implementation 7.0 September 2014 Proposed by ADS-B SITF/13 and adopted by APANPIRG/25.

“ADS-B OUT” is the transmission of ADS-B information out from an aircraft to other aircraft or to the ground. ADS-B OUT has been made mandatory for IFR aircraft over an extended transition period. Compliance dates for ADS-B OUT depend on whether the aircraft flies in upper or lower airspace, is newly registered or existing, Revision: This AD revises EASA AD 2010-0188 dated 20 September 2010, including the B Within 3 000 EH since the last inspection accomplished before 04 October 2010 [the effective date of the original issue of this AD] in accordance with RR NMSB RB211-73-D685 Revision 3 C

Jeder Iridium-NEXT-Satellit wird mit einem ADS-B-Empfänger ausgestattet. Satellitengestütztes ADS-B ermöglicht die Flugverkehrskontrolle in Regionen, die heute nicht durch ein Flugsicherungsradar abgedeckt werden. Durch die ADS-B-Empfänger auf den Iridium-NEXT-Satelliten ist der weltweite, lückenlose Empfang von ADS-B-Signalen möglich. EASA SIB No: 2009-33 This is information only. Recommendations are not mandatory. EASA Form 117 Page 2/2 (b) An operator shall establish a check-list system to be used by crew members for all phases of operation of the aeroplane under normal, abnormal and emergency conditions as …

This AD supersedes DGAC France AD 1999-263-134(B) dated 30 June 1999. Publication(s) and related information: Airbus SB A320-24-1092 Revision 04. Any later approved revision is acceptable. Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS–B) Out Doc No.: WHTP-2013-14-05 Revised, August 2016 EUROCONTROL/EASA AMC 20-24 mandates ADS–B Out in production in June 8, 2016 and for entire European airspace (retrofit) by January 7, 2020.

designated ADS-B airspaces Supported fleets • A320 family • 737NG • 777 • 767 • MD-11 … others on request The ADS-B mandate ADS-B Out is mandated by the FAA and the EASA for their respective airspace until 2020. Canada and Asia also have active ADS-B programs in effect and other countries are preparing for their ADS-B regulations. Info-USA (PDF) Produkte: Übersicht Minor Changes: Minor Changes (PDF) Produkte: Wartungsanforderungen: Wartungsanforderungen (PDF) AGB: Allgemeine Geschäftsbedingungen: FAV AGB (PDF) ISO 9001:2015: ISO-Zertifikat: FAV ISO 9001:2015 (PDF) EASA APDOA: Design Organisation: EASA APDOA (PDF) EASA Part 21G: Herstellungsbetrieb: EASA Part 21G (PDF

This can be an indicator dedicated to an ADS-B failure, however a single transponder failure indicator may be acceptable if the crew are able to distinguish between ADS-B device or function failures and other transponder failures using suitable troubleshooting procedures. AMC 20-24 does not contain an equivalent requirement. Working Arrangement between the Hong Kong Civil Aviation Department and the European Aviation Safety Agency on validation of certificates for under 5.2.b). d) The HKCAD will assist EASA in understanding and applying its additional technical conditions.

375 kb - EASA ADs - Europa.eu. Oct 28, 2016 Leonardo AW189 helicopters, serial numbers 49007 to 49021 determined that the affected windows were incorrectly installed during vom 24.12.2018 bis zum 11.01.2019 bleibt unser Betrieb geschlossen. Ab dem 14.01.2019 sind wir wieder fГјr Sie da. Wir wГјnschen ein frohes Fest und einen guten Start ins Neue Jahr 2019.

2. The original issue of this AD was posted on 30 January 2012 as PAD 12-005 for consultation until 27 February 2012. No comments were received during the consultation period. 3. Enquiries regarding this AD should be referred to the Safety Information Section, Certification Directorate, EASA. E-mail ADs@easa.europa.eu. 4. EASA AD 2018-0259R1: EFB USB Receptacle - Modification. With reference to EASA AD 2018-0259R1, Fokker Services issued a list of Engineering Bulletins to modify the USB receptacle LS03-05050A that are installed as part of Fokker Services provisions for an Electronic Flight Bag (EFB) solution.

Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS–B) Out Doc No.: WHTP-2013-14-05 Revised, August 2016 EUROCONTROL/EASA AMC 20-24 mandates ADS–B Out in production in June 8, 2016 and for entire European airspace (retrofit) by January 7, 2020. [effective date of EASA AD 2009-0184] but no later than 30 June 2010 [original compliance date of EASA AD 2009-0184] A292 73 2830 version B Group 2 Within 750 EFH after 28 October 2010 [ the effective date of the original issue of EASA AD 2010-0215] , but no later than 14 months after 28 October 2010 [ the effective date of the

“ADS-B OUT” is the transmission of ADS-B information out from an aircraft to other aircraft or to the ground. ADS-B OUT has been made mandatory for IFR aircraft over an extended transition period. Compliance dates for ADS-B OUT depend on whether the aircraft flies in upper or lower airspace, is newly registered or existing, Global Surveillance through Space-Based ADS-B . 2 AIREON LLC PROPRIETARY INFORMATION Agenda Of Surveillance Through Space-Based ADS-B EASA Certification Safety is part of developing the system and maintaining operations for the life of the

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation. unsicherer Zustand angesehen, der die Herausgabe einer Lufttüchtigkeitsanweisung (AD) entsprechend der VO(EU) 748/2012, Teil 21A.3B rechtfertigen würde. Das SIB wurde geändert, um einen Verweis auf Transpondersysteme Mode C aufzunehmen und wird gleichzeitig mit der Streichung der EASA AD 2006-0265 verbunden.

EASA Safety Information Bulletin

Airworthiness Directive. Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of ., This AD supersedes DGAC France AD 1999-263-134(B) dated 30 June 1999. Publication(s) and related information: Airbus SB A320-24-1092 Revision 04. Any later approved revision is acceptable. Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA;.

AIRWORTHINESS DIRECTIVE. unsicherer Zustand angesehen, der die Herausgabe einer Lufttüchtigkeitsanweisung (AD) entsprechend der VO(EU) 748/2012, Teil 21A.3B rechtfertigen würde. Das SIB wurde geändert, um einen Verweis auf Transpondersysteme Mode C aufzunehmen und wird gleichzeitig mit der Streichung der EASA AD 2006-0265 verbunden., GSAC AIRWORTHINESS DIRECTIVE ref. : 2002-365(B) Page n° 2 3. Within 600 flight hours from the effective date of this AD, perform the additional test required after the relocation of the relay 11QG, in accordance with SB A320-24-1092 Revision 4. Note: This additional test is mandatory even with SB A320-24-1092 Revision 1, 2 or 3 already embodied..

EASA Safety Publications Tool

Automatic Dependent Surveillance – Wikipedia. This AD supersedes DGAC France AD 1999-263-134(B) dated 30 June 1999. Publication(s) and related information: Airbus SB A320-24-1092 Revision 04. Any later approved revision is acceptable. Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA; ADS-B OUT (AMC 20-24): EASA Experience ¾Various applications ¾In general, EASA considers the classification of a change that introduces ADS-B is a MAJOR change. ¾However, the change may be classified as a minor change if certain conditions are met,,g e.g. • Transponder is ETSO-2C112b approved and complies with.

Review of Aviation Mandates White Paper Introduction With commercial airspace becoming increasingly crowded, safety and EASA Forward Fit FAA ADS-B Out Forward Fit and Retrofit EASA ADS-B Out Retrofit ADS-B In DO-260A or later DO-260 or later DO-260 or later DO-260 or later This AD supersedes DGAC France AD 1999-263-134(B) dated 30 June 1999. Publication(s) and related information: Airbus SB A320-24-1092 Revision 04. Any later approved revision is acceptable. Remarks: Comments regarding this AD should be referred to the Programming and Continued Airworthiness Information Section, Certification Directorate, EASA;

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of 2. Based on the required actions and the compliance time, EASA have decided to issue a Final AD with Request for Comments, postponing the public consultation process until after publication. 3. Enquiries regarding this AD should be referred to the EASA Safety Information Section, Certification Directorate. E-mail: ADs@easa.europa.eu. 4.

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of Understanding Compliance with Automatic Dependent Surveillance – Broadcast (ADS–B) Out Doc No.: WHTP-2013-14-05 Revised, August 2016 EUROCONTROL/EASA AMC 20-24 mandates ADS–B Out in production in June 8, 2016 and for entire European airspace (retrofit) by January 7, 2020.

unsicherer Zustand angesehen, der die Herausgabe einer Lufttüchtigkeitsanweisung (AD) entsprechend der VO(EU) 748/2012, Teil 21A.3B rechtfertigen würde. Das SIB wurde geändert, um einen Verweis auf Transpondersysteme Mode C aufzunehmen und wird gleichzeitig mit der Streichung der EASA AD 2006-0265 verbunden. Review of Aviation Mandates White Paper Introduction With commercial airspace becoming increasingly crowded, safety and EASA Forward Fit FAA ADS-B Out Forward Fit and Retrofit EASA ADS-B Out Retrofit ADS-B In DO-260A or later DO-260 or later DO-260 or later DO-260 or later

EASA EMERGENCY AIRWORTHINESS DIRECTIVE AD No : 2006-0105-E Date: 28. April 2006 No person may operate an aircraft to which an Airworthiness Directive applies, except in accordance with the unsicherer Zustand angesehen, der die Herausgabe einer Lufttüchtigkeitsanweisung (AD) entsprechend der VO(EU) 748/2012, Teil 21A.3B rechtfertigen würde. Das SIB wurde geändert, um einen Verweis auf Transpondersysteme Mode C aufzunehmen und wird gleichzeitig mit der Streichung der EASA AD 2006-0265 verbunden.

This can be an indicator dedicated to an ADS-B failure, however a single transponder failure indicator may be acceptable if the crew are able to distinguish between ADS-B device or function failures and other transponder failures using suitable troubleshooting procedures. AMC 20-24 does not contain an equivalent requirement. EASA SIB No: 2009-33 This is information only. Recommendations are not mandatory. EASA Form 117 Page 2/2 (b) An operator shall establish a check-list system to be used by crew members for all phases of operation of the aeroplane under normal, abnormal and emergency conditions as …

ADS-B OUT (AMC 20-24): EASA Experience ¾Various applications ¾In general, EASA considers the classification of a change that introduces ADS-B is a MAJOR change. ¾However, the change may be classified as a minor change if certain conditions are met,,g e.g. • Transponder is ETSO-2C112b approved and complies with EASA SIB No: 2009-33 This is information only. Recommendations are not mandatory. EASA Form 117 Page 2/2 (b) An operator shall establish a check-list system to be used by crew members for all phases of operation of the aeroplane under normal, abnormal and emergency conditions as …

Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of . Supersedure: This AD supersedes EASA AD 2014-0275R1 dated 19 January 2015. compliance with the requirements of this AD. B/E Aerospace SIL D1019-01 Revision 1, dated 03 January 2000, provides instructions for the activation and the disposal of a removed generator.

Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation (EC) No 216/2008 on behalf of the European Community, its Member States and of the European third countries that participate in the activities of EASA under Article 66 of that Regulation. unsicherer Zustand angesehen, der die Herausgabe einer Lufttüchtigkeitsanweisung (AD) entsprechend der VO(EU) 748/2012, Teil 21A.3B rechtfertigen würde. Das SIB wurde geändert, um einen Verweis auf Transpondersysteme Mode C aufzunehmen und wird gleichzeitig mit der Streichung der EASA AD 2006-0265 verbunden.

ADS-B SITF/11 and adopted by APANPIRG/23 Included sample template on harmonization framework 6.0 June 2013 Proposed by ADS-B SITF/12 and adopted by APANPIRG/24 Revamped to include the latest ADS-B developments and references to guidance materials on ADS-B implementation 7.0 September 2014 Proposed by ADS-B SITF/13 and adopted by APANPIRG/25 [effective date of EASA AD 2009-0184] but no later than 30 June 2010 [original compliance date of EASA AD 2009-0184] A292 73 2830 version B Group 2 Within 750 EFH after 28 October 2010 [ the effective date of the original issue of EASA AD 2010-0215] , but no later than 14 months after 28 October 2010 [ the effective date of the

ADS-B SITF/11 and adopted by APANPIRG/23 Included sample template on harmonization framework 6.0 June 2013 Proposed by ADS-B SITF/12 and adopted by APANPIRG/24 Revamped to include the latest ADS-B developments and references to guidance materials on ADS-B implementation 7.0 September 2014 Proposed by ADS-B SITF/13 and adopted by APANPIRG/25 Training Material EASA Part 21 AMC & GM EASA Part 21 Acceptable Means of Compliance & Guidance Material . AMC & GM to Subpart A. General Provisions . AMC & GM to Subpart J. Design Organisation Approval (DOA) AMC 21.A.3A(b)(2) Reporting to the Agency . Within the overall limit of .