Nachrichten für Luftfahrer 2019 Teil 2 (weicht ggf. von Druckversion ab)
EASA AD No.: 2019-0049
Consequently, for an aeroplane to which that AMP applies, it is acceptable to accomplish the
new and/or more restrictive tasks as specified in the ALS, as applicable to aeroplane model and
depending on aeroplane configuration, within the compliance times (see Note 1 of this AD) as
specified in the ALS, to comply with paragraph (1) of this AD.
For that AMP, it is acceptable to incorporate the new and/or more restrictive tasks as specified
in the ALS, as applicable to aeroplane model and depending on aeroplane configuration, into
the AMP to comply with paragraph (3) of this AD.
Recording AD compliance:
(5) When the AMP of an aeroplane has been revised as required by paragraph (3) or (4) of this AD,
as applicable, that action ensures continued accomplishment of the tasks as required by
paragraphs (1) and (2) of this AD for that aeroplane. Consequently, after revising the AMP, as
required by paragraph (3) or (4) of this AD, as applicable, it is not necessary that
accomplishment of individual action is recorded for demonstration of AD compliance on a
continued basis.
Ref. Publications:
Airbus A330 ALS Part 3 Revision 06 dated 15 October 2018.
The use of later approved revisions and variations of the above-mentioned document is acceptable
for compliance with the requirements of this AD.
Remarks:
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 17 December 2018 as PAD 18-179 for consultation until 14 January
2019. The Comment Response Document can be found in the EASA Safety Publications Tool, in
the compressed (zipped) file attached to the record for this AD.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs@easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on
a product, part or appliance not affected by this AD, can be reported to the EU aviation safety
reporting system.
5. For any question concerning the technical content of the requirements in this AD, please
contact: AIRBUS – EIAL (Airworthiness Office), E-mail: airworthiness.A330-A340@airbus.com.
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Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2019-069 38144 Braunschweig
EASA AD 2019-0050 vom 11.03.2019 Fax: +49-531-2355-5298
email: ad@LBA.de
AIRBUS 15.03.2019
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: AIRBUS S.A.S.
Hersteller: Airbus (vormals Airbus Industrie)
Muster: A340
Baureihen: A340-211, A340-212, A340-213, A340-311, A340-312, A340-313,
A340-541, A340-542, A340-642 und A340-643
Werknummern: Alle
Gerätenummer: 2850, EASA.A.015
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA AD 2019-0050 vom 11.03.2019
Genannte Airworthiness Directives unter dieser Rubrik, die nicht durch die EASA herausgegeben worden sind,
wurden durch die EASA über die Entscheidung Nr. 02/2003 übernommen und sind somit ebenfalls Airworthiness
Directives der EASA.
Die genannte Airworthiness Directive wird im Luftfahrt-Bundesamt unter der Nummer 2019-069 geführt.
Betrifft:
(ATA 05) Time Limits / Maintenance Checks - Airworthiness Limitations Section Part 3 - Certification Maintenance
Requirements - Amendment
Anmerkungen:
Gemäß der EU Verordnung Nr. 1321/2014, Anhang I, Teil M, Unterabschnitt C, M.A.301 5.i) und M.A.303 dür-
fen Luftfahrzeuge nach dem in der Lufttüchtigkeitsanweisung angegebenen Termin nur in Betrieb genom-
men werden, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind.
Die Europäische Agentur für Flugsicherheit (EASA) hat die oben referenzierte Lufttüchtigkeitsanweisung
EASA AD 2019-0050 vom 11.03.2019 herausgegeben oder per Entscheidung Nr. 02/2003 übernommen.
Gemäß § 14 Abs. 2 der Betriebsordnung für Luftfahrtgerät (LuftBO) sind diese Lufttüchtigkeitsanweisun-
gen direkt in der Bundesrepublik Deutschland gültig und bedürfen keiner Umsetzung durch das Luftfahrt-
Bundesamt.
Mit Hilfe dieser Übersichtsseite veröffentlicht das Luftfahrt-Bundesamt ebenfalls die über § 14 Abs. 2 direkt
gültigen Lufttüchtigkeitsanweisungen der EASA in den Nachrichten für Luftfahrer und im Internet unter
www2.LBA.de/LTAs/. Dieser Service dient reinen Informationszwecken und liegt keinem Verwaltungsver-
fahren zu Grunde. Rechtsmittel sind damit ausgeschlossen.
D-2019-069 Seite 1 von 1 119/2019
EASA AD No.: 2019-0050
Airworthiness Directive
AD No.: 2019-0050
Issued: 11 March 2019
Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation
(EU) 2018/1139 on behalf of the European Union, its Member States and of the European third
countries that participate in the activities of EASA under Article 129 of that Regulation.
This AD is issued in accordance with Regulation (EU) 748/2012, Part 21.A.3B. In accordance with Regulation (EU) 1321/2014 Annex I, Part M.A.301, the
continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which
an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I,
Part M.A.303] or agreed with the Authority of the State of Registry [Regulation (EU) 2018/1139, Article 71 exemption].
Design Approval Holder’s Name: Type/Model designation(s):
AIRBUS A340 aeroplanes
Effective Date: 25 March 2019
TCDS Number(s): EASA.A.015
Foreign AD: Not applicable
Supersedure: None
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section
Part 3 – Certification Maintenance Requirements – Amendment
Manufacturer(s):
Airbus, formerly Airbus Industrie
Applicability:
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541, A340-542,
A340-642 and A340-643 aeroplanes, all manufacturer serial numbers (MSN).
Definitions:
For the purpose of this AD, the following definitions apply:
The ALS: Airbus A340 Airworthiness Limitations Section (ALS) Part 3, Revision 04.
The AMP: The approved Aircraft Maintenance Programme (AMP) on the basis of which the
operator or the owner ensures the continuing airworthiness of each operated aeroplane. For
aeroplanes registered in Europe, complying with the approved AMP is required by Commission
Regulation (EU) 1321/2014, Part M.A.301, paragraph 3.
New and/or more restrictive tasks: This includes all tasks that are new and all tasks for which a
threshold or interval was reduced, which were introduced into the ALS (as defined in this AD) since
the previous ALS Revision that is currently incorporated in the AMP.
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EASA AD No.: 2019-0050
Reason:
The airworthiness limitations for the Airbus A340 aeroplanes, which are approved by EASA, are
currently defined and published in the A340 ALS documents. The airworthiness limitations
applicable to the Certification Maintenance Requirements (CMR), which are approved by EASA, are
published in the ALS.
Failure to accomplish these instructions could result in an unsafe condition.
Previously, EASA issued AD 2016-0066 to require accomplishment of all maintenance tasks as
described in A340 ALS Part 3 at Revision 03.
Since that AD was issued, Airbus published the ALS, including new and/or more restrictive
requirements.
For the reasons described above, this AD takes over the requirements for Airbus A340 aeroplanes
from EASA AD 2016-0066 and requires accomplishment of the actions specified in the ALS.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
Maintenance Tasks:
(1) From the effective date of this AD, within the thresholds and intervals as specified in the ALS
(see Note 1 of this AD), accomplish all tasks as specified in the ALS, as applicable to aeroplane
model and depending on aeroplane configuration.
Note 1: For the purpose of this AD, the thresholds and intervals as defined in the ‘Compliance Time’
pages of the ALS include specific compliance times for certain tasks.
Corrective Action(s):
(2) In case of finding discrepancies during accomplishment of any task as required by paragraph (1)
of this AD, before next flight, accomplish the applicable corrective action(s) in accordance with
the applicable Airbus maintenance documentation. If a detected discrepancy cannot be
corrected by using existing Airbus instructions, before next flight, contact Airbus for approved
instructions and accomplish those instructions accordingly.
AMP Revision:
(3) Within 12 months after the effective date of this AD, revise the approved AMP by incorporating
the maintenance tasks and associated thresholds and intervals described in the ALS, as
applicable to aeroplane model and depending on aeroplane configuration.
Credit:
(4) If, before the effective date of this AD, the AMP has been revised to incorporate the tasks as
specified in A340 ALS Part 3 at Revision 03, that action ensures the continued accomplishment
of those tasks.
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EASA AD No.: 2019-0050
Consequently, for an aeroplane to which that AMP applies, it is acceptable to accomplish the
new and/or more restrictive tasks as specified in the ALS, as applicable to aeroplane model and
depending on aeroplane configuration, within the compliance times (see Note 1 of this AD) as
specified in the ALS, to comply with paragraph (1) of this AD.
For that AMP, it is acceptable to incorporate the new and/or more restrictive tasks, as
applicable to aeroplane model and depending on aeroplane configuration, as specified in the
ALS, into the AMP to comply with paragraph (3) of this AD.
Recording AD compliance:
(5) When the AMP of an aeroplane has been revised as required by paragraph (3) or (4) of this AD,
as applicable, that action ensures continued accomplishment of the tasks as required by
paragraphs (1) and (2) of this AD for that aeroplane. Consequently, after revising the AMP, as
required by paragraph (3) or (4) of this AD, as applicable, it is not necessary that
accomplishment of individual action is recorded for demonstration of AD compliance on a
continued basis.
Ref. Publications:
Airbus A340 ALS Part 3 Revision 04 dated 15 October 2018.
The use of later approved revisions and variations of the above-mentioned document is acceptable
for compliance with the requirements of this AD.
Remarks:
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. This AD was posted on 17 December 2018 as PAD 18-180 for consultation until 14 January
2019. No comments were received during the consultation period.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs@easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on
a product, part or appliance not affected by this AD, can be reported to the EU aviation safety
reporting system.
5. For any question concerning the technical content of the requirements in this AD, please
contact: AIRBUS – EIAL (Airworthiness Office), E-mail: airworthiness.A330-A340@airbus.com.
TE.CAP.00110-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 3 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2019-070 38144 Braunschweig
EASA Emergency AD 2019-0055-E vom Fax: +49-531-2355-5298
18.03.2019 email: ad@LBA.de
ROTAX 18.03.2019
DRINGEND!
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugmotor
Inhaber der Musterzulassung: BRP-ROTAX GmbH & Co. KG
Hersteller: BRP-Rotax GmbH & Co. KG, vormals BRP-Powertrain GmbH & Co. KG,
Bombardier-Rotax GmbH & Co. KG, Bombardier-Rotax GmbH
Muster: ROTAX 912
ROTAX 915
Baureihen: Rotax 912 iSc2 Sport, 912 iSc3 Sport und Rotax 915 iSc3 A
Werknummern: Alle
Die betroffenen Flugmotoren sind in diversen Luftfahrzeugen der Allgemeinen
Luftfahrt installiert, aber nicht unbedingt auf diese beschränkt. Die Installation
der betroffenen Flugmotoren kann entweder mit der Musterzulassung der
Luftfahrzeuge oder als Ergänzende Musterzulassung mit einem "Supplemental
Type Certificate" (STC) zugelassen worden sein.
Gerätenummer: EASA.E.121
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA Emergency AD 2019-0055-E vom 18.03.2019
Genannte Airworthiness Directives unter dieser Rubrik, die nicht durch die EASA herausgegeben worden sind,
wurden durch die EASA über die Entscheidung Nr. 02/2003 übernommen und sind somit ebenfalls Airworthiness
Directives der EASA.
Die genannte Airworthiness Directive wird im Luftfahrt-Bundesamt unter der Nummer 2019-070 geführt.
Betrifft:
(ATA 73) Engine Fuel and Control - Fuel Pump Assembly - Inspection / Replacement
Anmerkungen:
Gemäß der EU Verordnung Nr. 1321/2014, Anhang I, Teil M, Unterabschnitt C, M.A.301 5.i) und M.A.303 dür-
fen Luftfahrzeuge nach dem in der Lufttüchtigkeitsanweisung angegebenen Termin nur in Betrieb genom-
men werden, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind.
Die Europäische Agentur für Flugsicherheit (EASA) hat die oben referenzierte Lufttüchtigkeitsanweisung
EASA Emergency AD 2019-0055-E vom 18.03.2019 herausgegeben oder per Entscheidung Nr. 02/2003
übernommen.
Gemäß § 14 Abs. 2 der Betriebsordnung für Luftfahrtgerät (LuftBO) sind diese Lufttüchtigkeitsanweisun-
gen direkt in der Bundesrepublik Deutschland gültig und bedürfen keiner Umsetzung durch das Luftfahrt-
Bundesamt.
Mit Hilfe dieser Übersichtsseite veröffentlicht das Luftfahrt-Bundesamt ebenfalls die über § 14 Abs. 2 direkt
gültigen Lufttüchtigkeitsanweisungen der EASA in den Nachrichten für Luftfahrer und im Internet unter
www2.LBA.de/LTAs/. Dieser Service dient reinen Informationszwecken und liegt keinem Verwaltungsver-
fahren zu Grunde. Rechtsmittel sind damit ausgeschlossen.
D-2019-070 Seite 1 von 1 125/2019
EASA AD No.: 2019-0055-E
Emergency Airworthiness Directive
AD No.: 2019-0055-E
Issued: 18 March 2019
Note: This Emergency Airworthiness Directive (AD) is issued by EASA, acting in accordance with
Regulation (EU) 2018/1139 on behalf of the European Union, its Member States and of the
European third countries that participate in the activities of EASA under Article 129 of that
Regulation.
This AD is issued in accordance with Regulation (EU) 748/2012, Part 21.A.3B. In accordance with Regulation (EU) 1321/2014 Annex I, Part M.A.301, the
continuing airworthiness of an aircraft shall be ensured by accomplishing any applicable ADs. Consequently, no person may operate an aircraft to which
an AD applies, except in accordance with the requirements of that AD, unless otherwise specified by the Agency [Regulation (EU) 1321/2014 Annex I,
Part M.A.303] or agreed with the Authority of the State of Registry [Regulation (EU) 2018/1139, Article 71 exemption].
Design Approval Holder’s Name: Type/Model designation(s):
BRP-ROTAX GmbH & Co KG Rotax 912 and 915 engines
Effective Date: 20 March 2019
TCDS Number(s): EASA.E.121
Foreign AD: Not applicable
Supersedure: None
ATA 73 – Engine fuel and Control – Fuel Pump Assembly – Inspection / Replacement
Manufacturer(s):
BRP-Rotax GmbH & Co KG, formerly BRP-Powertrain GmbH & Co. KG, Bombardier-Rotax GmbH &
Co. KG, Bombardier-Rotax GmbH
Applicability:
Rotax 912 iSc2 Sport, 912 iSc3 Sport and Rotax 915 iSc3 A engines, all serial numbers (s/n).
These engines are known to be installed on, but not limited to, various general aviation aeroplane
types and models. The installation of these engines was either done by the respective aeroplane
manufacturer, or through modification of the aeroplane by Supplemental Type Certificate (STC).
Definitions:
For the purpose of this AD, the following definitions apply:
The ASB: BRP-Rotax Alert Service Bulletin (ASB) ASB-912 i-010 / ASB-915 i A-006 (single document).
Affected part: Fuel pump assemblies, having part number (P/N) 889696 (part of assembly
P/N 889697) and s/n from 180500 to 189999 inclusive; or having P/N 889698 (part of assembly
P/N 889699) and s/n from 180500 to 189999 inclusive.
TE.CAP.00111-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 3
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EASA AD No.: 2019-0055-E
Serviceable part: Fuel pump assemblies which are not an affected part; or an affected part which
passes an inspection (no defects found) in accordance with the instructions of the ASB.
Groups: Group 1 engines have an affected part installed. Group 2 engines do not have an affected
part installed.
Reason:
Fuel leakage was observed on an engine still on the production line. Subsequent investigation
determined a manufacturing issue as root cause of the fuel leak, and a batch of fuel pump
assemblies was identified which could experience similar fuel leaks.
This condition, if not detected and corrected, could lead to engine fire, possibly resulting in a forced
landing with consequent damage to the aeroplane and injury to occupants.
To address this potential unsafe condition, BRP-Rotax issued the ASB, providing inspection
instructions.
For the reason described above, this AD requires a one-time inspection of the affected parts and,
depending on findings, replacement. This AD also provides additional requirements for installation
of a fuel pump assembly on an engine.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
Inspection:
(1) For Group 1 engines: Before next engine operation after the effective date of this AD, inspect
the affected part in accordance with the instructions of the ASB.
Corrective action(s):
(1) If, during the inspection as required by paragraph (1) of this AD, any discrepancy is found, as
identified in the ASB, before next engine operation, replace the affect part in accordance with
the instructions of the ASB.
Part(s) Installation:
(3) For Group 1 and Group 2 engines: From the effective date of this AD, it is allowed to install on
any engine a fuel pump assembly, provided that it is a serviceable part, as defined in this AD.
Ref. Publications:
BRP-Rotax ASB-912 i-010 / ASB-915 i A-006 (single document) original issue dated 13 March 2019.
The use of later approved revisions of the above-mentioned document is acceptable for compliance
with the requirements of this AD.
Remarks:
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
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EASA AD No.: 2019-0055-E
2. The results of the safety assessment have indicated the need for immediate publication and
notification, without the full consultation process.
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs@easa.europa.eu.
4. Information about any failures, malfunctions, defects or other occurrences, which may be
similar to the unsafe condition addressed by this AD, and which may occur, or have occurred on
a product, part or appliance not affected by this AD, can be reported to the EU aviation safety
reporting system.
5. For any question concerning the technical content of the requirements in this AD, please
contact: BRP-Rotax GmbH & Co KG, Telephone: +43 7246 601 0, Fax: +43 7246 601 9130,
E-mail: airworthiness@brp.com, Website www.flyrotax.com.
TE.CAP.00111-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 3 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2019-070R1 38144 Braunschweig
EASA Emergency AD 2019-0055-E (Correction: Fax: +49-531-2355-5298
19.03.2019) vom 18.03.2019 email: ad@LBA.de
ROTAX 19.03.2019
DRINGEND!
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugmotor
Inhaber der Musterzulassung: BRP-ROTAX GmbH & Co. KG
Hersteller: BRP-Rotax GmbH & Co. KG, vormals BRP-Powertrain GmbH & Co. KG,
Bombardier-Rotax GmbH & Co. KG, Bombardier-Rotax GmbH
Muster: ROTAX 912
ROTAX 915
Baureihen: Rotax 912 iSc2 Sport, 912 iSc3 Sport und Rotax 915 iSc3 A
Werknummern: Alle
Die betroffenen Flugmotoren sind in diversen Luftfahrzeugen der Allgemeinen
Luftfahrt installiert, aber nicht unbedingt auf diese beschränkt. Die Installation
der betroffenen Flugmotoren kann entweder mit der Musterzulassung der
Luftfahrzeuge oder als Ergänzende Musterzulassung mit einem "Supplemental
Type Certificate" (STC) zugelassen worden sein.
Gerätenummer: EASA.E.121
Revisionsstand:
Diese LTA ersetzt D-2019-070 vom 18.03.2019
Airworthiness Directive der ausländischen Behörde:
EASA Emergency AD 2019-0055-E (Correction: 19.03.2019) vom 18.03.2019
Genannte Airworthiness Directives unter dieser Rubrik, die nicht durch die EASA herausgegeben worden sind,
wurden durch die EASA über die Entscheidung Nr. 02/2003 übernommen und sind somit ebenfalls Airworthiness
Directives der EASA.
Die genannte Airworthiness Directive wird im Luftfahrt-Bundesamt unter der Nummer 2019-070R1 geführt.
Betrifft:
(ATA 73) Engine Fuel and Control - Fuel Pump Assembly - Inspection / Replacement
Anmerkungen:
Gemäß der EU Verordnung Nr. 1321/2014, Anhang I, Teil M, Unterabschnitt C, M.A.301 5.i) und M.A.303 dür-
fen Luftfahrzeuge nach dem in der Lufttüchtigkeitsanweisung angegebenen Termin nur in Betrieb genom-
men werden, wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind.
Die Europäische Agentur für Flugsicherheit (EASA) hat die oben referenzierte Lufttüchtigkeitsanweisung
EASA Emergency AD 2019-0055-E (Correction: 19.03.2019) vom 18.03.2019 herausgegeben oder per Ent-
scheidung Nr. 02/2003 übernommen.
Gemäß § 14 Abs. 2 der Betriebsordnung für Luftfahrtgerät (LuftBO) sind diese Lufttüchtigkeitsanweisun-
gen direkt in der Bundesrepublik Deutschland gültig und bedürfen keiner Umsetzung durch das Luftfahrt-
Bundesamt.
Mit Hilfe dieser Übersichtsseite veröffentlicht das Luftfahrt-Bundesamt ebenfalls die über § 14 Abs. 2 direkt
gültigen Lufttüchtigkeitsanweisungen der EASA in den Nachrichten für Luftfahrer und im Internet unter
www2.LBA.de/LTAs/. Dieser Service dient reinen Informationszwecken und liegt keinem Verwaltungsver-
fahren zu Grunde. Rechtsmittel sind damit ausgeschlossen.
D-2019-070R1 Seite 1 von 1 129/2019
