Nachrichten für Luftfahrer 2019 Teil 2 (weicht ggf. von Druckversion ab)
EASA AD No.: 2019-0047
Airworthiness Directive
AD No.: 2019-0047
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 A330 aeroplanes
Effective Date: 25 March 2019
TCDS Number(s): EASA.A.004
Foreign AD: Not applicable
Supersedure: None
ATA 05 – Time Limits / Maintenance Checks – Airworthiness Limitations Section
Part 4 – System Equipment Maintenance Requirements – Amendment
Manufacturer(s):
Airbus, formerly Airbus Industrie
Applicability:
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301,
A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343
aeroplanes, all manufacturer serial numbers.
Definitions:
For the purpose of this AD, the following definitions apply:
The ALS: Airbus A330 Airworthiness Limitations Section (ALS) Part 4 Revision 07.
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, and which were introduced into the ALS (as defined in this AD)
since the previous ALS Revision that is currently incorporated in the AMP.
TE.CAP.00110-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
EASA AD No.: 2019-0047
Reason:
The airworthiness limitations for the Airbus A330 aeroplanes, which are approved by EASA, are
currently defined and published in the A330 ALS documents. The airworthiness limitations
applicable to the System Equipment Maintenance Requirements, 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 2017-0228 to require accomplishment of all maintenance tasks as
described in A330 ALS Part 4 at Revision 06.
Since that AD was issued, Airbus published the ALS, as defined in this AD, including new and/or
more restrictive tasks.
For the reasons described above, this AD takes over the requirements for Airbus A330 aeroplanes
from EASA AD 2017-0228, and requires accomplishment of the actions specified in the ALS.
This AD also takes over Airbus A330 requirements from EASA AD 2013-0201 and AD 2017-0044, as
the requirements of these ADs have been embodied into the ALS.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
Maintenance Tasks and Replacement of Life Limited Parts:
(1) From the effective date of this AD, accomplish the actions as specified in the applicable ALS, as
required by paragraph (1.1) and (1.2) of this AD.
(1.1) Replace each component before exceeding the applicable life limit.
(1.2) Within the thresholds and intervals (see Note 1 of this AD), accomplish all applicable
maintenance tasks.
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 applicable ALS,
as applicable to aeroplane model and depending on aeroplane configuration.
TE.CAP.00110-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
EASA AD No.: 2019-0047
Credit:
(4) If, before the effective date of this AD, the AMP has been revised to incorporate the tasks as
specified in a previous applicable ALS Part 4 Revision 06, that action ensures the continued
accomplishment of those tasks.
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, 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 4 Revision 07 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 25 January 2019 as PAD 19-012 for consultation until 22 February 2019.
The Comment Response Documents 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.
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-2019-067 38144 Braunschweig
EASA AD 2019-0048 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 2019-0048 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 2019-067 geführt.
Betrifft:
(ATA 05) Time Limits / Maintenance Checks - Airworthiness Limitations Section Part 4 - System Equipment
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 2019-0048 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-2019-067 Seite 1 von 1 117/2019
EASA AD No.: 2019-0048
Airworthiness Directive
AD No.: 2019-0048
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 4 – System Equipment 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.
Definitions:
For the purpose of this AD, the following definitions apply:
The ALS: Airbus A340 Airworthiness Limitations Section (ALS) Part 4 Revision 06.
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, and which were introduced into the ALS (as defined in this AD)
since the previous ALS Revision that is currently incorporated in the AMP.
TE.CAP.00110-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
EASA AD No.: 2019-0048
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 System Equipment Maintenance Requirements, 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 2017-0228 to require accomplishment of all maintenance tasks as
described in A340 ALS Part 4 at Revision 05.
Since that AD was issued, Airbus published the ALS, as defined in this AD, including new and/or
more restrictive tasks.
For the reasons described above, this AD takes over the requirements for Airbus A340 aeroplanes
from EASA AD 2017-0228, and requires accomplishment of the actions specified in the ALS.
This AD also takes over Airbus A340 requirements from EASA AD 2013-0201 and AD 2017-0044, as
the requirements of these ADs have been embodied into the ALS.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
Maintenance Tasks and Replacement of Life Limited Parts:
(1) From the effective date of this AD, accomplish the actions as specified in the applicable ALS, as
required by paragraph (1.1) and (1.2) of this AD.
(1.1) Replace each component before exceeding the applicable life limit.
(1.2) Within the thresholds and intervals (see Note 1 of this AD), accomplish all applicable
maintenance tasks.
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 applicable ALS,
as applicable to aeroplane model and depending on aeroplane configuration.
TE.CAP.00110-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
EASA AD No.: 2019-0048
Credit:
(4) If, before the effective date of this AD, the AMP has been revised to incorporate the tasks as
specified in a previous applicable ALS Part 4 Revision 05, that action ensures the continued
accomplishment of those tasks.
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, 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 A340 ALS Part 4 Revision 06, dated 15 October 2018.
The use of later approved revisions or 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 25 January 2019 as PAD 19-013 for consultation until 22 February 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-2019-068 38144 Braunschweig
EASA AD 2019-0049 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: A330
Baureihen: A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F,
A330-301, A330-302, A330-303, A330-321, A330-322, A330-323, A330-341,
A330-342 und A330-343
Werknummern: Alle
Gerätenummer: 2849, EASA.A.004
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA AD 2019-0049 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 2019-068 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 2019-0049 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-2019-068 Seite 1 von 1 118/2019
EASA AD No.: 2019-0049
Airworthiness Directive
AD No.: 2019-0049
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 A330 aeroplanes
Effective Date: 25 March 2019
TCDS Number(s): EASA.A.004
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 A330-201, A330-202, A330-203, A330-223, A330-223F, A330-243, A330-243F, A330-301,
A330-302, A330-303, A330-321, A330-322, A330-323, A330-341, A330-342 and A330-343
aeroplanes, all manufacturer serial numbers (MSN).
Definitions:
For the purpose of this AD, the following definitions apply:
The ALS: Airbus A330 Airworthiness Limitations Section (ALS) Part 3, Revision 06.
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.
TE.CAP.00110-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 1 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
EASA AD No.: 2019-0049
Reason:
The airworthiness limitations for the Airbus A330 aeroplanes, which are approved by EASA, are
currently defined and published in the A330 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 A330 ALS Part 3 at Revision 05.
Since that AD was issued, Airbus published the ALS, as defined in this AD, including new and/or
more restrictive tasks.
For the reasons described above, this AD takes over the requirements for Airbus A330 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 defined 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) For an AMP that, on the effective date of this AD, is already updated to incorporate the tasks as
specified in a previous ALS Part 3 Revision 05, that action ensures the continued
accomplishment of those tasks.
TE.CAP.00110-009 © European Union Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 2 of 3
Proprietary document. Copies are not controlled. Confirm revision status through the EASA-Internet/Intranet.
An agency of the European Union
