Nachrichten für Luftfahrer 2016 Teil 2 (weicht ggf. von Druckversion ab)
EASA AD No.: 2016-0029R1
Remarks:
1. If requested and appropriately substantiated, EASA can approve Alternative Methods of
Compliance for this AD.
2. The original issue of this AD was posted on 19 January 2016 as PAD 16-003 for consultation
until 16 February 2016. 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. For any question concerning the technical content of the requirements in this AD, please
contact: Fokker Services B.V., Technical Services Dept., P.O. Box 1357, 2130 EL, Hoofddorp,
The Netherlands, Telephone +31-88-6280-350, Fax +31-88-6280-111,
E-mail: technicalservices@fokker.com.
The referenced publication can be downloaded from www.myfokkerfleet.com.
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Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2016-287 38144 Braunschweig
EASA AD 2016-0210 vom 24.10.2016 Fax: +49-531-2355-5298
email: ad@LBA.de
B/E AEROSPACE FISCHER 07.11.2016
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Sitze und Liegen
Inhaber der Musterzulassung: B/E AEROSPACE FISCHER GmbH
Hersteller: B/E Aerospace Fischer GmbH (vormals Fischer + Entwicklungen GmbH & Co.
KG)
Muster: Attendant Seat NG
Pilot Seat 120/335
Baureihen: B/E Aerospace Fischer "Attendant Seat NG" Flugbegleitersitze der Part-
Nummer (P/N) 1021-A-B-10221-0WX01 und "Pilot Seat 120/335" Pilotensitze
der Part-Nummer (P/N) 9911-0-0-X05X11101L2, 9911-0-0-X05X11101R2,
9911-0-0-X05X111L1R2 und 9911-0-0-X05X111R1L2.
Werknummern: Gemäß der Seriennummern im Appendix I der EASA AD 2016-0210.
Die betroffenen Sitze sind in Leonardo (vormals Finmeccanica,
AgustaWestland, Agusta) A109, AW109SP und AW169 Hubschraubern
installiert, aber nicht auf diese beschränkt.
Gerätenummer: EASA.21O.10042168 REV. A und LBA.O.30.131/114NTSO
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA AD 2016-0210 vom 24.10.2016
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 2016-287 geführt.
Betrifft:
(ATA 25) Equipment / Furnishings - Seat Energy Absorber Assembly - Replacement
Anmerkungen:
Gemäß M.A.303 und M.A.301 5.i) des Anhang I der Verordnung (EU) Nr. 1321/2014 (Teil-M) dürfen Luftfahr-
zeuge nach dem in der Lufttüchtigkeitsanweisung angegebenen Termin nur in Betrieb genommen werden,
wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind.
Die Europäische Agentur für Flugsicherheit (EASA) hat die oben referenzierte Lufttüchtigkeitsanweisung
EASA AD 2016-0210 vom 24.10.2016 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
gültige 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-2016-287 Seite 1 von 1 494/2016
EASA AD No.: 2016-0210
Airworthiness Directive
AD No.: 2016-0210
Issued: 24 October 2016
Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation
(EC) 216/2008 on behalf of the European Union, its Member States and 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 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 (EC) 216/2008, Article 14(4) exemption].
Design Approval Holder’s Name: Type/Model designation(s):
B/E AEROSPACE FISCHER GmbH Attendant Seats NG and
Pilot Seats 120/335
Effective Date: 07 November 2016
ETSO Approval(s): EASA.21O.10042168 REV. A and LBA.O.30.131/114NTSO
Foreign AD: Not applicable
Supersedure: None
ATA 25 – Equipment / Furnishings – Seat Energy Absorber Assembly – Replacement
Manufacturer(s):
B/E Aerospace Fischer GmbH, formerly Fischer + Entwicklungen GmbH & Co. KG
Applicability:
Attendant Seats NG and Pilot Seats 120/335, all Part Numbers (P/N) and serial numbers (s/n) listed
in Appendix I of this AD.
These seats are known to be installed on, but not limited to, Leonardo (formerly Finmeccanica,
AgustaWestland, Agusta) A109, AW109SP and AW169 helicopters.
Reason:
It was discovered that rivets with insufficient strength were used during the manufacturing of
energy absorber (EA) assemblies, installed on certain seats. As a consequence, these EA assemblies
may not be fully functional during an emergency landing.
This condition, if not detected and corrected, could lead to injury of the seat occupant.
To address this unsafe condition, B/E Aerospace Fischer issued Service Bulletin (SB) SB 9911-001 to
provide replacement instructions.
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EASA AD No.: 2016-0210
For the reason described above, this AD requires replacement of the EA assemblies on the affected
seats.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
(1) Within 45 days after the effective date of this AD, replace the EA assemblies on each affected
seat with serviceable assemblies in accordance with the instructions of B/E Aerospace Fischer
SB 9911-001.
(2) From the effective date of this AD, installation of an affected seat on an aircraft is allowed,
provided that, prior to installation, it is determined that the EA assemblies have been replaced
in accordance with the instructions of B/E Aerospace Fischer SB 9911-001.
Ref. Publications:
B/E Aerospace Fischer SB 9911-001 original issue, dated 14 July 2016.
The use of later approved revisions of this 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 07 October 2016 as PAD 16-143 for consultation until 21 October 2016.
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. For any question concerning the technical content of the requirements in this AD, please
contact: B/E Aerospace Fischer GmbH, Müller-Armack-Str. 4, D-84034 Landshut, Germany
Fax: +49 (0)871 93248-22, E-Mail: spares@fischer-seats.de.
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EASA AD No.: 2016-0210
Appendix I - List of Affected Seats
Seat Type Seat P/N s/n EA-Assembly P/N
Attendant Seat NG 1021-A-B-10221-0WX01 0232 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0237 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0252 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0253 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0254 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0255 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0263 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0284 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0285 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0286 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0287 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0288 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0290 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0291 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0307 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0308 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0309 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0310 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0311 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0312 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0313 1021-220
Attendant Seat NG 1021-A-B-10221-0WX01 0314 1021-220
Pilot Seat 120/335 9911-0-0-X05X11101L2 1524 9911-220
Pilot Seat 120/335 9911-0-0-X05X11101L2 1525 9911-220
Pilot Seat 120/335 9911-0-0-X05X11101L2 1531 9911-220
Pilot Seat 120/335 9911-0-0-X05X11101L2 1534 9911-220
Pilot Seat 120/335 9911-0-0-X05X11101R2 1529 9911-220
Pilot Seat 120/335 9911-0-0-X05X11101R2 1530 9911-220
Pilot Seat 120/335 9911-0-0-X05X111L1R2 1542 9911-220
Pilot Seat 120/335 9911-0-0-X05X111L1R2 1543 9911-220
Pilot Seat 120/335 9911-0-0-X05X111R1L2 1541 9911-220
TE.CAP.00110-005 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 3 of 3
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An agency of the European Union
Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2016-288 38144 Braunschweig
EASA AD 2016-0219 vom 03.11.2016 Fax: +49-531-2355-5298
email: ad@LBA.de
AIRBUS 07.11.2016
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: AIRBUS
Hersteller: Airbus (vormals Airbus Industrie)
Muster: A340
Baureihen: A340-541, A340-542 und A340-642
Werknummern: Alle
Gerätenummer: 2850, EASA.A.015
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA AD 2016-0219 vom 03.11.2016
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 2016-288 geführt.
Betrifft:
(ATA 32) Landing Gear - Nose Landing Gear Hydraulic Control Unit - Replacement
Anmerkungen:
Gemäß M.A.303 und M.A.301 5.i) des Anhang I der Verordnung (EU) Nr. 1321/2014 (Teil-M) dürfen Luftfahr-
zeuge nach dem in der Lufttüchtigkeitsanweisung angegebenen Termin nur in Betrieb genommen werden,
wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind.
Die Europäische Agentur für Flugsicherheit (EASA) hat die oben referenzierte Lufttüchtigkeitsanweisung
EASA AD 2016-0219 vom 03.11.2016 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
gültige 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-2016-288 Seite 1 von 1 503/2016
EASA AD No.: 2016-0219
Airworthiness Directive
AD No.: 2016-0219
Issued: 03 November 2016
Note: This Airworthiness Directive (AD) is issued by EASA, acting in accordance with Regulation
(EC) 216/2008 on behalf of the European Union, its Member States and 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 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 (EC) 216/2008, Article 14(4) exemption].
Design Approval Holder’s Name: Type/Model designation(s):
AIRBUS A340 aeroplanes
Effective Date: 17 November 2016
TCDS Numbers: EASA.A.015
Foreign AD: Not applicable
Supersedure: None
ATA 32 – Landing Gear – Nose Landing Gear Hydraulic Control Unit – Replacement
Manufacturer(s):
Airbus (formerly Airbus Industrie)
Applicability:
Airbus A340-541, A340-542 and A340-642 aeroplanes, all manufacturer serial numbers.
Reason:
An aeroplane experienced a sudden veering during the take-off run, at a speed of 47 kts. Analysis of
the Flight Data Recorder showed a “Braking and Steering Control Unit Channel 1 Fault”, followed by
a loss of the nose wheel steering. Investigation results showed that a brief “hydraulic lock” occurred
in the Hydraulic Control Unit (HCU), causing a slow return of the nose wheel to centre in castoring
mode.
This condition, if not corrected, could lead to the loss of the control of the aeroplane during
take-off, possibly resulting in damage to the aeroplane and injury to the occupants.
To initially address this potential unsafe condition, for A330 and A340-200/-300 aeroplanes, Airbus
developed a modification of the HCU by adding a check valve between the selector valve and the
servo valve. Airbus published Service Bulletin (SB) A330-32-3156 and SB A340-32-4194 for
accomplishment of this modification in-service. Consequently, DGAC France issued AD F-2005-016
(EASA approval 2005-499) to require this modification.
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EASA AD No.: 2016-0219
Since that AD was issued, it was determined that A340-500/-600 aeroplanes are also affected by
this unsafe condition, and Airbus published SB A340-32-5117 to provide modification instructions.
For the reasons described above, this AD requires modification of the affected aeroplanes by
installing a modified HCU. This AD also prohibits reinstallation of pre-mod HCU, and allows
installation of a later approved HCU standard.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
Part Replacement:
(1) Within 48 months after the effective date of this AD, modify the aeroplane by replacing the
affected HCU P/N D24067000-3 with an improved HCU P/N D24067000-6, in accordance with
the instructions of Airbus SB A340-32-5117.
Part Installation:
(2) Do not install on any aeroplane an HCU P/N D24067000-3, as required by paragraph (2.1) or
(2.2) of this AD, as applicable.
(2.1) For an aeroplane equipped with an HCU P/N D24067000-3: After modification of that
aeroplane as required by paragraph (1) of this AD.
(2.2) For an aeroplane not equipped with an HCU P/N D24067000-3: From the effective date of
this AD.
(3) Installation on an aeroplane of an HCU standard, approved after the effective date of this AD, is
equal to compliance with the requirements of paragraph (1) of this AD for that aeroplane,
provided the conditions as specified in paragraphs (3.1) and (3.2) are met.
(3.1) The HCU standard must be approved by EASA, or approved under Airbus Design
Organisation Approval (DOA); and
(3.2) The installation must be accomplished in accordance with aeroplane modification
instructions approved by EASA, or approved under DOA.
Ref. Publications:
Airbus SB A340-32-5117 original issue dated 31 August 2016.
The use of later approved revisions of this 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 12 September 2016 as PAD 16-132 for consultation until 10 October
2016. The Comment Response Document can be found at http://ad.easa.europa.eu.
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EASA AD No.: 2016-0219
3. Enquiries regarding this AD should be referred to the EASA Safety Information Section,
Certification Directorate. E-mail: ADs@easa.europa.eu.
4. 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.00110-005 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 3 of 3
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Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2016-289 38144 Braunschweig
EASA AD 2016-0207 vom 19.10.2016 Fax: +49-531-2355-5298
email: ad@LBA.de
AIRBUS 07.11.2016
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: AIRBUS
Hersteller: Airbus (vormals Airbus Industrie)
Muster: A330
Baureihen: A330-201, A330-202, A330-203, A330-223, A330-243, A330-223F, 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 2016-0207 vom 19.10.2016
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 2016-289 geführt.
Betrifft:
(ATA 53) Fuselage - Structural Parts / Joints - Modification / Reinforcement
Anmerkungen:
Gemäß M.A.303 und M.A.301 5.i) des Anhang I der Verordnung (EU) Nr. 1321/2014 (Teil-M) dürfen Luftfahr-
zeuge nach dem in der Lufttüchtigkeitsanweisung angegebenen Termin nur in Betrieb genommen werden,
wenn die angeordneten Maßnahmen ordnungsgemäß durchgeführt worden sind.
Die Europäische Agentur für Flugsicherheit (EASA) hat die oben referenzierte Lufttüchtigkeitsanweisung
EASA AD 2016-0207 vom 19.10.2016 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
gültige 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-2016-289 Seite 1 von 1 482/2016
