Nachrichten für Luftfahrer 2015 Teil 2 (weicht ggf. von Druckversion ab)
Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2015-022R1 38144 Braunschweig
EASA AD 2015-0119 vom 24.06.2015 Fax: +49-531-2355-5298
email: ad@LBA.de
AIRBUS 02.07.2015
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: AIRBUS
Hersteller: Airbus, Airbus Industrie
Muster: A330, A340
Baureihen: A330-201, A330-202, A330-203, A330-223, A3330-223F, A330-243,
A330-243F, A330-301, A330-302, A330-303, A330-321, A330-322, A330-323,
A330-341, A330-342, A330-343,
A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, A340-541,
A340-542, A340-642 und A340-643
Werknummern: Alle.
Ausgenommen sind A340-200/300 und A340-500/600 Flugzeuge, bei denen ein
"Gaseous System" für alle Sauerstoffbehälter installiert ist.
Gerätenummer: 2849, 2850, EASA.A.004, EASA.A.015
Revisionsstand:
Diese LTA ersetzt D-2015-022 vom 23.01.2015
Airworthiness Directive der ausländischen Behörde:
EASA AD 2015-0119 vom 24.06.2015
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 2015-022R1 ge-
führt.
Betrifft:
(ATA 35) Oxygen - Chemical Oxygen Generators - Replacement
Anmerkungen:
Gemäß M.A.303 und M.A.301 5.i) des Anhang I der Verordnung (EU) Nr. 1321/2014 (Teil-M) dürfen
Luftfahrzeuge 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 Lufttüchtigkeitsan-
weisung EASA AD 2015-0119 vom 24.06.2015 herausgegeben oder per Entscheidung Nr. 02/2003
übernommen.
Gemäß § 14 Abs. 2 der Betriebsordnung für Luftfahrtgerät (LuftBO) sind diese Lufttüchtigkeitsan-
weisungen 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 Verwaltungsverfahren zu Grunde. Rechtsmittel sind damit ausgeschlossen.
D-2015-022R1 Seite 1 von 1 271/2015
EASA AD No.: 2015-0119
EASA AIRWORTHINESS DIRECTIVE
AD No.: 2015-0119
Date: 24 June 2015
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.
This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with 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 [EU
1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemption].
Design Approval Holder’s Name: Type/Model designation(s):
AIRBUS A330 and A340 aeroplanes
TCDS Numbers: EASA.A.004 and EASA.A.015
Foreign AD: Not applicable
Supersedure: This AD supersedes EASA AD 2014-0277 dated 19 December 2014.
ATA 35 Oxygen – Chemical Oxygen Generators – Replacement
Manufacturer(s): Airbus (formerly Airbus Industrie)
Applicability: Airbus A330-201, A330-202, A330-203, A330-223, A3330-223F, 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), and
Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313,
A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN, except
those that have a gaseous system installed for all oxygen containers.
Reason: Reports have been received indicating premature ageing of certain chemical
oxygen generators, Part Number (P/N) 117042-XX (XX representing any
numerical value), manufactured by B/E Aerospace. Some operators reported
that when they tried to activate generators, some older units failed to activate.
Given the number of failed units reported, all generators manufactured in 1999,
2000 and 2001 were considered unreliable.
This condition, if not corrected, could lead to failure of the generator to activate
and consequently not deliver oxygen during an emergency, possibly resulting in
injury to aeroplane occupants.
To address this potential unsafe condition, Airbus issued Alert Operators
Transmission (AOT) A35L007-14, making reference to B/E Aerospace Service
Information Letter (SIL) D1019-01 (currently at Revision 1) and B/E Aerospace
Service Bulletin (SB) 117042-35-001. Consequently, EASA issued AD
2014-0277 to require identification and replacement of the affected oxygen
generators.
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EASA AD No.: 2015-0119
Since EASA AD 2014-0277 was issued, and following new investigation results,
EASA have decided to introduce a life limitation concerning all P/N 117042-XX
chemical oxygen generators, manufactured by B/E Aerospace.
For the reason described above, this AD retains the requirements of EASA AD
2014-0277, which is superseded, expands the scope of the AD to include
chemical oxygen generators manufactured after 2001, and requires their
removal from service before exceeding 10 years since date of manufacture.
Effective Date: 08 July 2015
Required Action(s) Required as indicated, unless accomplished previously:
and Compliance
Time(s): Partial restatement of the requirements of EASA AD 2014-0277:
(1) Within 30 days after 24 December 2014 [the effective date of EASA AD
2014-0277], identify the date of manufacture (see Appendix 1 of this AD
where this is located) of each oxygen generator, having a P/N as listed in
Table 1 of this AD, in accordance with the instructions of Airbus AOT
A35L007-14.
A review of aeroplane maintenance records is acceptable to make this
identification, provided those records can be relied upon for the purpose of
this requirement.
(2) Within the compliance time specified in Table 1 of this AD, as applicable,
remove and replace each affected oxygen generator from service in
accordance with the instructions of Airbus AOT A35L007-14 (for 15 and 22
min generators), or, in accordance with the instructions of B/E Aerospace
SB 117042-35-001 (for 15 min generators).
B/E Aerospace SIL D1019-01 Revision 1 provides instructions for the
activation and the disposal of a removed oxygen generator. Airbus AOT
A35L007-14 (Appendix 1) includes instructions for reporting the results of
the activation (including no findings) of removed units.
Table 1 – Replacement of pre-2002 Passenger Oxygen Generators
P/N (type) Compliance Time
For units manufactured in 1999,
before exceeding 180 months since
date of manufacture, or within 30 days
after 24 December 2014 [the effective
date of EASA AD 2014-0277],
whichever occurs later
117042-02 (15 min - 2 masks) For units manufactured in 2000,
117042-03 (15 min - 3 masks) before exceeding 174 months since
117042-04 (15 min - 4 masks) date of manufacture, or within 6
117042-22 (22 min - 2 masks) months after 24 December 2014 [the
117042-23 (22 min - 3 masks) effective date of EASA AD 2014-
117042-24 (22 min - 4 masks) 0277], whichever occurs later
For units manufactured in 2001,
before exceeding 168 months since
date of manufacture, or within 12
months after 24 December 2014 [the
effective date of EASA AD 2014-
0277], whichever occurs later
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EASA AD No.: 2015-0119
New requirements of this AD:
(3) Within the compliance time as specified in Table 2 of this AD, as
applicable, and, for generators with a manufacturing date 2009 or later,
before exceeding 10 years since date of manufacture of the oxygen
generator, whichever occurs later, as applicable, remove from service each
oxygen generator manufactured by B/E Aerospace and having a P/N
117042-XX, and replace it with a serviceable unit (see Note) in accordance
with the instructions of Airbus AOT A35L007-14 (for 15 and 22 min
generators), or the instructions of B/E Aerospace SB 117042-35-001 (for
15 min generators).
Note: For the purpose of this AD, a serviceable unit is an oxygen generator
having P/N 117042-XX with a manufacturing date not older than 10 years, or
any other approved P/N, provided that the generator has not exceeded the limit
established for that generator by the manufacturer.
Table 2 - Replacement of 2002-2008 Oxygen Generators
Compliance Time
Year of manufacture
(after the effective date of this AD)
2002 Within 12 months
2003 Within 16 months
2004 Within 20 months
2005 Within 24 months
2006 Within 28 months
2007 Within 32 months
2008 Within 36 months
(4) From the effective date of this AD, it is allowed to install on any aeroplane
an oxygen generator, provided it is determined, prior to installation, that the
oxygen generator is a serviceable unit (see Note).
Ref. Publications: Airbus AOT A35L007-14 original issue dated 18 December 2014, or Revision
01 dated 17 June 2015.
B/E Aerospace SB 117042-35-001 original issue dated 10 December 2014.
The use of later approved revisions of these documents is acceptable for
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.
Remarks: 1. If requested and appropriately substantiated, EASA can approve
Alternative Methods of Compliance for this AD.
2. This AD was posted on 22 May 2015 as PAD 15-065 for consultation until
19 June 2015. The Comment Response Document can be found at
http://ad.easa.europa.eu/.
3. Enquiries regarding this AD should be referred to the Safety Information
Section, Certification Directorate, EASA. E-mail: ADs@easa.europa.eu.
4. For any question concerning the technical content of the requirements in
this AD, please contact: AIRBUS – Airworthiness Office – EIAL;
E-mail: account.airworth-eas@airbus.com.
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EASA AD No.: 2015-0119
Appendix 1 – Passenger Oxygen Generator Date of Manufacture
Figure 1 – Location of date (MM-YY)
Figure 2 – MFG.DATE (05-02 = May 2002) example
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Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2015-139 38144 Braunschweig
EASA AD 2015-0110 vom 16.06.2015 Fax: +49-531-2355-5298
email: ad@LBA.de
BAE SYSTEMS 22.06.2015
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: BAE Systems (Operations) Ltd.
Hersteller: British Aerospace plc, Hawker Siddeley Aviation Ltd, A.V. Roe and Company
Muster: HS 748
Baureihen: Alle HS 748 Baureihen
Werknummern: Alle
Gerätenummer: 2833, EASA.A.397
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA AD 2015-0110 vom 16.06.2015
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 2015-139 geführt.
Betrifft:
(ATA 57) Wings - Lower Wing Skin - Inspection / Repair
Anmerkungen:
Gemäß M.A.303 und M.A.301 5.i) des Anhang I der Verordnung (EU) Nr. 1321/2014 (Teil-M) dürfen
Luftfahrzeuge 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 Lufttüchtigkeitsan-
weisung EASA AD 2015-0110 vom 16.06.2015 herausgegeben oder per Entscheidung Nr. 02/2003
übernommen.
Gemäß § 14 Abs. 2 der Betriebsordnung für Luftfahrtgerät (LuftBO) sind diese Lufttüchtigkeitsan-
weisungen 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 Verwaltungsverfahren zu Grunde. Rechtsmittel sind damit ausgeschlossen.
D-2015-139 Seite 1 von 1 252/2015
EASA AD No.: 2015-0110
EASA AIRWORTHINESS DIRECTIVE
AD No.: 2015-0110
Date: 16 June 2015
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.
This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with 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 [EU
1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemption].
Design Approval Holder’s Name: Type/Model designation(s):
BAE SYSTEMS (OPERATIONS) Ltd HS 748 aeroplanes
TCDS Number: EASA.A.397
Foreign AD: Not applicable
Supersedure: None
ATA 57 Wings – Lower Wing Skin – Inspection / Repair
Manufacturer(s): A.V. Roe and Company, Hawker Siddeley Aviation Ltd, British Aerospace plc
Applicability: HS 748 aeroplanes, all models, all serial numbers.
Reason: During an unscheduled removal of the right-hand (RH) main landing gear
(MLG) pivot bracket, significant corrosion was found on the wing lower skin in
the area behind the MLG inboard pivot bracket. Corrosion was also reportedly
found on the left-hand (LH) wing lower skin, albeit to a lesser extent. The
reported corrosion on the RH wing lower skin was determined to have been
caused by ingress of moisture between the ends of the inboard pivot bracket
and the MLG retraction jack bracket. Currently there is no scheduled inspection
of the wing lower skin in the area behind the MLG inboard pivot bracket.
This condition, if not detected and corrected, could lead to a high level of
corrosion that would compromise the structural integrity of the wing.
To address this unsafe condition, BAE Systems (Operations) Ltd issued
Inspection Service Bulletin (ISB) HS748-57-88 to provide instructions for close
visual inspections.
For the reason described above, this AD requires repetitive close visual
inspections of the wing lower skin under the MLG inboard pivot bracket, both
RH and LH sides, and, depending on findings, the accomplishment of
applicable corrective action(s).
Effective Date: 30 June 2015
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EASA AD No.: 2015-0110
Required Action(s) Required as indicated, unless accomplished previously.
and Compliance
(1) Within the compliance time as specified in Table 1 of this AD, as
Time(s):
applicable, and, thereafter, at intervals not to exceed 8 years, accomplish a
close visual inspection of the wing lower skin under the MLG inboard pivot
bracket, both RH and LH sides, in accordance with the instructions of BAE
Systems (Operations) Ltd ISB HS748-57-88.
Table 1 – Inspection Threshold
Condition Compliance Time
MLG inboard pivot bracket never
Within 6 months after the effective
removed in-service, or no records
date of this AD
available
Before exceeding 8 years since
MLG inboard pivot bracket (re)installation of the pivot bracket,
previously removed and or within 12 months after the
re-installed or replaced in-service effective date of this AD, whichever
occurs later
(2) If, during any inspection as required by paragraph (1) of this AD, any
corrosion is found, before next flight, contact BAE Systems (Operations)
Ltd for approved repair instructions and accomplish those instructions
accordingly.
(3) Repair of an aeroplane as required by paragraph (2) of this AD does not
constitute terminating action for the repetitive inspections as required by
paragraph (1) of this AD for that aeroplane, unless the approved repair
instructions state otherwise.
Ref. Publications: BAE Systems (Operations) Ltd ISB HS748-57-88, original issue, dated 27 June
2014.
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 08 May 2015 as PAD 15-059 for consultation until
05 June 2015. 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. For any question concerning the technical content of the requirements in
this AD, please contact:
BAE Systems (Operations) Ltd, Customer Information Department,
Prestwick International Airport, Ayrshire, KA9 2RW, Scotland, United
Kingdom; Telephone +44 1292 675207, Facsimile +44 1292 675704;
E-mail: RApublications@baesystems.com.
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Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2015-140 38144 Braunschweig
EASA AD 2015-0111 vom 16.06.2015 Fax: +49-531-2355-5298
email: ad@LBA.de
PILATUS 22.06.2015
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: Pilatus Aircraft Ltd.
Hersteller: Pilatus Aircraft Ltd.
Muster: PC-12
Baureihen: PC-12, PC-12/45 und PC-12/47E
Werknummern: Seriennummern 244, 307, 409, 646, 1447 bis 1450, 1461, 1462, 1466 bis 1514,
1516 bis 1520 und 1523.
Gerätenummer: 2077, EASA.A.089
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA AD 2015-0111 vom 16.06.2015
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 2015-140 geführt.
Betrifft:
(ATA 27) Flight Controls - Aileron Control System / Universal Joints - Replacement
Anmerkungen:
Gemäß M.A.303 und M.A.301 5.i) des Anhang I der Verordnung (EU) Nr. 1321/2014 (Teil-M) dürfen
Luftfahrzeuge 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 Lufttüchtigkeitsan-
weisung EASA AD 2015-0111 vom 16.06.2015 herausgegeben oder per Entscheidung Nr. 02/2003
übernommen.
Gemäß § 14 Abs. 2 der Betriebsordnung für Luftfahrtgerät (LuftBO) sind diese Lufttüchtigkeitsan-
weisungen 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 Verwaltungsverfahren zu Grunde. Rechtsmittel sind damit ausgeschlossen.
D-2015-140 Seite 1 von 1 253/2015
EASA AD No.: 2015-0111
EASA AIRWORTHINESS DIRECTIVE
AD No.: 2015-0111
Date: 16 June 2015
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.
This AD is issued in accordance with EU 748/2012, Part 21.A.3B. In accordance with 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 [EU
1321/2014 Annex I, Part M.A.303] or agreed with the Authority of the State of Registry [EC 216/2008, Article 14(4) exemption].
Design Approval Holder’s Name: Type/Model designation(s):
PILATUS AIRCRAFT Ltd. PC-12 aeroplanes
TCDS Number: EASA.A.089
Foreign AD: Not applicable
Supersedure: None
Flight Controls – Aileron Control System / Universal Joints –
ATA 27
Replacement
Manufacturer(s): Pilatus Aircraft Ltd.
Applicability: PC-12, PC-12/45 and PC-12/47E aeroplanes, manufacturer serial numbers
(MSN) 244, MSN 307, MSN 409, MSN 646, MSN 1447 through MSN 1450,
MSN 1461, MSN 1462, MSN 1466 through MSN 1514, MSN 1516 through
MSN 1520 and MSN 1523.
Reason: A case of malfunctioning was reported of a universal joint installed between
the control tube assembly and the control column on a PC-12/47E aeroplane.
Investigation determined that the malfunction was caused by an incorrectly
manufactured universal joint. Universal joints from the same manufacturing
batch were provided to operators between 01 March 2014 and 28 February
2015, and are thus potentially affected.
This condition, if not corrected, could lead to other cases of malfunctioning of
a universal joint, possibly resulting in reduced control of the aeroplane.
To address this potential unsafe condition, Pilatus Aircraft Ltd. issued Service
Bulletin (SB) No. 27-022 to provide instructions for replacement of the universal
joints in the flight controls.
For the reason described above, this AD requires removal from service of the
potentially incorrectly manufactured universal joints.
Effective Date: 30 June 2015
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