Nachrichten für Luftfahrer 2015 Teil 2 (weicht ggf. von Druckversion ab)
EASA AD No.: 2015-0235
Component Part Number Old Part F-28C/F-28C-2/280C
Name (P/N) Number
MTOW = MTOW = MTOW =
2200 lbs 2350 lbs 2600 lbs
Coupling, Tail Rotor 28-13609-1 1 200 FH 1 200 FH 1 200 FH
Driveshaft
Coupling, Flex Pack 28-01041-3 A005-1992 1 200 FH 1 200 FH 1 200 FH
Assembly (Dana)
Tail Rotor Gear set ECD074-1, XR-137-2YL, 1 200 FH 1 200 FH 1 200 FH
ECD074-2 XR-137-2R
Tail Rotor Gear set ECD100-1, 1 200 FH 1 200 FH 1 200 FH
ECD100-2,
ECD100-1A,
ECD100-2A,
ECD100-1B,
ECD100-2B
Tail Rotor Gear set ECD101-1, 1 200 FH 1 200 FH 1 200 FH
ECD101-2
Drag Link 28-14283-1 + + 13 750 FH
Main Rotor Spindle 28-14282-11 19 000 FH 19 000 FH 19 000 FH
Thrust Bearing 28-14320-12, ΔΔ ΔΔ ΔΔ
(Lamiflex) 28-14320-15
Tachometer Drive NAS1611-333 Δ Δ Δ
Belt (O-Ring)
** On Condition when used with grease fitting
+ No Time limit. Remove Component on condition per Maintenance
Manual inspection criteria.
++ Right hand installations only (28-16300); left hand installations are on
condition.
ΔΔ Retire from service 5 calendar years from date of manufacture all Lamiflex
bearings serial number 5997 and prior.
Retire from service 5 calendar years from date of installation* or 8
calendar years from date of manufacture, whichever occurs first, all
Lamiflex bearings serial numbers 5998 and subsequent.
*Note: Date of installation is defined as the date the Lamiflex bearing
packaging is opened.
Δ Retire from service 5 calendar years from date of installation or package
opening, or 8 years from date of manufacture, whichever occurs first.
N/A Not approved for installation.
TE.CAP.00110-005 © European Aviation Safety Agency. All rights reserved. ISO9001 Certified. Page 6 of 6
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-2015-296 38144 Braunschweig
EASA AD 2015-0236 vom 16.12.2015 Fax: +49-531-2355-5298
email: ad@LBA.de
AIRBUS 21.12.2015
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: AIRBUS
Hersteller: Airbus
Muster: A380
Baureihen: A380-841, A380-842 und A380-861
Werknummern: Seriennummern (S/N) 0030, 0035, 0036, 0039, 0042, 0044, 0046, 0048, 0049,
0052, 0054 bis 0059, 0061 bis 0090, 0092 bis 0096, 0098 bis 0101, 0103, 0105
bis 0117, 0119 bis 0128, 0130 bis 0159, 0161 bis 0164 und 0166.
Gerätenummer: EASA.A.110
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
EASA AD 2015-0236 vom 16.12.2015
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 2015-296 geführt.
Betrifft:
(ATA 53) Fuselage - Cabin / Cargo Compartment Parts - Inspection / Replacement [Wrong Material]
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 2015-0236 vom 16.12.2015 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-2015-296 Seite 1 von 1 512/2015
EASA AD No.: 2015-0236
Airworthiness Directive
AD No.: 2015-0236
Issued: 16 December 2015
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 A380 aeroplanes
Effective Date: 30 December 2015
TCDS Number(s): EASA.A.110
Foreign AD: Not applicable
Supersedure: None
ATA 53 – Fuselage – Cabin / Cargo Compartment Parts – Inspection / Replacement
[Wrong Material]
Manufacturer(s):
Airbus
Applicability:
Airbus A380-841, A380-842 and A380-861 aeroplanes, manufacturer serial numbers (MSN) 0030,
0035, 0036, 0039, 0042, 0044, 0046, 0048 to 0049 inclusive, 0052, 0054 to 0059 inclusive, 0061 to
0090 inclusive, 0092 to 0096 inclusive, 0098 to 0101 inclusive, 0103, 0105 to 0117 inclusive, 0119 to
0128 inclusive, 0130 to 0159 inclusive, 0161 to 0164 inclusive, and MSN 0166.
Reason:
Quality control involving final assembly line review identified that improper aluminium alloy was
used to manufacture several structural parts installed in cabin and cargo compartments.
This condition, if not detected and corrected, could reduce the structural integrity of the aeroplane.
To address this potential unsafe condition, Airbus issued Service Bulletin (SB) A380-53-8099 and SB
A380-53-8100 to provide instructions to identify the affected parts.
TE.CAP.00110-005 © European 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.: 2015-0236
For the reasons described above, this AD requires a one-time special detailed inspection (SDI) of
certain cabin and cargo compartment parts to identify the material they are made of and,
depending on findings, replacement with serviceable parts.
Required Action(s) and Compliance Time(s):
Required as indicated, unless accomplished previously:
(1) Before exceeding 6 years since the aeroplane date of manufacture, accomplish an SDI of the
cabin and cargo compartment parts identified as “Affected part numbers (P/N)” and listed in
Appendix 1 of this AD in accordance with the instructions of Airbus SB A380-53-8099 and/or SB
A380-53-8100, as applicable to aeroplane MSN defined in Appendix 2 of Airbus SB
A380-53-8099 and SB A380-53-8100.
Note: For the purpose of this AD, the date of manufacture is the date of transfer of title, which is
referenced in Airbus documentation at the time of first delivery to an operator.
(2) If, during the SDI, as required by paragraph (1) of this AD, a part manufactured from improper
material is detected, before exceeding 6 years since the aeroplane date of manufacture,
replace each affected part with a serviceable part identified as an “Acceptable Replacement
P/N” and listed in Appendix 1 of this AD, in accordance with the instructions of Airbus SB
A380-53-8099 and/or SB A380-53-8100, as applicable.
Ref. Publications:
Airbus SB A380-53-8099 original issue, dated 05 August 2015.
Airbus SB A380-53-8100 original issue, dated 25 September 2015.
The use of later approved revisions of these documents 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 09 November 2015 as PAD 15-139 for consultation until 07 December
2015. The Comment Response Document can be found at http://ad.easa.europa.eu.
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 SAS - EIANA (Airworthiness Office), Telephone : +33 562 110 253;
Fax: +33 562 110 307, E-mail: account.airworth-A380@airbus.com.
TE.CAP.00110-005 © European 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.: 2015-0236
Appendix 1 – Affected Cabin and Cargo Compartment Parts and Acceptable Replacement Parts
Affected P/N Acceptable Replacement P/N Affected Area
L5347059120200 L5347059120200
L5347059120300 L5347059120300
L5347074722400 L5347074722451
L5347074722500 L5347074722551
L5347074722600 L5347074722651 Cargo
L5347074722700 L5347074722751
L5347074722800 L5347074722851
L5347074722900 L5347074722951
L5347074723000 L5347074723051
L5327029020000 L5327029020000
L5327051020000 L5327051020051
L5327051020100 L5327051020151
L5327057420000 L5327057420000
L5327057420100 L5327057420100
L5327057520000 L5327057520000
L5327057520100 L5327057520100
L5327338320300 L5327338320351
L5327349620500 L5327349620500
L5347038720800 L5347038720851
L5347038720900 L5347038720951 Cabin
L5347058020000 L5347058020051
L5347058020100 L5347058020151
L5347059125400 L5347059125451
L5347059125500 L5347059125551
L5347518320200 L5347518320200
L5347518320300 L5347518320300
L5347531020200 L5347531020200
L5347531020300 L5347531020300
L5347532220000 L5347532220051
L5347532220100 L5347532220151
TE.CAP.00110-005 © European 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
DFS GmbH | BueroNfL3 2:PN | 22.12.2015 | 10:40:32 GMT | redaktion.nfl@dfs.de
