Nachrichten für Luftfahrer 2016 Teil 2 (weicht ggf. von Druckversion ab)
EASA AD No.: 2016-0095
2. This AD was posted on 19 April 2016 as PAD 16-059 for consultation until 17 May 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: AIRBUS - EIANA (Airworthiness Office), Telephone : +33 562 110 253;
Fax: +33 562 110 307, E-mail: account.airworth-A380@airbus.com.
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EASA AD No.: 2016-0095
Appendix 1 – Middle and Outboard Flaps to be inspected
For the purpose of these Tables:
N/A - not applicable;
The starting date for the service life calculation is shown as day/month/year (dd/mm/yyyy).
Note 4: The starting date for service life calculation corresponds to the transfer of title of
aeroplane where the s/n of the flap has been recorded and referenced in Airbus
documentation at the time of aeroplane first delivery to an operator.
Table 1 – Middle Flaps
s/n Starting date s/n Starting date
for service life for service life
LH RH LH RH
calculation calculation
TB1021 TB1021 04/06/2010 TB2016 TB2016 25/11/2011
TB1015 TB1015 22/08/2009 TB2001 TB2001 17/06/2011
TB1050 TB1050 28/05/2010 TB2004 TB2004 29/09/2011
TB1051 TB1051 02/07/2010 TB2007 TB2007 31/03/2011
TB2011 TB2011 12/10/2011 TB2033 TB2017 05/06/2012
TB2006 TB2006 31/05/2011 TB2017 TB2018 07/09/2011
TB2021 TB2021 16/12/2011 TB2020 TB2008 04/05/2011
TB1047 TB1047 15/05/2010 TB2010 TB2010 05/07/2011
TB2009 TB2009 13/07/2011 TB2005 TB2005 14/09/2011
TB9004 TB9004 10/02/2010 TB2012 TB2012 14/05/2012
TB1031 TB1048 16/07/2010 TB2035 TB2034 13/06/2012
TB1042 TB1042 28/09/2010 TB2019 TB2019 15/12/2011
TBE1021 TBE1021 14/04/2010 TB2024 TB2024 28/11/2011
TB1044 TB1044 20/08/2010 TB2014 TB2020 12/01/2012
TBE1019 TBE1019 06/09/2009 TB2022 TB2014 14/10/2011
TB1046 TB1046 12/08/2010 TB2032 TB2032 29/05/2012
TB1043 TB1043 16/12/2010 TB2028 TB2029 02/04/2012
TB1048 TB1056 27/10/2010 TB2023 TB2023 28/10/2011
TB1049 TB1049 12/08/2010 TB2038 TB2037 27/07/2012
TB1028 TB1028 31/01/2011 TB2029 TB2028 08/02/2012
TB1030 TB1030 16/07/2010 TB2025 TB2025 25/11/2011
TB1052 TB1052 17/05/2011 TB2043 TB2043 26/10/2012
TB2018 TB2022 28/02/2012 TB2037 TB2036 31/07/2012
TB1057 TB1064 13/01/2011 TB2026 TB2026 16/12/2011
TB1055 TB1055 05/11/2010 TB2045 TB2045 26/09/2012
TB1062 TB1062 30/11/2010 TB2046 TB2046 13/09/2012
TB2000 TB2000 16/06/2011 TB2052 TB2051 31/10/2012
TB2013 TB2013 19/08/2011 TB2027 TB2027 02/12/2011
TB2003 TB2003 15/03/2011 TB2042 TB2042 06/09/2012
TB1061 TBE1041 08/04/2011 TB2054 TB2053 28/11/2012
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EASA AD No.: 2016-0095
Table 1 – Middle Flaps
s/n Starting date s/n Starting date
for service life for service life
LH RH LH RH
calculation calculation
TB2059 TB2058 07/02/2013 TB2076 TB2075 25/10/2013
TB2063 TB2062 03/07/2013 TB2094 TB2091 27/06/2014
TB2065 TB2054 10/12/2012 TB2081 TB2080 29/11/2013
TB2015 TB2015 24/02/2012 TB2075 TB2074 29/08/2013
TB2030 TB2030 02/05/2012 TB2079 TB2078 27/11/2013
TB2066 TB2056 20/12/2012 TB2086 TB2084 14/11/2013
TB2034 TB2033 30/07/2012 TB2088 TB2085 27/11/2013
TB2039 TB2038 29/08/2012 TB2072 TB2086 29/10/2013
TB2044 TB2044 01/10/2012 TB2055 TB2088 12/12/2013
TB2047 TB2047 01/10/2012 TB2092 TB2089 19/12/2013
TB2048 TB2048 12/10/2012 TB2093 TB2090 19/12/2013
TB2049 TB2059 19/12/2012 N/A TB2081 14/02/2014
TB2051 TB2050 09/11/2012 N/A TB2100 27/03/2014
TB2053 TB2052 30/11/2012 TB2089 TB2087 16/01/2014
TB2056 TB2055 28/12/2012 TB2090 TB2094 28/03/2014
TB2058 TB2057 27/12/2012 TB2097 TB2064 27/03/2014
TB2064 TB2066 03/05/2013 TB2095 TB2093 06/03/2014
TB2062 TB2061 13/03/2013 TB2100 TB2099 05/05/2014
TB2067 TB2065 12/09/2013 TB2084 TB2083 19/05/2014
TB2068 TB2067 08/05/2013 TB2078 TB2077 14/05/2014
N/A TB2082 20/06/2014 TB2057 TB2098 28/05/2014
TB2069 TB2068 04/06/2013 TB2103 TB2102 27/06/2014
TB2060 TB2060 28/02/2013 TB2107 TB2105 09/07/2014
TB2073 TB2072 19/09/2013 TB2104 TB2103 29/07/2014
TB2061 TB2063 21/03/2013 TB2087 TB2104 28/07/2014
TB2071 TB2070 17/06/2013 TB2108 TB2092 18/08/2014
TB2077 TB2076 17/10/2013 TB2105 N/A 25/08/2014
TB2080 TB2079 29/10/2013 N/A TB2101 22/12/2014
TB2070 TB2069 28/08/2013
TB2074 TB2073 19/09/2013
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EASA AD No.: 2016-0095
Table 2 – Outboard Flaps
s/n Starting date s/n Starting date
for service life for service life
LH RH LH RH
calculation calculation
TB2006 TB2016 16/12/2011 TB2043 TB2043 19/12/2012
TB1056 TB1056 17/05/2011 TB2046 TB2044 09/11/2012
TB2021 TB2021 28/02/2012 TB2048 TB2046 30/11/2012
TB2026 TB2027 05/06/2012 TB2051 TB2058 28/12/2012
TB2010 TB2010 14/05/2012 TB2053 TB2052 27/12/2012
TB2030 TB2032 13/06/2012 TB2059 TB2061 03/05/2013
TB2016 TB2023 28/11/2011 TB2057 TB2056 13/03/2013
TB2018 TB2018 14/10/2011 TB2063 TB2062 12/09/2013
TB2028 TB2030 29/05/2012 TB2055 TB2063 08/05/2013
TB2023 TB2024 02/04/2012 TB2089 TB2065 04/06/2013
TB2019 TB2019 28/10/2011 TB2061 TB2054 28/02/2013
TB2032 TB2034 27/07/2012 TB2066 TB2064 19/09/2013
TB2024 TB2025 08/02/2012 TB2056 TB2055 21/03/2013
TB2020 TB2020 25/11/2011 TB2067 TB2059 17/06/2013
TB2037 TB2037 26/10/2012 TB2070 TB2069 17/10/2013
TB2031 TB2033 31/07/2012 TB2078 TB2077 29/10/2013
TB2022 TB2022 16/12/2011 TB2060 TB2060 28/08/2013
TB2039 TB2039 26/09/2012 TB2065 TB2068 19/09/2013
TB2040 TB2040 13/09/2012 TB2068 TB2067 25/10/2013
TB2047 TB2045 31/10/2012 TB2079 TB2078 29/11/2013
TB2008 TB2008 02/12/2011 TB2062 TB2066 29/08/2013
TB2036 TB2036 06/09/2012 TB2077 TB2070 27/11/2013
TB2049 TB2047 28/11/2012 TB2080 TB2079 14/11/2013
TB2054 TB2053 07/02/2013 TB2072 TB2076 27/11/2013
TB2058 TB2057 03/07/2013 TB2081 TB2081 29/10/2013
TB2050 TB2048 10/12/2012 TB2082 TB2049 12/12/2013
TB2025 TB2026 24/02/2012 TB2090 TB2082 19/12/2013
TB2027 TB2029 02/05/2012 TB2071 TB2083 19/12/2013
TB2052 TB2050 20/12/2012 TB2083 TB2085 16/01/2014
TB2029 TB2031 30/07/2012 TB2088 TB2089 28/03/2014
TB2033 TB2035 29/08/2012 TB2064 TB2090 27/03/2014
TB2038 TB2038 01/10/2012 TB2087 TB2087 06/03/2014
TB2041 TB2041 01/10/2012 TB2093 TB2092 05/05/2014
TB2042 TB2042 12/10/2012
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Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2016-139 38144 Braunschweig
ANAC BAD 2016-05-01 - Amdt. 39-1399 vom Fax: +49-531-2355-5298
27.05.2016 email: ad@LBA.de
EMBRAER 27.05.2016
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugzeug
Inhaber der Musterzulassung: Embraer S.A.
Hersteller: Embraer S.A., EMBRAER - Empresa Brasileira de Aeronáutica S.A., Embraer
Executive Aircraft Inc.
Muster: EMB-500, EMB-505
Baureihen: EMB-500 und EMB-505
Werknummern: Gemäß Embrear S.A. Service Bulletin 500-25-0016 vom 08.12.2015 und
Embrear S.A. Service Bulletin 505-25-0020 vom 08.12.2015
Gerätenummer: EASA.IM.A.157, EASA.IM.A.158
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
ANAC BAD 2016-05-01 - Amdt. 39-1399 vom 27.05.2016
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 2016-139 geführt.
Betrifft:
(ATA 53) Fuselage - Passenger Seat Attachment Fittings - Inspection
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
ANAC BAD 2016-05-01 - Amdt. 39-1399 vom 27.05.2016 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-2016-139 Seite 1 von 1 235/2016
AGÊNCIA NACIONAL DE AVIAÇÃO CIVIL – BRAZIL
BRAZILIAN AIRWORTHINESS DIRECTIVE
AD No.: 2016-05-01 Effective Date: 27 May 2016
The following Brazilian Airworthiness Directive (AD), issued by the Agência Nacional de Aviação Civil
(ANAC) in accordance with provisions of Chapter IV, Title III of Código Brasileiro de Aeronáutica - Law No.
7,565 dated 19 December 1986 - and Regulamento Brasileiro da Aviação Civil (RBAC) 39, applies to all aircraft
registered in the Registro Aeronáutico Brasileiro. No person may operate an aircraft to which this AD applies,
unless it has previously complied with the requirements established herein.
AD No. 2016-05-01 - EMBRAER / 39-1399.
APPLICABILITY:
(a) This Airworthiness Directive (AD) applies to Embraer S.A. airplanes specified in
paragraphs (a)(1) and (a)(2) of this AD.
(1) Embraer S.A. EMB-500 airplanes, as identified in Embraer S.A. Service Bulletin 500-25-
0016, original issue, dated December 8, 2015.
(2) Embraer S.A. EMB-505 airplanes, as identified in Embraer S.A. Service Bulletin 505-25-
0020, original issue, dated December 8, 2015.
CANCELLATION / REVISION:
Not applicable.
REASON:
There is the possibility that certain attachment fittings of passenger seats have been
incorrectly installed. This AD results from a determination that the passenger seat on which the attachment
fittings were improperly installed may not meet certain static strength, and dynamic strength criteria. Failure
to meet static and dynamic strength criteria could result in injuries to the occupants during an emergency
landing condition.
REQUIRED ACTION:
This AD requires the inspection of each passenger seat for the correct installation of the
attachment fittings and correction, if necessary.
COMPLIANCE:
Required as indicated below, unless already accomplished.
Inspection and correction of the attachment fittings of each passenger seat
(b) Within 30 month after the effective date of this AD, do a detailed inspection on each
passenger seat for the correct installation of the attachment fittings, and prior to further flight after this
inspection, correct any discrepancy; in accordance with the Accomplishment Instructions of Embraer S.A
Service Bulletin 500-25-0016, original issue, dated December 8, 2015, or Embraer S.A. Service Bulletin
505-25-0020, original issue, dated December 8, 2015, as applicable.
Form F-900-04F
CONTINUATION OF AD No.: 2016-05-01 / 39-1399 PAGE No.: 2/2
Material Incorporated by Reference
(c) You must use the service information specified in paragraphs (c)(1) or (c)(2) of this this
AD, as applicable, to do the actions required by this AD.
(1) Embraer S.A. Service Bulletin 500-25-0016, original issue, dated December 8, 2015, or
further revisions approved by the ANAC.
(2) Embraer S.A. Service Bulletin 505-25-0020, original issue, dated December 8, 2015, or
further revisions approved by the ANAC.
Alternative Means of Compliance (AMOC)
(d) A different method or a different compliance time, with the requirements of this AD, may
be used if approved by the General Manager of the Aeronautical Product Certification Branch (Gerência-
Geral de Certificação de Produtos Aeronáuticos – GGCP)
CONTACT:
For additional technical information, contact:
National Civil Aviation Agency (ANAC)
Aeronautical Products Certification Branch (GGCP)
Rua Laurent Martins, n° 209, Jardim Esplanada
CEP 12242-431 – São José dos Campos - SP
Fax: (12) 3203-6600; E-mail: pac@anac.gov.br
APPROVAL:
MÁRIO IGAWA
General Manager
GGCP
DINO ISHIKURA
Airworthiness Superintendent
ANAC
NOTE: Original in Portuguese language signed and available in the files of the Aeronautical Products
Certification Branch (GGCP) of the National Civil Aviation Agency (ANAC).
Form F-900-04F
Lufttüchtigkeitsanweisung Luftfahrt-Bundesamt
- Sachgebiet T23 -
D-2016-140 38144 Braunschweig
FAA AD 2016-08-09 - Amdt. 39-18485 Fax: +49-531-2355-5298
email: ad@LBA.de
PRATT & WHITNEY 31.05.2016
Betroffenes Luftfahrtgerät:
Art des Luftfahrtgerätes: Flugmotor
Inhaber der Musterzulassung: Pratt & Whitney Division
Hersteller: PRATT & WHITNEY
Muster: PW4000-94"
PW4000-100"
Baureihen: PW4000-94": PW4050, PW4052, PW4056, PW4060, PW4060A, PW4060C,
PW4062, PW4062A, PW4152, PW4156, PW4156A, PW4158, PW4160,
PW4460, PW4462 und PW4650 (inklusive Baureihen mit einem "-3" Suffix).
PW4000-100": PW4164, PW4168, PW4168A, PW4164C, PW4164C/B,
PW4170, PW4168A-1D, PW4168-1D, PW4164-1D, PW4164C-1D und
PW4164C/B-1D.
Werknummern: Alle
Es sind PW4000-94'' Triebwerke betroffen, die im Hochdruckverdichter (High
Pressure Compressor (HPC)) eine "HPC 10th Stage Disk" der Part-Nummer
(P/N) 51H710 installiert haben und die Seriennummer der "HPC 10th Stage
Disk" in der TABELLE 1 des Pratt & Whitney Division Alert Service Bulletin
PW4ENG A72-833 vom 20.08.2015 aufgeführt ist.
Es sind PW4000-94'' Triebwerke betroffen, die im Hochdruckverdichter (High
Pressure Compressor (HPC)) eine "HPC 10th Stage Disk" der Part-Nummer
(P/N) 53H976-06 installiert haben und die Seriennummer der "HPC 10th Stage
Disk" in der TABELLE 2 des Pratt & Whitney Division Alert Service Bulletin
PW4ENG A72-833 vom 20.08.2015 aufgeführt ist.
Es sind PW4000-100'' Triebwerke betroffen, die im Hochdruckverdichter (High
Pressure Compressor (HPC)) eine "HPC 10th Stage Disk" der Part-Nummer
(P/N) 53H976-06 installiert haben und die Seriennummer der "HPC 10th Stage
Disk" in der TABELLE 1 des Pratt & Whitney Division Alert Service Bulletin
PW4G-100-A72-255 vom 31.08.2015 aufgeführt ist.
Gerätenummer: 6323, 6331, EASA.IM.E.043, EASA.IM.E.050, FAA TCDS E24NE, FAA TCDS
E36NE
Revisionsstand:
Originalausgabe
Airworthiness Directive der ausländischen Behörde:
FAA AD 2016-08-09 - Amdt. 39-18485
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 2016-140 geführt.
Betrifft:
(ATA 72) Engine - High-Pressure Compressor 10th Stage Disk - Inspection
D-2016-140 Seite 1 von 2 210/2016
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 FAA AD 2016-08-09 - Amdt. 39-18485 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-2016-140 Seite 2 von 2 210/2016
[Federal Register Volume 81, Number 81 (Wednesday, April 27, 2016)]
[Rules and Regulations]
[Pages 24696-24699]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2016-09687]
––––––––––––––––––––––––––––––––––
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2015-4474; Directorate Identifier 2015-NE-34-AD; Amendment 39-18485;
AD 2016-08-09]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney Division Turbofan Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
––––––––––––––––––––––––––––––––––
SUMMARY: We are adopting a new airworthiness directive (AD) for certain Pratt & Whitney
Division (PW) PW4000-94 inch and PW4000-100 inch model turbofan engines. This AD was
prompted by a report of a crack found in the high-pressure compressor (HPC) 10th stage disk. This
AD requires performing an ultrasonic inspection (USI) or an eddy current inspection (ECI) of the
HPC 10th stage disk. We are issuing this AD to prevent failure of the HPC 10th stage disk,
uncontained disk release, damage to the engine, and damage to the airplane.
DATES: This AD is effective June 1, 2016.
The Director of the Federal Register approved the incorporation by reference of certain
publications listed in this AD as of June 1, 2016.
ADDRESSES: For service information identified in this final rule, contact Pratt & Whitney Division,
400 Main St., East Hartford, CT 06108; phone: 860 565-8770; fax: 860 565-4503. You may view this
service information at the FAA, Engine & Propeller Directorate, 1200 District Avenue, Burlington,
MA. For information on the availability of this material at the FAA, call (781) 238-7125. It is also
available on the Internet at http://www.regulations.gov by searching for and locating Docket No.
FAA-2015-4474.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov by searching for
and locating Docket No. FAA-2015-4474; or in person at the Docket Management Facility between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD,
the regulatory evaluation, any comments received, and other information. The address for the Docket
Office (phone: 800-647-5527) is Document Management Facility, U.S. Department of
1
