EASA Biweeky AD Report 2015-04

The latest EASA bi-weekly AD report 2015-04.

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<img src="http://www.myairlease.com/images2/adm/easa_ad_2015-0019R1.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/2015-0019R1" target="_blank">
Optional Equipment - External Rescue Hoist System - Inspection /
Modification
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
MBB-BK117 C-2 and MBB-BK117 D-2 helicopters, all serial numbers, if
equipped with a Goodrich external mounted hoist.
</td></tr>
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<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> EASA AD 2014-0057<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
AHD ASB MBB-BK117 C-2-85A-041 Revision 3, dated 03 February 2015, or
Revision 4, dated 12 February 2015.<br />
AHD ASB MBB-BK117 D-2-85A-002 original issue, dated 03 February 2015, or
Revision 1, dated 12 February 2015.<br />
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD.
</td></tr>


<tr><td style="font-size:0.9em; font-family:arial,'times',serif;">
<img src="http://www.myairlease.com/images2/adm/easa_ad_2015-0021.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/2015-0021" target="_blank">
Powerplant - Aft Engine Mount Retainers - Inspection / Replacement
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
Airbus A318-111, A318-112, A319-111, A319-112, A319-113, A319-114, A319-115, A320-211, A320-212, A320-214, A320-215, A320-216, A321-111, A321-112, A321-211, A321-212 and A321-213 aeroplanes, all manufacturer serial numbers.
</td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; padding-bottom:30px;">
<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> EASA AD 2013-0050<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
Airbus AOT A71N001-12, Revision 01 dated 09 August 2012, or Revision 02 dated 27 February 2013.<br />
Airbus SB A320-71-1060 dated 09 October 2014.<br />
Goodrich Aerostructures SB RA32071-146, Revision 2 dated 26 July 2012.<br />
Goodrich Aerostructures SB RA32071-160, original issue dated 18 September 2014.<br />
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
</td></tr>


<tr><td style="font-size:0.9em; font-family:arial,'times',serif;">
<img src="http://www.myairlease.com/images2/adm/casa_ad_GA8-8.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/GA8-8" target="_blank">
Engine Mount Fire Seal Washer
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
All GA8-TC 320 aircraft.
</td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; padding-bottom:30px;">
<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
GippsAero Service Bulletin SB-GA8-2014-115
</td></tr>


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<img src="http://www.myairlease.com/images2/adm/easa_ad_2015-0020.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/2015-0020" target="_blank">
Doors - Sliding Door Star Support - Modification
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
EC 120 B helicopters, all Serial Numbers (S/N), equipped with sliding door Part Number (P/N) C526A2370101, except those helicopters that have incorporated modification (MOD) A00565 (reinforcement of the sliding door star support attachment), and<br />
EC 130 B4 helicopters, all S/N, equipped with sliding door P/N C526S1101051, except those helicopters that have incorporated MOD 07 3796 (reinforcement of the sliding door star support attachment), or have incorporated Eurocopter MOD 07 2921 (industrialized sliding door).
</td></tr>
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<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> EASA AD 2013-0093<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
Eurocopter ASB EC120 No 52A014 original issue dated 16 January 2004, or Revision 1 dated 25 January 2013, and Airbus Helicopters EC120 ASB No.52A014 Revision 2 dated 28 October 2013.<br />
Eurocopter ASB EC130 No 52A009 original issue dated 30 March 2010, or Revision 1 dated 25 January 2013.<br />
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.<br />
</td></tr>


<tr><td style="font-size:0.9em; font-family:arial,'times',serif;">
<img src="http://www.myairlease.com/images2/adm/easa_ad_2015-0018.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/2015-0018" target="_blank">
Equipment / Furnishing - Type III Emergency Exit Door -
Modification
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
ATR 42-500 aeroplanes, all manufacturer serial numbers (MSN), on which ATR
Modification (mod) 6518 has been embodied in production, except those
aeroplanes on which ATR mod 7294 has been embodied in production.<br />
ATR 72-212A aeroplanes, all MSN, on which ATR mod 6517 has been
embodied in production, except those aeroplanes on which ATR mod 7294 has
been embodied in production.<br />
Note: ATR mod 6517 and mod 6518 install the &#39;Armonia&#39; Cabin respectively on
ATR 72-212A and ATR 42-500 aeroplane.
</td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; padding-bottom:30px;">
<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> EASA AD 2013-0280<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
ATR SB ATR42-25-0180 original issue, dated 19 August 2013,<br />
ATR SB ATR72-25-1141 original issue, dated 19 August 2013,<br />
ATR SB ATR42-25-0185 original issue, dated 21 November 2014,<br />
ATR SB ATR42-25-0186 original issue, dated 21 November 2014,<br />
ATR SB ATR72-25-1148 original issue, dated 21 November 2014,<br />
ATR SB ATR72-25-1149 original issue, dated 21 November 2014.<br />
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD.
</td></tr>


<tr><td style="font-size:0.9em; font-family:arial,'times',serif;">
<img src="http://www.myairlease.com/images2/adm/easa_ad_2012-0052R1.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/2012-0052R1" target="_blank">
Wings - Leading Edge Shear Cleats - Inspection / Replacement
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial
numbers (MSN), except aeroplanes having embodied Airbus modification
(mod) 73979, mod 73981 and mod 73983 in producti
</td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; padding-bottom:30px;">
<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
Airbus SB A380-57-8035 original issue, dated 16 September 2011, or
Revision 01 dated 30 August 2013.<br />
Airbus SB A380-57-8089 original issue 01 October 2014.<br />
The use of later approved revisions of these documents is acceptable for
compliance with the requirements of this AD.
</td></tr>


<tr><td style="font-size:0.9em; font-family:arial,'times',serif;">
<img src="http://www.myairlease.com/images2/adm/easa_ad_2015-0017.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/2015-0017" target="_blank">
Equipment / Furnishings - Rescue Hoist Control Grip - Inspection / Replacement
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
BO105 A, BO105 C, BO105 D, BO105 S and BO105 LS A-3 helicopters, all variants, all serial numbers, if equipped with a rescue hoist system Part Number (P/N) 105-81100, P/N 105-81103 or P/N105-811011.
</td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; padding-bottom:30px;">
<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> EASA AD 2014-0235<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
AHD ASB BO105-80A-150 original issue dated 27 October 2014, or Revision 1 dated 02 February 2015.<br />
AHD ASB BO105 LS-80A-036 original issue dated 27 October 2014, or Revision 1 dated 02 February 2015.<br />
AHD BO105 C/CS TempRev 1, EASA approved on 29 January 2015.<br />
AHD BO105 CB/CBS TempRev 1, EASA approved on 29 January 2015.<br />
AHD BO105 CB-5/CBS-5 TempRev 1, EASA approved on 29 January 2015.<br />
AHD BO105 DB/DBS TempRev 1, EASA approved on 29 January 2015.<br />
AHD BO105 DBS-5 TempRev 1, EASA approved on 29 January 2015.<br />
AHD BO105 LS A-3 TempRev 1, EASA approved on 29 January 2015.<br />
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
</td></tr>


<tr><td style="font-size:0.9em; font-family:arial,'times',serif;">
<img src="http://www.myairlease.com/images2/adm/easa_ad_2015-0010R1.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/2015-0010R1" target="_blank">
Starting - Starter Solenoid - Inspection / Modification
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
GROB G 115E and G 115EG aeroplanes, all serial numbers (S/N) up to and including S/N 82323/E, and<br />
GROB G 120A and G 120A-I aeroplanes, all S/N up to and including S/N 85063.
</td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; padding-bottom:30px;">
<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> EASA AD 2014-0212<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
GROB Aircraft AG MSB1078-196 original issue dated 14 July 2014 or MSB1078-196/1 dated 01 December 2014. (for G 115E and G 115EG).<br />
GROB Aircraft AG MSB1121-144 original issue dated 14 July 2014 or MSB1121-144/1 dated 12 January 2015. (for G 120A and G 120A-I).<br />
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
</td></tr>


<tr><td style="font-size:0.9em; font-family:arial,'times',serif;">
<img src="http://www.myairlease.com/images2/adm/iac_ad_RU-2014-55-01.png" alt="EASA">
<a href="http://ad.easa.europa.eu/ad/RU-2014-55-01" target="_blank">
Tu-204 and Tu-214 stabilizers
</a></td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; color:#666666;">
TU-204-100,
TU-204-100B,
TU-204-100C,
TU-204-100E,
TU-204-120,
TU-204-120CE,
TU-204-204C,
TU-204-300,
TU-204-300A,
TU-204CE
</td></tr>
<tr><td style="font-size:0.8em; font-family:arial,'times',serif; padding-bottom:30px;">
<img src="http://www.myairlease.com/images2/adm/supersedes.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/relates.png" style="vertical-align:middle;"> N/A<br />
<img src="http://www.myairlease.com/images2/adm/refpubs.png"><br />
See AD
</td></tr>


</table>

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