EASA Biweekly AD Report 06-2015

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EASA Main Rotor - Main Rotor Blade Vibration Absorber - Modification

MBB-BK 117 C-2 and MBB-BK 117 D-2 helicopters, all serial numbers
N/A
N/A

AHD ASB MBB-BK117 C-2-62A-009 original issue dated 20 January 2015.
AHD ASB MBB-BK117 D-2-62A-001 original issue dated 20 January 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Electrical Power - Terminal Lugs - Inspection / Replacement
MBB-BK117 C-2 helicopters, serial numbers (s/n) as listed in Appendix 1 of this AD
N/A
N/A

AHD ASB MBB-BK117 C-2-24A-013 Revision 0 (original issue) dated 29 October 2014 or Revision 1 dated 25 November 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Powerplant - Propeller Governor Idler Gear Shaft - Inspection
F260, F260B, F260C, F260D, F260E and F260F aeroplanes, all serial numbers, if equipped with a Lycoming O-540, IO-540 or AEIO-540 'wide cylinder flange' engine with a front crankcase mounted propeller governor, and S208 and S208A aeroplanes, all serial numbers, if equipped with a Lycoming O-540 'wide cylinder flange' engine with a front crankcase mounted propeller governor. Note: Wide cylinder flange engines are identified by the suffix "A" or "E" in the serial number (refer to Lycoming Service Letter L220C).
N/A
FAA AD 2015-02-07

Alenia Aermacchi BT N° 260SB-136 dated 26 October 2012, or Revision 1 dated 12 November 2012.
Alenia Aermacchi BT N° 205B65 dated 26 October 2012, or Revision 1 dated 12 November 2012.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
Lycoming Service Instruction No. 1343B dated 15 June 2007.
Lycoming Service Letter No. L220C dated 2 August 2011.
EASA Wings - Movable Flap Track Fairing # 6 / Pivot Bracket - Inspection
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers on which Airbus modification (mod.) 68729 has been embodied in production or Airbus Service Bulletin (SB) A380-57-8017 has been embodied in service, except those on which Airbus mod. 71589 has been embodied in production or Airbus SB A380-57-8036 has been embodied in service.
N/A
N/A

Airbus AOT A57R008-15 original issue dated 10 March 2015.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
Airbus TD L5757D14029282 issue A dated 10 February 2015.
EASA Equipment / Furnishings - Life Raft / Sponson Ejectable Cowlings - Inspection / Modification
AS 332 L2 and EC 225 LP helicopters, all manufacturer serial numbers, if equipped with life rafts in the sponsons.
EASA AD 2013-0211-E
N/A

Eurocopter EC225 ASB No. 25A141 original issue, dated 10 September 2013.
Eurocopter AS332 ASB No 25.02.75 original issue, dated 10 September 2013.
Airbus Helicopters ASB EC225-25A155 original issue dated 14 January 2015.
Airbus Helicopters ASB AS332-25.02.89 original issue dated 14 January 2015.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Time Limits / Maintenance Checks - Airworthiness Limitations / Tension-Torsion Straps - Amendment / Replacement
BO105 LS A-3 helicopters, all variants, all serial numbers
N/A
N/A

AHD ASB BO105LS-10A-013 Revision 0 (original issue) dated 09 March 2015.
AHD AMM BO105LS A-3, Chapter 101-15.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA Wings - Aileron Fittings - Inspection
CN-235, CN-235-100, CN-235-200 and CN-235-300 aeroplanes, all serial numbers.
N/A
N/A

EADS-CASA (Airbus Military) AOT-CN235-57-0001 original issue dated 26 February 2014 or Revision 1 dated 14 March 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Powerplant - Forward Engine Mount - Inspection
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.
N/A
N/A

Airbus A318/A319/A320/A321 ALS Part 2, Revision 03, dated 27 October 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Fuselage - Fuselage Skin Repairs - Inspection
Airbus A318-111, A318-112, A318-121, A318-122, A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, A321-111, A321-112, A321-131, A321-211, A321-212, A321-213, A321-231 and A321-232 aeroplanes, all manufacturer serial numbers.
N/A
N/A

Airbus AOT A53N007-14 original issue, dated 22 July 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA Equipment / Furnishings - Cockpit Door - Modification
This AD applies to:
1. Airbus 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 and A330-343 aeroplanes, all manufacturer serial numbers (MSN), if modified in-service with Airbus Service Bulletin (SB) A330-25-3161, or with Airbus modification (mod) 50014 in production,
2. Airbus A340-211, A340-212, A340-213, A340-311, A340-312, A340-313, all MSN, if modified in service with Airbus SB A340-25-4181, or with Airbus mod 50014 in production, and
3. Airbus A340-541, A340-542, A340-642 and A340-643 aeroplanes, all MSN,
except aeroplanes on which Airbus mod 203066, or mod 203074, or mod 203372 has been embodied in production.
N/A
N/A

Airbus SB A330-25-3534 Revision 01 dated 23 October 2014.
Airbus SB A340-25-4349 Revision 01 dated 27 October 2014.
Airbus SB A340-25-5212 Revision 01 dated 27 October 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

 

 

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