EASA Biweeky AD Report

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EASA AD 2014-0280 - Oxygen - Passenger Chemical Oxygen Generators - Replacement

A310, A300-600 and A300-600STaeroplanes, all models, all manufacturer serial numbers.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus AOT A35W008-14 dated 18 December 2014.
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.
EASA AD 2014-0278 - Fuselage - Skin Above Lap Joint - Inspection
A320 aeroplanes, identified by Model and manufacturer serial number (MSN):
A320-212 MSN 1011, A320-214 MSN 1009, 1026 and 1030, A320-232 MSN 0977, and A320-233 MSN 1007 and 1013.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus AOT A53N009-14 original issue dated 17 December 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0277 - Oxygen - Passenger Chemical Oxygen Generators - Replacement
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, 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).
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.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus AOT A35L007-14 dated 18 December 2014.
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.
EASA AD 2014-0279 - Equipment / Furnishing - Restraint System Rotary Buckle Sub-Assembly - Identification / Replacement
Romtex Anjou Aeronautique model 358 torso restraint systems.
These restraint systems are known to be installed on, but not limited to, Airbus Helicopters EC130 T2, AS 350 B2 and B3 helicopters.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Romtex Anjou Aeronautique SB 358SB-14-101, original issue dated 09 October 2014, or Revision 01 dated 12 October 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0276 - Power Plant - Fan Cowl Door Hinge Nuts - Inspection / Replacement
Airbus A318-111, A318-112, A319-111, A319-112, A319-115, A320-214, A320-215, A320-216, A321-111, A321-112, A321-211, A321-212 and A321-213 aeroplanes, all manufacturer serial numbers.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus SB A320-71-1062, original issue dated 28 July 2014.
Goodrich Aerostructures SB RA32071-151, original issue dated 11 June 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0275 - Oxygen - Passenger Chemical Oxygen Generators - Replacement
 
Supersedes: N/A
Relates to: N/A
Ref. Publications
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 (MSN).
EASA AD 2014-0274 - Wings - Movable Flap Track Fairing - Inspection / Repair / Replacement
Airbus A380-841, A380-842 and A380-861 aeroplanes, all manufacturer serial numbers.
Supersedes: EASA AD 2012-0062
Relates to: N/A
Ref. Publications
Airbus ISB A380-57-8031 original issue dated 02 February 2012.
Airbus SB A380-57-8090 original issue dated 12 November 2014.
Airbus SB A380-57-8040 original issue dated 02 February 2012.
Airbus AOT A380-57A8027 original issue dated 24 June 2011.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0251R1 - Landing Gear - Brake Dual Distribution Valve - Modification
Airbus A319-111, A319-112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, A320-214, 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, except those on which Airbus modification (mod) 26925 has been embodied in production, which introduces a modified alternate braking system that removes the BDDV.
Supersedes: DGAC AD 2000-258-146(B)
Relates to: N/A
Ref. Publications
Airbus SB A320-32-1200, original Issue dated 17 September 1998, or Revision 01 dated 23 March 1999, or Revision 02 dated 29 January 2001.
Airbus SB A320-32-1203, original Issue dated 04 June 1999, or Revision 01 dated 12 October 2000, or Revision 02 dated 09 February 2001.
Airbus SB A320-32-1415, original Issue dated 02 September 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0270R1 - Wings - Wing Bottom Skin at Main Landing Gear Rib 5 - Inspection
Airbus A319-115, A319-133, A320-214, A320-216, A320-232 and A320-233 aeroplanes, manufacturer serial numbers (MSN) 5817, 5826, 5837, 5848, 5855, 5864, 5875, 5886, 5896 and 5910, and MSN 5918 and up.
Supersedes: N/A
Relates to: N/A
Ref. Publications
AOT A57N006-14 original issue dated 04 December 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
TC AD CF-2013-39R2 - Wings - Inboard Flap Hinge Box - Incorrectly Oriented (Hi-LOK/Hi-LITE) Fastener on Forward Attachment Fitting
Bombardier Inc.:
Model CL-600-1A11 (600) aeroplanes, serial numbers 1004 through 1085;
Model CL-600-2A12 (601 Variant) aeroplanes, serial numbers 3001 through 3066;
Model CL-600-2B16 (601-3A/3R Variant) aeroplanes, serial numbers 5001 through 5194.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Bombardier SB A600-0763 Revision 2
Bombardier A601-0627 Revision 2
TC AD CF-2014-43 - Propeller Overspeed Governor - Incorporation of New Certification Maintenance Requirement (CMR) Task
Bombardier Inc. model DHC-8-400, -401 and -402 aeroplane
Supersedes: N/A
Relates to: N/A
Ref. Publications
Maintenance Requirements Manual, PSM-1-84-7
TC AD CF-2014-44 - Flight Controls - Elevator Control System - Disconnect
Bombardier Inc.
Model CL-600-2C10 aeroplanes, serial numbers 10002 through 10337,
Models CL-600-2D15 and CL-600-2D24 aeroplanes, serial numbers 15001 through 15298.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Bombardier Aerospace SB 670BA-27-062
EASA AD 2014-0271 - Wings - Trailing Edge Rib at Wing Station 8700 - Inspection
F28 Mark 0070 and Mark 0100 aeroplanes, all serial numbers.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Fokker Services SBF100-57-048 original issue dated 27 October 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
More information on this subject can be found in Fokker Services All Operators Message AOF100.192.
EASA AD 2014-0272 - Wings - Frame 40 Lower Junction Fastener Holes - Inspection / Repair
Airbus A300 and A300-600 aeroplanes, all models, all Manufacturer Serial Numbers (MSN), and
Airbus A300-600ST aeroplanes, all MSN.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus SB A300-57-0257 original issue, dated 04 April 2014.
Airbus SB A300-57-6115 original issue, dated 04 April 2014.
Airbus SB A300-57-9030 original issue, dated 31 March 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0269 - Engine - Engine Redundancy System - Modification
Solo 2625 02i engines (Solo 2625 02 engines modified in accordance with the instructions of Solo Kleinmotoren GmbH Service Bulletin (SB)/Technische Mitteilung (TM) 4600-3 "Fuel Injection System"), all manufacturer serial numbers.
These engines are known to be installed on, but not limited to, Binder Motorenbau, DG-Flugzeugbau and Schempp-Hirth powered sailplanes.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Solo Kleinmotoren GmbH SB/TM 4600-5, issue 1 dated 24 November 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0140R1 - Main Rotor - Hydraulic Drag Damper Lug - Replacement
PZL SW-4 helicopters, all serial numbers. Those helicopters are fitted with main rotor hydraulic drag dampers Part Number (P/N) TLH48-1.
Supersedes: N/A
Relates to: N/A
Ref. Publications
WSK &PZL-Swidnik& S.A. MB No. BO-60-13-65 Revision 1 dated 27 May 2014 or Revision 2 dated 28 November 2014. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0234R1 - Fuel - Fuel Vent Protector - Inspection / Replacement
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 (MSN).
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus SB A320-28-1221 original issue dated 21 July 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
TC AD CF-2014-42 - Landing Gear - Main Landing Gear Door Forward Member Cracking
Bombardier Inc. model CL-600-2C10 aeroplanes, serial number 10002 and subsequent, equipped with inboard Main Landing Gear (MLG) door part numbers included in Section 1.A, Effectivity, of Bombardier Service Bulletin (SB) 670BA-32-042, Revision A, dated 2 July 2014.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Bombardier SB 670BA-32-043
EASA AD 2014-0268 - Main Rotor - Main Rotor Swashplate Pitch Link Spherical Bearings - Inspection / Replacement
PZL SW-4 helicopters, all serial numbers
Supersedes: N/A
Relates to: N/A
Ref. Publications
WSK "PZL-Swidnik" S.A. MB No. BO-60-14-72 dated 28 November 2014. The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0253R1 - Doors - Main Deck and Upper Deck Passenger Doors - Inspection
Airbus A380-841, A380-842, and A380-861 aeroplanes, all manufacturer serial numbers, except aeroplanes on which all the following Airbus modifications (mod) have been embodied in production: 75447, 75448, 75449, 75450, 75451, 75452, 75116, 75117, 75118, 75119, 75120, 75121, 75122, 75123, 75124 and 75125.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Inspection SB: as identified in Appendix 1 of this AD.
(Optional) Modification SB: as identified in Appendix 2 of this AD.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0225R1 - Engine - Engine Air Intake Box By-Pass Flap - Modification
R 1180 T and R 1180 TD aeroplanes, all serial numbers (s/n), and
ATL and ATL "S" aeroplanes, all s/n, and
DR 300 aeroplanes, all models, all s/n, except DR 380 and DR 300/180 R, and
DR 400 aeroplanes, all models, all s/n, except DR 400/125 i, DR 400/200 R, DR 400 RP and DR 400/500 aeroplanes.
This AD does not apply to DR 400/140 B aeroplanes, if modified in accordance with EASA STC No. 10014219 or STC EASA.A.S.01380 (TAE 125 diesel engine installation).
This AD does not apply to aeroplanes, if equipped with Air Box P/N 56.12.50.000 or P/N 56.15.01.010 or with By-Pass Flap P/N 56.15.01.120 or P/N 56.15.01.121.
Supersedes: DGAC AD 2001-036
Relates to: N/A
Ref. Publications
CEAPR SB No 120203 original issue dated 6 May 2014, or Revision 1 dated 3 July 2014, or Revision 2 dated 3 November 2014. Robin Aviation SB No. 174 dated November 29, 2000.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0243R1 - Engine Fuel and Control - Low Pressure Fuel Tubes and Clips, Fuel Oil Heat Exchanger Mounts - Inspection / Replacement
RB211 Trent 768-60, 772-60, 772B-60 and 772C-60 engines, all serial numbers, if fitted with fuel tube Part Number (P/N) FW53576, which was incorporated through RR modification 73-F343 in production, or by in-service modification in accordance with RR Service Bulletin (SB) RB.211-73-F343.
These engines are known to be installed on, but not limited to, Airbus A330 aeroplanes.
Supersedes: EASA AD 2014-0089
Relates to: N/A
Ref. Publications
Rolls-Royce NMSB RB.211-73-AH522 dated 20 September 2013, or Revision 1 dated 18 March 2014.
Rolls-Royce SB RB.211-73-F343 dated 08 November 2006, or Revision 1 dated 14 May 2009, or Revision 2 dated 1 July 2009, or Revision 3 dated 15 July 2009, or Revision 4 dated 26 May 2011.
Rolls-Royce NMSB RB.211-73-AH837 dated 09 September 2014.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0266E EMERGENCY - Airplane Flight Manual - Undue Activation of Alpha Protection - Emergency Procedure
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
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus AFM A320 TR 502 issue 1, EASA approved 05 December 2014.
The use of later approved revisions of this document is acceptable for compliance with the requirements of this AD.
EASA AD 2014-267E EMERGENCY - Airplane Flight Manual - Undue Activation of Alpha Protection - Emergency Procedure
Airbus A330-201, A330-202, A330-203, A330-223, A330-223F, 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).
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.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Airbus AFM A330 TR 528 issue 1, EASA approved 05 December 2014.
Airbus AFM A340 TR 529 issue 1, EASA approved 05 December 2014.
The use of later approved revisions of these documents are acceptable for compliance with the requirements of this AD.
EASA AD 2014-0264 - Power Plant - Engine Mounts - Inspection / Replacement
ASW 28-18E powered sailplanes, all manufacturer serial numbers.
Supersedes: N/A
Relates to: N/A
Ref. Publications
Alexander Schleicher ASW 28-18E TN 15, dated 01 September 2014,
Alexander Schleicher ASW 28-18E TN 10, dated 18 February 2009.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.
EASA AD 2014-0265 - Fuselage - Widespread Fatigue Damage / Sections 13 to 18 Longitudinal Lap Joints - Inspection
Airbus A300 aeroplanes, all certified models, all manufacturer serial numbers, (MSN), except those on which Airbus modification (MOD) 2611 has been embodied in production.
Note: Airbus MOD 2611 has been embodied in production from MSN 157 onwards.

Supersedes: EASA AD 2007-0091
Relates to: N/A
Ref. Publications
Airbus SB A300-53-0229 Revision 05 dated 08 April 1997.
Airbus SB A300-53-0211 Revision 08 dated 26 November 2013.
The use of later approved revisions of these documents is acceptable for compliance with the requirements of this AD.

 

                                                                           

 

 

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