FAA Biweekly AD Report 2016-01

Read the latest FAA airworthiness directives from myairlease.

FAA CORRECTION Air Transport Association (ATA) of America Code 57, Wings
This AD applies to The Boeing Company Model 747-100, 747-100B, 747-100B SUD, 747-200B, 747-200C, 747-200F, 747-300, 747-400, 747-400D, 747-400F, and 747SR series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 747-57A2343, Revision 1, dated June 23, 2014.
FAA AD 2013-23-03
N/A

(3) The following service information was approved for IBR on January 28, 2016.
(i) Boeing Alert Service Bulletin 747-57A2343, Revision 1, dated June 23, 2014.
(ii) Reserved.
(4) The following service information was approved for IBR on November 29, 2013 (78 FR 68345, November 14, 2013).
(i) Boeing Alert Service Bulletin 747-57A2343, dated September 12, 2013.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 54, Nacelles/Pylons
This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category.
(1) Airbus Model A300 B2-1C, B2-203, B2K-3C, B4-103, B4-203, and B4-2C airplanes, on which Airbus Modification 02434 has been embodied in production.
(2) Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes, except those on which Airbus Modification 10432 has been embodied in production.
(3) Airbus Model A300 B4-601, B4-603, B4-605R, B4-620, B-622, and B4-622R airplanes, except those on which Airbus Modification 10432 has been embodied in production.
FAA AD 2010-06-04
EASA AD 2013-0136R1

(3) The following service information was approved for IBR on February 2, 2016.
(i) Airbus Service Bulletin A300-54-0075, Revision 03, excluding Appendixes 1, 2, 3, and 5; including Appendix 4; dated March 27, 2013.
(ii) Airbus Service Bulletin A300-54-0081, dated August 11, 1993.
(iii) Airbus Service Bulletin A300-54-6015, Revision 03, excluding Appendixes 1, 2, 3, and 5; including Appendix 4; dated April 11, 2013.
(iv) Airbus Service Bulletin A300-54-6021, Revision 02, dated May 21, 2008.
(v) Airbus Service Bulletin A310-54-2018, Revision 03, excluding Appendixes 1, 2, 3, and 5; including Appendix 4; dated April 11, 2013.
(vi) Airbus Service Bulletin A310-54-2024, dated August 11, 1993.
(4) The following service information was approved for IBR on April 15, 2010 ((75 FR 11428, March 11, 2010); corrected May 4, 2010 (75 FR 23572)).
(i) Airbus Mandatory Service Bulletin A300-54-0075, excluding Appendixes 1, 2, and 3, Revision 02, dated June 26, 2008.
(ii) Airbus Mandatory Service Bulletin A300-54-6015, excluding Appendixes 1, 2, and 3, Revision 02, dated June 26, 2008.
(iii) Airbus Mandatory Service Bulletin A310-54-2018, excluding Appendixes 1, 2, and 3, Revision 02, dated June 26, 2008.
FAA Air Transport Association (ATA) of America Code 29, Hydraulic Power
This AD applies to all Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD, all manufacturer serial numbers.
(1) Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
(2) Model A340-211, -212, -213, -311, -312, -313, -541, and -642 airplanes.
N/A
FAA AD 2012-21-19, FAA AD 2012-21-20 and EASA AD 2013-0274

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Service Bulletin A330-29-3122, dated October 25, 2012.
(ii) Airbus Service Bulletin A330-29-3126, dated June 12, 2014.
(iii) Airbus Service Bulletin A340-29-4093, dated October 25, 2012.
(iv) Airbus Service Bulletin A340-29-4097, dated June 12, 2014.
(v) Airbus Service Bulletin A340-29-5021, dated October 2, 2012.
(vi) Airbus Service Bulletin A340-29-5025, dated June 16, 2014.
(vii) Hamilton Sundstrand Service Bulletin ERPS06M-29-19, dated August 6, 2012.
FAA Air Transport Association (ATA) of America Code 25, Equipment/Furnishings
This AD applies to Bombardier, Inc. Model BD-100-1A10 (Challenger 300) airplanes, certificated in any category, serial numbers 20001 through 20274.
FAA AD AD 2011-07-10
TC AD CF-2010-06R1

(3) The following service information was approved for IBR on February 2, 2016.
(i) Bombardier Service Bulletin 100-25-21, Revision 02, dated July 25, 2013.
(ii) Reserved.
(4) The following service information was approved for IBR on May 5, 2011, (76 FR 17758, March 31, 2011).
(i) Bombardier Service Bulletin A100-21-08, dated June 18, 2009.
(ii) Bombardier Service Bulletin 100-25-14, dated June 30, 2008.
(iii) Bombardier Service Bulletin 100-25-21, dated June 30, 2008.
(iv) Bombardier Temporary Revision (TR) 5-2-53, dated October 1, 2009, to Section 5-10-40, "Certification Maintenance Requirements," in Part 2 of Chapter 5 of Bombardier Challenger 300 BD-100 Time Limits/Maintenance Checks.
FAA Air Transport Association (ATA) of America Code 53, Fuselag
(1) This AD applies to The Boeing Company Model 767-200, -300, -300F series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 767-53A0261, dated August 12, 2014.
(2) Installation of Supplemental Type Certificate (STC) ST01920SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01920SE is installed, a "change in product" alternative method of compliance (AMOC) approval request is not necessary to comply with the requirements of 14 CFR 39.17.
N/A
N/A

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Boeing Alert Service Bulletin 767-53A0261, dated August 12, 2014.
(ii) Reserved.
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