FAA Biweekly AD Report 2016-02

Air Transport Association (ATA) of America Code 57, Wings

(1) This AD applies to the airplanes identified in paragraphs (c)(1)(i) and (c)(1)(ii) of this AD, certificated in any category, except as provided by paragraph (c)(2) of this AD.
(i) Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes, all serial numbers, except those on which Airbus modification 55306 or 55792 has been embodied in production.
(ii) Airbus Model A340-211, -212, -213, -311, -312, and -313 airplanes, all serial numbers, except those on which Airbus modification 55306 or 55792 has been embodied in production.
(2) This AD does not apply to Airbus Model A340-211, -212, -213, -311, -312, and -313 airplanes on which the repair specified in Airbus Repair Drawing R57115053, R57115051, or R57115047 (installation of titanium doubler on both sides) has been accomplished. AD 2007-12-08, Amendment 39-15086 (72 FR 31171, June 6, 2007), applies to these airplanes.

FAA AD 2011-24-05
EASA AD 2014-0010R1

(3) The following service information was approved for IBR on February 17, 2016.
(i) Airbus Service Bulletin A330-57-3081, Revision 05, dated November 13, 2012.
(ii) Airbus Service Bulletin A330-57-3090, Revision 01, dated June 15, 2011.
(iii) Airbus Service Bulletin A330-57-3098, dated August 30, 2007.
(iv) Airbus Service Bulletin A330-57-3098, Revision 02, June 15, 2011.
(v) Airbus Service Bulletin A330-57-3098, Revision 03, dated September 24, 2012.
(vi) Airbus Service Bulletin A330-57-3117, dated January 25, 2013.
(vii) Airbus Service Bulletin A340-57-4089, Revision 05, dated November 13, 2012.
(viii) Airbus Service Bulletin A340-57-4098, Revision 01, dated June 15, 2011.
(ix) Airbus Service Bulletin A340-57-4106, dated August 30, 2007.
(x) Airbus Service Bulletin A340-57-4106, Revision 02, dated June 15, 2011.
(xi) Airbus Service Bulletin A340-57-4106, Revision 03, dated September 24, 2012.
(xii) Airbus Service Bulletin A340-57-4126, dated January 25, 2013.
(4) The following service information was approved for IBR on January 3, 2012 (76 FR 73496, November 29, 2011).
(i) Airbus Mandatory Service Bulletin A330-57-3081, including Appendix 01, Revision 04, dated May 31, 2011.
(ii) Airbus Service Bulletin A330-57-3098, Revision 01, excluding Appendix 1, dated July 31, 2009.
(iii) Airbus Mandatory Service Bulletin A340-57-4089, including Appendix 01, Revision 04, dated May 31, 2011.
(iv) Airbus Service Bulletin A340-57-4106, excluding Appendix 1, Revision 01, dated July 31, 2009.
(5) The following service information was approved for IBR on September 13, 2007 (72 FR 44731, August 9, 2007).
(i) Airbus Service Bulletin A330-57-3081, Revision 02, including Appendix 01, dated January 24, 2006.
(ii) Airbus Service Bulletin A340-57-4089, Revision 02, including Appendix 01, dated January 24, 2006.

Air Transport Association (ATA) of America Code 28, Fuel

This AD applies to Fokker Services B.V. Model F.28 Mark 1000, 2000, 3000, and 4000 airplanes, certificated in any category, all serial numbers

N/A
EASA AD 2014-0109

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Fokker F28 Proforma Service Bulletin SBF28-28-059, Revision 1, dated July 15, 2014.
(ii) Fokker F28 Appendix SB SBF28-28-059/APP01, dated July 15, 2014.

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to Airbus Model A320-211, -212, and -231 airplanes, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 22418 has been embodied in production.

FAA AD 2004-14-09
EASA AD 2014-0065

(3) The following service information was approved for IBR on February 18, 2016.
(i) Airbus Service Bulletin A320-57-1043, Revision 06, dated December 5, 2013.
(ii) Airbus Service Bulletin A320-57-1082, Revision 04, dated December 5, 2013.
(4) The following service information was approved for IBR on August 13, 2004 (69 FR 41398, July 9, 2004).
(i) Airbus Service Bulletin A320-57-1043, Revision 05, dated April 30, 2002.
(ii) Airbus Service Bulletin A320-57-1082, Revision 03, dated April 30, 2002.
(5) The following service information was approved for IBR on November 27, 1998 (63 FR 56542, October 22, 1998).
(i) Airbus Service Bulletin A320-57-1043, Revision 02, dated May 14, 1997. Pages 1 through 6, 8, 13, and 14 of this service bulletin are marked Revision 02, dated May 14, 1997; pages 7, 9 through 12, and 15 of this service bulletin are from the original issue, dated February 16, 1993.
(ii) Airbus Service Bulletin A320-57-1082, Revision 01, dated December 10, 1997.

Air Transport Association (ATA) of America Codes 53, Fuselage; and 57, Wings.

This AD applies to all ATR-GIE Avions de Transport Regional (ATR) Model ATR42-200, -300, -320, and -500 airplanes, certificated in any category.

N/A
EASA AD 2012-0193

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) ATR Job Instruction Card 535100 DVI 10097, "DVI of FR26 Floor Beam Around Cut-outs for Cooling & Hydrau Ducts," dated February 9, 2012.
(ii) Reserved.

No subject

This AD applies to General Electric Company (GE) GE90-76B, -77B, -85B, -90B, and -94B turbofan engines with high-pressure compressor (HPC) stage 8-10 spool, part number 1694M80G04, installed.

N/A
N/A

None

Air Transport Association (ATA) of America Code 27, Flight Controls

This AD applies to Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes, certificated in any category, serial numbers 7003 and subsequent, equipped with horizontal stabilizer trim actuator (HSTA) part numbers (P/N) 601R92305-1 (vendor P/N 8396-2), 601R92305-3 (vendor P/N 8396-3), or 601R92305-5 (vendor P/N 8396-4).

N/A
TC AD CF-2013-14

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 601R-27-161, Revision A, dated January 30, 2014.
(ii) Supplement 23, "Horizontal Stabilizer Trim Check," of Chapter 7 "Supplements," of Bombardier CL-600-2B19 Airplane Flight Manual CSP A-012, Volume 3, Revision 61, dated April 2, 2013.
(iii) Task C27-40-103-04, ''Operational Check (ground maintenance test) of the horizontal stabilizer trim control unit,'' in Bombardier CL-600-2B19 Temporary Revision 2A-56, dated June 4, 2012, to Appendix A, Certification Maintenance Requirements, of Part 2, Airworthiness Requirements, of the Bombardier CL-600-2B19 Maintenance Requirements Manual.

Air Transport Association (ATA) of America Code 32, Landing Gear

This AD applies to Airbus airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Model 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 airplanes; all manufacturer serial numbers; except those on which Airbus Modification 58896 has been embodied in production or embodied through Airbus Service Bulletin A330-32-3237.
(2) Model A340-211, A340-212, A340-213, A340-311, A340-312, and A340-313 airplanes; all manufacturer serial numbers; except those on which Airbus Modification 58896 has been embodied in production or embodied through Airbus Service Bulletin A340-32-4279.

N/A
EASA AD 2014-0222

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Alert Operators Transmission A32L004-14, dated July 28, 2014, including Appendixes 1, 2, 3, and 4, which are not dated.
(ii) Messier-Dowty Service Bulletin A33/34-32-272, dated November 16, 2007, including Appendixes A, B, C, and D, dated November 16, 2007.
(iii) Messier-Dowty Service Bulletin A33/34-32-272, Revision 1, dated September 22, 2008, including Appendixes A, B, C, and D, dated September 22, 2008.

Air Transport Association (ATA) of America Code 53, Fuselage.

This AD applies to The Boeing Company Model 747-100, -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 747-53A2494, Revision 1, dated January 9, 2015.

FAA AD AD 2005-01-09
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 747-53A2494, Revision 1, dated January 9, 2015.
(ii) Reserved.

Air Transport Association (ATA) of America Code 26, Fire Protection

This AD applies to The Boeing Company Model 737-400 series airplanes, certificated in any category, having serial numbers 23865, 24231, 24706, 24474, 25417, 27003, 27149, 25375, 26281, 28661, and 28881, as modified by Supplemental Type Certificate ST01114WI

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) Advanced Aircraft Extinguishers Service Bulletin TFA10-26-0020, Revision IR, dated January 12, 2015.
(ii) Reserved.

Air Transport Association (ATA) of America Code 71, Power Plant

This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) Airbus Model A319-113 and A319-114 airplanes, all manufacturer serial numbers.
(2) Airbus Model A320-211 and A320-212 airplanes, all manufacturer serial numbers.

N/A
EASA AD 2015-0229

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus Alert Operators Transmission (AOT) A71N010-15, dated September 30, 2015.
(ii) Reserved.

Air Transport Association (ATA) of America Code 32, Landing G

This AD applies to Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-211, -212, -214, -231, -232, and -233 airplanes; and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes; certificated in any category; all manufacturer serial numbers.

FAA AD 2013-13-04
EASA AD 2013-0202

(3) The following service information was approved for IBR on February 17, 2016.
(i) Airbus Service Bulletin A320-32-1346, Revision 07, dated February 10, 2015, including Appendices 01 and 02, dated February 10, 2015.
(ii) Task 32.30.00.17, "Functional Check of LGCIU Power Supply Relays," of Section C-32 of Section C, Systems and Powerplant, of the Airbus A318/A319/A320/A321 Maintenance Review Board Report, Revision 18, dated March 2013.
(4) The following service information was approved for IBR on August 14, 2013 (78 FR 41286, July 10, 2013).
(i) Airbus Service Bulletin A320-32-1346, Revision 04, including Appendices 01 and 02, dated April 22, 2011.
(ii) Airbus Service Bulletin A320-32-1349, Revision 03, including Appendix 1, dated October 5, 2011.

Air Transport Association (ATA) of America Code 52, Doors

This AD applies to Bombardier, Inc. Model DHC-8-400, -401, and -402 airplanes, certificated in any category, serial numbers 4001 and subsequent

N/A
TC AD CF-2013-20R1

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 84-52-77, Revision C, dated June 5, 2014, including Appendix A, which is undated, and attached Short Brothers Service Bulletin D8400-52-0011, Revision C, dated February 26, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 57, Wings

This AD applies to Airbus Model A320-211, -212, and -231 airplanes, certificated in any category, manufacturer serial numbers (MSN) 0001 through 0155 inclusive

FAA AD 98-18-26
EASA AD 2014-0069

(3) The following service information was approved for IBR on February 25, 2016.
(i) Airbus Service Bulletin A320-57-1178, Revision 01, dated May 28, 2014, including Appendix 01, dated May 28, 2014.
(ii) Reserved.

Air Transport Association (ATA) of America Code 52, Doors.

This AD applies to Bombardier, Inc. Model BD-700-1A10 and BD-700-1A11 airplanes, certificated in any category, serial numbers 9001 through 9476 inclusive and 9998.

N/A
TC AD CF-2014-25

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Service Bulletin 700-1A11-52-019, dated March 29, 2012.
(ii) Bombardier Service Bulletin 700-52-042, dated March 29, 2012.
(iii) Bombardier Service Bulletin 700-52-5007, dated March 29, 2012.
(iv) Bombardier Service Bulletin 700-52-6007, dated March 29, 2012.

Air Transport Association (ATA) of America Code 55, Stabilizers.

This AD applies to all Airbus Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes; Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes; Model A300 B4-605R and B4-622R airplanes; and Model A300 F4-605R, F4-622R, and A300 C4-605R Variant F airplanes; certificated in any category.

N/A
EASA AD 2014-0026

(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Airbus Service Bulletin A300-55-6050, Revision 01, dated August 20, 2014.
(ii) Airbus Service Bulletin A310-55-2051, Revision 01, dated August 20, 2014.

Air Transport Association (ATA) of America Code 05, Time Limits/Maintenance Checks

This AD applies to all DASSAULT AVIATION Model MYSTERE-FALCON 900 airplanes, certificated in any category.

FAA AD 2002-23-20
FAA AD 2010-26-05 and EASA AD 2013-0053

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Chapter 5-40, Airworthiness Limitations, Revision 20, dated October 2012, of the Dassault Aviation Falcon 900 Maintenance Manual.
(ii) Reserved.

Air Transport Association (ATA) of America Code 32, Landing Gear

This AD applies to Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, certificated in any category, serial numbers 10002 and subsequent, as identified in Bombardier Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014, including Appendixes A and B, both dated November 5, 2013.

N/A
TC AD CF-2014-42

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Modification Summary Package IS670528200033, Revision A-2, dated October 11, 2005.
(ii) Bombardier Service Bulletin 670BA-32-040, Revision D, dated July 2, 2014, including Appendix A, Revision A, dated July 2, 2014, and Appendix B, Revision B, dated July 2, 2014.
(iii) Bombardier Service Bulletin 670BA-32-040, Revision E, dated November 13, 2014, including Appendix A, Revision A, dated July 2, 2014, and Appendix B, Revision B, dated July 2, 2014.
(iv) Bombardier Service Bulletin 670BA-32-042, Revision A, dated July 2, 2014, including Appendixes A and B, both dated November 5, 2013.
(v) Bombardier Service Bulletin 670BA-32-043, dated July 2, 2014.
(vi) Bombardier Service Bulletin 670BA-32-043, Revision A, dated November 13, 2014.

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