FAA Biweekly AD Report

The latest ADs from myairlease.

FAA Air Transport Association (ATA) of America Code 53, Fuselage
(1) This AD applies to The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes; certificated in any category; as identified in Boeing Alert Service Bulletin 737-53A1163, Revision 1, dated January 8, 2014.
(2) Installation of Supplemental Type Certificate (STC) ST01219SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01219SE 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 Service Bulletin 737-53-1163, dated December 21, 1993.
(ii) Boeing Alert Service Bulletin 737-53A1163, Revision 1, dated January 8, 2014.
FAA Air Transport Association (ATA) of America Code 53, Fuselage
This AD applies to Airbus Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes; Model A300 B4-605R and B4-622R airplanes; Model A300 F4-605R and F4-622R airplanes; and Model A300 C4-605R Variant F airplanes; certificated in any category; on which Airbus Modification 6146 has not been installed.
FAA AD 98-13-23
EASA AD 2013-0048

(i) Airbus Service Bulletin A300-53-6042, Revision 03, dated August 30, 2012.
(ii) Reserved.
(4) The following service information was approved for IBR on July 30, 1998 (63 FR 34576, June 25, 1998).
(i) Airbus Service Bulletin A300-53-6042, Revision 1, dated February 20, 1995.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 28, Fuel.
This AD applies to Bombardier, Inc. Model DHC-8-102, -103, -106, -201, -202, -301, -311, and -315 airplanes, certificated in any category, serial numbers (S/N) 003 through 624 inclusive, and 626.
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FAA AD 2008-13-09 and TC AD CF-2007-32R2

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Temporary Revision AWL 2-43, dated August 31, 2007, to Part 2, "Airworthiness Limitations," of the Bombardier Dash 8 Series 200 Maintenance Program Manual, PSM 1-82-7.
(ii) Bombardier Temporary Revision AWL 2-47, dated February 16, 2011, to Part 2, "Airworthiness Limitations," of the Bombardier Dash 8 Series 200 Maintenance Program Manual, PSM 1-82-7.
(iii) Bombardier Temporary Revision AWL 3-109, dated August 31, 2007, to Part 2, "Airworthiness Limitations," of the Bombardier Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7.
(iv) Bombardier Temporary Revision AWL 3-117, dated February 16, 2011, to Part 2, "Airworthiness Limitations," of the Bombardier Dash 8 Series 300 Maintenance Program Manual, PSM 1-83-7.
(v) Subject 5-FSL of Section 5, "Fuel System Limitations," of the "Airworthiness Limitations List," of the Bombardier Dash 8 Series 100 Maintenance Program Manual, PSM 1-8-7, Revision 18, dated February 23, 2012.
FAA No subject
This AD applies to all Pratt & Whitney (PW) JT8D-217C and JT8D-219 turbofan engines with low-pressure turbine (LPT) shaft part numbers 783319, 783319-001, 783319-003, 783319-004, 783320, 783320-001, 783320-003, 783320-004, 820514-001, 820514-003, 820514-004, or 820514-005, installed.
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N/A

None
FAA Air Transport Association (ATA) of America Code 27, Flight Controls.
This AD applies to The Boeing Company airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD.
(1) Model 747-8 and 747-8F series airplanes, as identified in Boeing Alert Service Bulletin 747-27A2506, dated February 3, 2014.
(2) Model 747-8 and 747-8F series airplanes, as identified in Boeing Service Bulletin 747-27A2513, Revision 1, dated July 18, 2014.
(3) Model 747-8 series airplanes that are operated less than 1,200 flight hours per calendar year.
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 747-27A2506, dated February 3, 2014.
(ii) Boeing Service Bulletin 747-27A2513, Revision 1, dated July 18, 2014.
(iii) Boeing 747-8/8F Certification Maintenance Requirements (CMRs) Document D011U721-02-03, Revision December 2013.
FAA Air Transport Association (ATA) of America Code 27, Flight Controls
This AD applies to The Boeing Company Model 787-8 airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin B787-81205-SB270020-00, Issue 002, dated February 12, 2015.
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 B787-81205-SB270020-00, Issue 002, dated February 12, 2015.
(ii) Boeing Service Bulletin B787-81205-SB270023-00, Issue 001, dated July 24, 2014.
(iii) Boeing Service Bulletin B787-81205-SB270027-00, Issue 002, dated March 9, 2015.
(iv) Boeing Alert Service Bulletin B787-81205-SB270017-00, Issue 001, dated September 18, 2013.
FAA Air Transport Association (ATA) of America Code 71, Powerplant
This AD applies to Airbus Model A310-203 airplanes, certificated in any category, all manufacturer serial numbers.
N/A
EASA AD 2014-0191

(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 A310-71-2038, including Appendices 01 and 02, dated April 8, 2014.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 53, Fuselage.
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, 747SR, 747SP, 747-8F, and 747-8 series airplanes, certificated in any category, equipped with a main deck side cargo door (MDSCD)
N/A
N/A

None
FAA Air Transport Association (ATA) of America Code 53, Fuselage
This AD applies to The Boeing Company Model 747-100, -200B, and -200F series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 747-53A2463, Revision 2, dated June 16, 2014.
FAA AD 2004-13-02
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 747-53A2463, Revision 2, dated June 16, 2014.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 24, Electrical Power
This AD applies to the airplanes specified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Airbus Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes.
(2) Airbus Model A300 B4-601, B4-603, B4-620, B4-622, B4-605R, B4-622R, F4-605R, and F4-622R airplanes.
(3) Airbus Model A300 C4-605R Variant F airplanes.
FAA AD 2012-13-06
EASA AD 2013-0204

(3) The following service information was approved for IBR on August 28, 2015.
(i) Airbus Service Bulletin A300-24-0106, Revision 01, dated March 26, 2013.
(ii) Airbus Service Bulletin A300-24-6108, Revision 01, dated March 26, 2013.
FAA No subject
This AD applies to all General Electric Company (GE) GEnx-1B model turbofan engines with full authority digital engine control (FADEC) software version B175 or earlier, installed, and GEnx-2B model turbofan engines with FADEC software version C065 or earlier, installed.
N/A
N/A

None
FAA Air Transport Association (ATA) of America Code 53, Fuselage
(1) This AD applies to The Boeing Company Model 737-100, -200, -200C, -300, -400, and -500 series airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin 737-53A1108, Revision 7, dated July 7, 2014.
(2) Installation of Supplemental Type Certificate (STC) ST01219SE does not affect the ability to accomplish the actions required by this AD. Therefore, for airplanes on which STC ST01219SE 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.
FAA AD 98-22-10
FAA AD 90-06-02

(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 737-53A1108, Revision 7, dated July 7, 2014.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 27, Flight Controls.
This AD applies to Bombardier, Inc. Model BD-100-1A10 (Challenger 300) airplanes, equipped with a spoiler electronic control unit (SECU) having part number (P/N) C47330-006, C47330-007, or C47330-008; certificated in any category.
N/A
TC AD CF-2014-24

(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 100-27-16, dated October 31, 2013.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 27, Flight controls
This AD applies to BAE Systems (Operations) Limited Model 4101 airplanes, certificated in any category, all serial numbers.
N/A
EASA AD 2015-0099

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) BAE Systems (Operations) Limited Inspection Service Bulletin J41-27-068, dated January 21, 2014.
(ii) Reserved.
FAA Air Transport Association (ATA) of America Code 27, Flight Controls
This AD applies to the Airbus airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), (c)(3), and (c)(4) of this AD, all manufacturer serial numbers.
(1) Model A318-111, -112, -121, and -122 airplanes.
(2) Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.
(3) Model A320-211, -212, -214, -231, -232, and -233 airplanes.
(4) Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.
N/A
EASA AD 2014-0011R1

(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 A320-27-1227, Revision 01, dated October 7, 2013.
(ii) Reserved.
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