FAA Biweekly AD Report 2015-23

The latest airworthiness directive biweekly report from FAA by myairlease.com

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FAA

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

This AD applies to The Boeing Company Model 737-200, -200C, -300, -400, and -500 series airplanes, certificated in any category, line numbers 292 through 2565 inclusive.

FAA AD 2002-07-08

FAA AD 2013-09-01



(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 737-53A1177, Revision 7, dated June 14, 2013.

(ii) Reserved.

(3) The following service information was approved for IBR on May 17, 2002 (67 FR 17917, April 12, 2002).

(i) Boeing Service Bulletin 737-53A1177, Revision 5, dated February 15, 2001.

(ii) Boeing Service Bulletin 737-53A1177, Revision 6, dated May 31, 2001.

FAA

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

This AD applies to Airbus Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes; 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, and A300 C4-605R Variant F airplanes; and Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes; certificated in any category, all manufacturer serial numbers.

FAA AD 2009-18-15

FAA AD 84-02-04 and
EASA AD 2013-0248



(3) The following service information was approved for IBR on November 27, 2015.

(i) ALS Part 1, "Safe Life Airworthiness Limitation Items," Revision 01, dated September 5, 2013, of the Airbus Model A300 Airworthiness Limitations Section.

(ii) ALS Part 1, "Safe Life Airworthiness Limitation Items," Revision 01, dated September 5, 2013, of the Airbus Model A300-600 Airworthiness Limitations Section.

(iii) ALS Part 1, "Safe Life Airworthiness Limitation Items," Revision 01, dated September 5, 2013, of the Airbus Model A310 Airworthiness Limitations Section.

(4) The following service information was approved for IBR on October 27, 2009 (74 FR 48143, September 22, 2009).

(i) Section 05-10-00 of Chapter 05, "Service Life Limits and Maintenance Checks," of the Airbus A300 Aircraft Maintenance Manual (AMM), Revision 28, dated February 27, 1998.

(A) The AMM title page; the Record of Revisions, Effective Pages, and Table of Content pages; and Section 05-10-00; for Chapter 05 of Airbus A300 AMM are all dated February 27, 1998.

(B) The revision level of Chapter 05 of the Airbus A300 AMM is indicated only in the Record of Revisions section of Chapter 05.

(C) The List of Effective Pages (LOEP) for Chapter 05 of the Airbus A300 AMM contains the discrepancies identified in paragraphs (n)(4)(i)(C)(1) through (n)(4)(i)(C)(4) of this AD.

bsection 05-00-01, Subsection 05-10-00, and page 1 of Subsection 05-11-11, are not listed in the LOEP for Chapter 05 of the Airbus A300 AMM.

(2) The LOEP for Chapter 05 of the Airbus A300 AMM does not specify a date for the Record of Revisions page.

(3) The LOEP for Chapter 05 of the Airbus A300 AMM identifies three pages for Subsection 05-11-00, Configuration 5; however, only one page exists.

(4) The LOEP for Chapter 05 of the Airbus A300 AMM identifies three pages for Subsection 05-11-00, Configuration 9; however, those pages do not exist.

(ii) Airbus A300 Airworthiness Limitations Section, ALS Part 1, "Safe Life Airworthiness Limitations Items" dated September 6, 2007.

(iii) Airbus A300-600 Airworthiness Limitations Section, ALS Part 1, "Safe Life Airworthiness Limitations Items" dated December 21, 2006.

(iv) Airbus A310 Airworthiness Limitations Section, ALS Part 1, "Safe Life Airworthiness Limitation Items" dated December 21, 2006.

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) through (c)(4) of this AD, all manufacturer serial numbers.

(1) Airbus Model A318-111, -112, -121, and -122 airplanes.

(2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.

(3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes.

(4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.

N/A

EASA AD 2015-0191



(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.

(i) Airbus A318/A319/A320/A321 Temporary Revision TR572, Issue 1.0, dated August 13, 2015, to the Airbus A318/A319/A320/A321 Airplane Flight Manual.

(ii) Reserved.

FAA

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

This AD applies to Lockheed Martin Corporation/Lockheed Martin Aeronautics Company Model 188A and 188C airplanes, certificated in any category, serial numbers 1001 and subsequent

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) Lockheed Martin Electra Service Bulletin 88/SB-722, dated April 30, 2014.

(ii) Reserved.

FAA

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

This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category, 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.

N/A

FAA 2014-23-15 and
EASA AD 2014-0141



(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.

(i) Airbus A318/A319/A320/A321 ALS Part 1-Safe Life Airworthiness Limitation Items, Revision 02, dated May 13, 2011. The revision level of this document is identified on only the title page and in the Record of Revisions. The revision date is not identified on the title page of this document.

(ii) Reserved.

FAA

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

This AD applies to The Boeing Company Model 787-8 airplanes, certificated in any category, as identified in Boeing Alert Service Bulletin B787-81205-SB530024-00, Issue 002, dated June 5, 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-SB530024-00, Issue 002, dated June 5, 2015.

(ii) Reserved.

FAA

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

This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(4) of this AD, certificated in any category, all manufacturer serial numbers.

(1) Airbus Model A318-111, -112, -121, and -122 airplanes.

(2) Airbus Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes.

(3) Airbus Model A320-211, -212, -214, -231, -232, and -233 airplanes.

(4) Airbus Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes.

N/A

EASA AD 2013-0302



(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 A320-55-1041, Revision 01, dated February 24, 2014.

(ii) Reserved.

FAA

No subject

This AD applies to all General Electric Company (GE) GEnx-1B model turbofan engines with oil filler cap, part number (P/N) 2349M62G01, installed, that do not contain any of the following markings after the P/N on the oil filler cap scupper: "P/M BALL PP," or "RW," or "79-0022."

N/A

N/A



None

 

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