FAA Biweekly AD Report 2015-07

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

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 003 through 672 inclusive.
FAA AD 2014-06-08
TC AD CF-2014-11

(3) The following service information was approved for IBR on April 14, 2014 (79 FR 17390, March 28, 2014).
(i) Bombardier Service Bulletin 8-32-173, Revision A, dated December 17, 2012.
(ii) Bombardier Service Bulletin 8-32-176, Revision A, dated February 22, 2013.
(iii) Bombardier Service Bulletin 8-32-177, dated October 9, 2013.
(iv) Bombardier Service Bulletin 8-33-56, Revision A, dated February 22, 2013.
FAA Air Transport Association (ATA) of America Code 05, Periodic Inspections
This AD applies to all Airbus Model A318-111, -112, -121, and -122 airplanes; Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes; Model A320-111, -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.
FAA AD AD 2014-23-15
EASA AD 2012-0008 and EASA AD 2013-0147

(3) The following service information was approved for IBR on March 2, 2015 (80 FR 3871, January 26, 2015).
(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) Airbus A318/A319/A320/A321 ALS Part 2-Damage-Tolerant Airworthiness Limitation Items (DT ALI), Revision 02, dated May 28, 2013. The revision date of this document is not identified on the title page of this document.
(4) The following service information was approved for IBR on August 22, 2011 (76 FR 42024, July 18, 2011).
(i) Airbus A318/A319/A320/A321 Airworthiness Limitation Items, Document AI/SE-M4/95A.0252/96, Issue 10, dated October 2009. The revision level of this document is identified on only the title page and in the Record of Revisions.
(ii) Airbus A318/A319/A320/A321 Airworthiness Limitation Items, Document AI/SE-M4/95A.0252/96, Issue 11, dated September 2010. The revision level of this document is identified on only the title page and in the Record of Revisions.
(5) The following service information was approved for IBR on November 7, 2007 (72 FR 56262, October 3, 2007).
(i) Airbus A318/A319/A320/A321 ALS Part 1-Safe Life Airworthiness Limitation Items, Revision 00, dated February 28, 2006.
(ii) Airbus A318/A319/A320/A321 Airworthiness Limitation Items, Document AI/SE-M4/95A.0252/96, Issue 7, dated December 2005.
Note 2 to paragraph (r)(5)(ii) of this AD: This document contains the following errors: The Summary of Changes is comprised of 11 pages, which are all identified as Page 2-LEP of Section LEP instead of Page 1-SOC [through] Page 11-SOC of Section SOC; the List of Effective Pages only refers to Page 1-SOC for the Summary of Changes. The List of Effective Pages is comprised of two pages, and both of those pages are identified as Page 2-LEP. The first page of Section 2 is identified as Page 6 of Section 1 and is not referred to in the List of Effective Pages.
(iii) Airbus A318/A319/A320/A321 Airworthiness Limitation Items, Document AI/SE-M4/95A.0252/96, Issue 08, dated March 2006.
Note 3 to paragraph (r)(5)(iii) of this AD: This document contains the following errors: Pages 3-ROR and 2-SOC are not referred to in the List of Effective Pages. The List of Effective Pages is identified as Pages 1-SOC and 2-SOC, instead of 1-LEP and 2-LEP. The first page of Section 2 is identified as Page 6 of Section 1 and is not referred to in the List of Effective Pages.
(iv) Airbus A318/A319/A320/A321 Airworthiness Limitation Items, Document AI/SE-M4/95A.0252/96, Issue 09, dated November 2006.
FAA Air Transport Association (ATA) of America Code 34, Navigation
This AD applies to Dassault Aviation Model FALCON 7X airplanes, certificated in any category, all serial numbers
FAA AD 2011-13-07
EASA AD 2009-0208R3

(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Procedure 3-140-70A, "Avionics-Sensor miscompare (A/C with M566)," Issue 2, of Section 3-Abnormal Procedures, of the Dassault Falcon 7X Airplane Flight Manual, DGT 105608, Revision 15, dated January 30, 2012.
(ii) Procedure 3-140-70A, "Avionics-Sensor miscompare," Issue 4, of Section 3-Abnormal Procedures, of the Dassault Falcon 7X Airplane Flight Manual, DGT105608, Revision 18, dated November 15, 2013.
FAA Air Transport Association (ATA) of America Code 53, Fuselage
This AD applies to the Airbus airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category.
(1) Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes, all manufacturer serial numbers.
(2) 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; all manufacturer serial numbers, except those on which Airbus Modification 12699 has been embodied in production.
(3) Model A310-203, -204, -221, -222, -304, -322, -324, and -325 airplanes, all manufacturer serial numbers.
N/A
EASA AD 2013-0220
FAA Air Transport Association (ATA) of America Code 24, Electrical Power
This AD applies to BAE Systems (Operations) Limited Model 4101 airplanes, certificated in any category, all serial numbers
N/A
EASA AD 2014-0006

(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 J41-24-043, Revision 3, dated June 16, 2014.
(ii) Reserved.
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 Special Attention Service Bulletin 737-53-1083, Revision 5, dated July 22, 2014.
(2) Installation of Supplemental Type Certificate (STC) ST01219SE does not affect the ability to accomplish the actions required by this AD. For airplanes on which STC ST01219SE is installed, therefore, 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 Special Attention Service Bulletin 737-53-1083, Revision 5, dated July 22, 2014.
(ii) Reserved.
FAA No subject
This AD applies to all Rolls-Royce plc (RR) RB211-524B-02, RB211-524B-B-02, RB211-524B2-19, RB211-524B2-B-19, RB211-524B3-02, RB211-524C2-19, and RB211-524C2-B-19 turbofan engines with low-pressure turbine (LPT) stage 3 turbine blade, part number (P/N) LK55386, LK86483, or LK86503, installed
N/A
EASA AD 2014-0210

None
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