FAA Biweeky AD Report 2015-03

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FAA AD 2014-23-15 - 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.
Supersedes/Replaces: FAA AD 2011-14-06
Relates to: EASA AD 2012-0008
Material Incorporated by Reference
(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) 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.
(iii) Airbus A318/A319/A320/A321 ALS Part 4-Ageing Systems Maintenance, dated January 8, 2008. The revision date of this document is not identified on the title page of this document.
(3) 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.
(4) 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 (approved by the European Aviation Safety Agency (EASA) on February 7, 2006).
Note 2 to paragraph (r)(4)(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 (approved by the EASA on January 4, 2007).
(iv) Airbus A318/A319/A320/A321 Airworthiness Limitation Items, Document AI/SE-M4/95A.0252/96, Issue 09, dated November 2006 (approved by the EASA on May 21, 2007).
FAA AD 2014-26-08 - Air Transport Association (ATA) of America Code 05, Periodic inspections.
This AD applies to all Airbus Model A330-201, -202, -203, -223, -223F -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes, certificated in any category, all manufacturer serial numbers.
Supersedes/Replaces: FAA AD 2011-13-09
Relates to: EASA AD 2013-0245
Material Incorporated by Reference
(3) The following service information was approved for IBR on March 2, 2015.
(i) Airbus A330 Airworthiness Limitations Section ALS Part 3-
Certification Maintenance Requirements, Revision 04, dated August 27, 2013. 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.
(4) The following service information was approved for IBR on August 1, 2011 (76 FR 37255, June 27, 2011).
(i) Airbus A330 ALS Part 3-Certification Maintenance Requirements, Revision 03, dated July 29, 2010. 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 AD 2015-02-02 - Air Transport Association (ATA) of America Code 27, Flight Controls
This AD applies to the Bombardier, Inc. airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Model CL-215-6B11 (CL-215T Variant) airplanes, serial numbers 1056 through 1125 inclusive.
(2) Model CL-215-6B11 (CL-415 Variant) airplanes, serial numbers 2001 through 2990 inclusive.
Supersedes/Replaces: N/A
Relates to: TC AD CF-2013-08
Material Incorporated by Reference
(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Alert Service Bulletin 215-A3171, Revision 1, dated January 25, 2012.
(ii) Bombardier Alert Service Bulletin 215-A4452, Revision 1, dated January 3, 2012.
FAA AD 2015-02-03 - Air Transport Association (ATA) of America Code 54, Nacelles/Pylons
This AD applies to Airbus Model A300 B4-601, B4-603, B4-605R, F4-605R, and C4-605R Variant F airplanes, certificated in any category, all manufacturer serial numbers, except those on which Airbus Modification 11110 has been embodied in production, or that have been modified in service as specified in Airbus Service Bulletin A300-54-6031, dated May 30, 1996.
Supersedes/Replaces: N/A
Relates to: EASA AD 2013-0286R1
Material Incorporated by Reference
(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 A300-54-6031, dated May 30, 1996.
(ii) Airbus Service Bulletin A300-54-6034, Revision 02, dated August 26, 2013.
FAA AD 2015-02-04 CORRECTED - Air Transport Association (ATA) of America Code 24, Electrical Power
This AD applies to Dassault Aviation Model MYSTERE-FALCON 50 airplanes, certificated in any category, as identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Airplanes with manufacturer serial numbers 5, 7, 27, 30, 34, 36, 78, 132, and 251 through 352 inclusive.
(2) Airplanes with manufacturer serial numbers 2 through 250 inclusive, having Honeywell (formerly Allied Signal, Garrett AiResearch) TFE731-40-1C engines modified by Dassault Aviation Service Bulletin F50-280.
Supersedes/Replaces: N/A
Relates to: EASA AD 2014-0024
Material Incorporated by Reference
(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Dassault Service Bulletin F50-530, dated November 12, 2013.
(ii) Reserved.
FAA AD 2015-02-05 - Air Transport Association (ATA) of America Code 34, Navigation
This AD applies to all The Boeing Company airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category.
(1) The Boeing Company Model 717-200 airplanes.
(2) The Boeing Company Model DC-10-10, DC-10-10F, DC-10-15, DC-10-30, DC-10-30F (KC-10A and KDC-10), DC-10-40, and DC-10-40F airplanes; and Model MD-10-10F and MD-10-30F airplanes.
(3) The Boeing Company Model DC-9-81 (MD-81), DC-9-82 (MD-82), DC-9-83 (MD-83), and DC-9-87 (MD-87) airplanes; Model MD-88 airplanes; and Model MD-90-30 airplanes
Supersedes/Replaces: N/A
Relates to: N/A
Material Incorporated by Reference
(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Special Compliance Item (SCI) 34-4, "Functional Test of the Captain and First Officer's Altimeter," of Appendix A "SCIs," to Boeing Report No. MDC-02K1003, "Trijet Special Compliance Item Report," Revision K, dated February 1, 2013. There is no page "i" identified in this document.
(ii) Special Compliance Item (SCI) 34-1, "Functional Test of the Captain and First Officer's Altimeter," of Appendix A "SCIs," to Boeing Report No. MDC-92K9145, "Twinjet Special Compliance Item Report", Revision M, dated February 5, 2013
FAA AD 2015-02-06 CORRECTED - Air Transport Association (ATA) of America Code 27, Flight Controls.
This AD applies to Bombardier, Inc. Model CL-600-2B16 (CL-604 Variant) airplanes, certificated in any category, serial numbers 5301 and subsequent, equipped with horizontal stabilizer trim actuator (HSTA) part number (P/N) 604-92305-3 (vendor P/N 8454-1) or P/N 604-92305-5 (vendor P/N 8454-2).
Supersedes/Replaces: N/A
Relates to: TC AD CF-2013-18
Material Incorporated by Reference
(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 604-27-032, Revision 02, dated April 22, 2014.
(ii) Bombardier Service Bulletin 605-27-002, Revision 02, dated April 22, 2014.
(iii) Bombardier Temporary Revision 604/37, dated May 21, 2013, to the Bombardier Challenger CL-604 Airplane Flight Manual, PSP 604-1.
(iv) Bombardier Temporary Revision 605/18, dated May 21, 2013, to the Bombardier Challenger CL-605 Airplane Flight Manual, PSP 605-1.
FAA AD 2015-02-08
This AD applies to all Rolls-Royce Corporation (RRC) AE 2100D2, 2100D2A, 2100D3, and 2100P turboprop engines and AE 3007A1, A1/1, A1/3, A1E, A1P, A2, A3, C, C1, and C2 turbofan engines:
(1) With an installed 1st stage gas generator turbine wheel, part number (P/N) 23079946, 23088906, or 23089692, all serial numbers (S/Ns) listed in Table 2 and Table 3 of RRC Alert Service Bulletin (ASB) No. AE 2100D2-A-72-085, dated July 25, 2013; and in Table 2 and Table 3 of RRC ASB No. AE 2100D3-A-72-277, dated July 25, 2013.
(2) With an installed high-pressure turbine (HPT) stage 1 or HPT stage 2 wheel, P/N 23079946, 23088906, 23088784, 23084520, 23084781, 23088817, or 23088818, all S/Ns listed in Table 1 through Table 7 of RRC ASB No. AE 3007A-A-72-407, Revision 1, dated August 29, 2014, except those S/Ns excluded by Table 1, Table 2, Table 4, and Table 5 of RRC ASB No. AE 3007A-A-72-407, Revision 1, dated August 29, 2014.
(3) With an installed HPT stage 2 wheel, P/N 23084520 or 23088818, all S/Ns listed in Table 1 and Table 2 of RRC ASB No. AE 3007C-A-72-316, dated December 6, 2013, except those S/Ns excluded by Table 1 of RRC ASB No. AE 3007C-A-72-316, dated December 6, 2013.
(4) With an installed 4th stage turbine wheel, P/N 23083536, all S/Ns listed in Table 2 of RRC ASB No. AE 2100P-A-72-019, dated July 25, 2013.
Supersedes/Replaces: N/A
Relates to: N/A
Material Incorporated by Reference
(2) You must use this service information as applicable to do the actions required by this AD, unless the AD specifies otherwise.
(i) Rolls-Royce Alert Service Bulletin (ASB) No. AE 2100D2-A-72-085, dated July 25, 2013.
(ii) Rolls-Royce ASB No. AE 2100D3-A-72-277, dated July 25, 2013.
(iii) Rolls-Royce ASB No. AE 2100P-A-72-019, dated July 25, 2013.
(iv) Rolls-Royce ASB No. AE 3007A-A-72-407, Revision 1, dated August 29, 2014.
(v) Rolls-Royce ASB No. AE 3007A-A-72-408, Revision 1, dated August 29, 2014.
(vi) Rolls-Royce ASB No. AE 3007C-A-72-316, dated December 6, 2013.
FAA AD 2015-02-11 - Air Transport Association (ATA) of America Code 55, Stabilizers
This AD applies to Airbus Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes; and Model A340-211, -212, -213, -311, -312, and -313 airplanes; certificated in any category; except airplanes on which Airbus Modification 41800 has been embodied in production.
Supersedes/Replaces: N/A
Relates to: EASA AD 2013-0270R1
Material Incorporated by Reference
(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 A55L001-12, dated December 20, 2012, including Inspection Flow Chart AOpT ref.: A55L001-12, not dated. The document number and date of this document are identified on only the first page of this AOT.
(ii) Reserved.
FAA AD 2015-02-12 - Air Transport Association (ATA) of America Code 32; Main Landing Gear
This AD applies to Bombardier, Inc. Model DHC-8-400, -401 and -402 airplanes, certificated in any category, serial numbers 4001 through 4454 inclusive.
Supersedes/Replaces: N/A
Relates to: TC AD CF-2013-19
Material Incorporated by Reference
(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 84-32-121, dated May 27, 2013.
(ii) Reserved.
FAA AD 2015-02-13 - Transport Association (ATA) of America Code 54, Nacelles/pylons; 53, Fuselage
This AD applies to Empresa Brasileira de Aeronautica S.A. (Embraer) Model EMB -135ER, -135KE, -135KL, -135LR, -145, -145ER, -145MR, -145LR, -145XR, -145MP, and -145EP airplanes, certificated in any category, all serial numbers.
Supersedes/Replaces: N/A
Relates to: ANAC AD BR-2014-01-01
Material Incorporated by Reference
(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) EMBRAER EMB145 Temporary Revision 15-3, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER EMB145 Maintenance Review Board Report MRB 145/1150.
(ii) EMBRAER EMB145 Temporary Revision 15-4, dated August 26, 2013, to the Airworthiness Limitation Requirements of the EMBRAER EMB145 Maintenance Review Board Report MRB-145/1150.
FAA AD 2015-02-16 - Air Transport Association (ATA) of America Code 27, Flight Controls; Code 32, Landing Gear
This AD applies to 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; Model A300 F4-605R and F4-622R airplanes, and Model A300 C4-605R Variant F airplanes; certificated in any category; all manufacturer serial numbers.
Supersedes/Replaces: FAA AD 2009-06-06
Relates to: EASA AD 2013-0075
Material Incorporated by Reference
(3) The following service information was approved for IBR on March 6, 2015.
(i) Airbus A300-600 ALS Part 4-Ageing Systems Maintenance, Revision 02, dated April 18, 2012.
(ii) Airbus A300-600 Variation 0CVLG120001/C0S, dated August 24, 2012, to Airbus A300-600 ALS Part 4-Ageing Systems Maintenance, Revision 02, dated April 18, 2012.
(iii) Airbus A310 ALS Part 4-Ageing Systems Maintenance, Revision 02, dated November 30, 2012.
(4) The following service information was approved for IBR on April 28, 2009 (74 FR 12228, March 24, 2009).
(i) Airbus A300-600 ALS Part 4-Ageing Systems Maintenance, Revision 01, dated December 21, 2006.
(ii) Airbus A310 ALS Part 4-Ageing Systems Maintenance, Revision 01, dated December 21, 2006.
FAA AD 2015-02-17 - Air Transport Association (ATA) of America Code 24, Electrical Power
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Airbus Model A330-201, -202, -203, -223, -223F, -243, and -243F airplanes.
(2) Airbus Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
Supersedes/Replaces: N/A
Relates to: EASA AD 2014-0281
Material Incorporated by Reference
(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Airbus A330/A340 Airplane Flight Manual (AFM) Temporary Revision TR427, UPDATE OF ELEC-EMER CONFIG PROCEDURE, Issue 1.0, dated November 7, 2014.
(ii) Airbus A330/A340 AFM Temporary Revision TR428, UPDATE OF ELEC-EMER CONFIG PROCEDURE, Issue 1.0, dated November 7, 2014.
FAA AD 2015-02-18 - Air Transport Association (ATA) of America Code 71, Powerplant
This AD applies to Airbus Model A330-201, -202, -203, -301, -302, and -303 airplanes, certificated in any category, all manufacturer serial numbers
Supersedes/Replaces: N/A
Relates to: EASA AD 2013-0094
Material Incorporated by Reference
(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 A71L002-13, dated April 8, 2013.
(ii) Reserved.
FAA AD 2015-02-19 - Air Transport Association (ATA) of America Code 57, Wings
This AD applies to the Airbus airplanes specified in paragraphs (c)(1) through (c)(5) of this AD, certificated in any category, all manufacturer serial numbers.
(1) Model A300 B2-1A, B2-1C, B2K-3C, B2-203, B4-2C, B4-103, and B4-203 airplanes.
(2) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes.
(3) Model A300 B4-605R and B4-622R airplanes.
(4) Model A300 F4-605R airplanes.
(5) Model A300 C4-605R Variant F airplanes.
Supersedes/Replaces: FAA AD 95-24-04
Relates to: EASA AD 2013-0013R1
Material Incorporated by Reference
(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(3) The following service information was approved for IBR on effective March 11, 2015.
(i) Airbus Service Bulletin A300-57-6059, Revision 04, dated February 22, 2011.
(ii) Reserved.
(4) The following service information was approved for IBR on December 27, 1995 (60 FR 58213, November 27, 1995).
(i) Airbus Service Bulletin A300-57-0213, dated August 12, 1994.
(ii) Airbus Service Bulletin A300-57-6059, dated August 12, 1994.
FAA AD 2015-02-20
This AD applies to all Rolls-Royce plc (RR) RB211-Trent 553-61, 553A2-61, 556-61, 556A2-61, 556B-61, 556B2-61, 560-61, 560A2-61, 768-60, 772-60, 772B-60, 875-17, 877-17, 884-17, 884B-17, 892-17, 892B-17, 895-17, 970-84, 970B-84, 972-84, 972B-84, 977-84, 977B-84, and 980-84 turbofan engines.
Supersedes/Replaces: FAA AD 2013-15-10
Relates to: EASA AD 2014-0152
Material Incorporated by Reference
(3) The following service information was approved for IBR on March 11, 2015.
(i) Rolls-Royce plc (RR) Non-Modification Service Bulletin (NMSB) No. RB.211-72-G448, Revision 4, dated August 21, 2014.
(ii) RR Alert NMSB No. RB.211-72-AH058, Revision 1, dated July 7, 2014.
(4) The following service information was approved for IBR on October 8, 2013 (78 FR 54149, September 3, 2013).
(i) RR Alert NMSB No. RB.211-72-AH059, dated December 11, 2012.
(ii) Reserved.
(5) The following service information was approved for IBR on June 29, 2012, (77 FR 31176, May 25, 2012).
(i) RR Alert NMSB No. RB.211-72-AG270, Revision 4, dated March 21, 2011.
(ii) RR Alert NMSB No. RB.211-72-AG085, Revision 2, dated July 7, 2011.
(iii) RR Alert NMSB No. RB.211-72-AG264, Revision 5, dated March 21, 2011.
FAA AD 2015-02-23 - Air Transport Association (ATA) of America Code 57, Wings
This AD applies to the Bombardier, Inc. airplanes identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD, certificated in any category.
(1) Bombardier, Inc. Model CL-600-1A11 (CL-600) airplanes, having serial numbers (S/Ns) 1004 through 1085 inclusive.
(2) Bombardier, Inc. Model CL-600-2A12 (CL-601) airplanes, having S/Ns 3001 through 3066 inclusive.
(3) Bombardier, Inc. Model CL-600-2B16 (CL-601-3A and CL-601-3R Variants) airplanes, having S/Ns 5001 through 5194 inclusive.
Supersedes/Replaces: N/A
Relates to: FAA AD 2014-03-17 and TC CF-2013-39R2
Material Incorporated by Reference
service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Alert Service Bulletin A600-0763, Revision 02, dated December 9, 2014, including Appendices 1 and 2, dated September 26, 2013.
(ii) Bombardier Alert Service Bulletin A601-0627, Revision 02, dated December 9, 2014, including Appendices 1 and 2, dated September 26, 2013.
FAA AD 2015-02-26 - Air Transport Association (ATA) of America Code 53, Fuselage
This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD, certificated in any category.
(1) The Boeing Company Model 737-100, -200, -200C, -300,-400, and -500 series airplanes, as identified in Boeing Special Attention Service Bulletin 737-53-1260, Revision 1, dated May 23, 2013.
(2) The Boeing Company Model 737-600, -700, -700C, -800, and -900 series airplanes, as identified in Boeing Service Bulletin 737-53-1244, Revision 5, dated July 27, 2011.
Supersedes/Replaces: FAA AD 2013-24-13
Relates to: N/A
Material Incorporated by Reference
(3) The following service information was approved for IBR on January 7, 2014 (78 FR 72558, December 3, 2013).
(i) Boeing Service Bulletin 737-53-1120, Revision 1, dated May 13, 1993.
(ii) Boeing Service Bulletin 737-53-1244, Revision 5, dated July 27, 2011.
(iii) Boeing Special Attention Service Bulletin 737-53-1260, Revision 1, dated May 23, 2013.
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