Adoption of the Amendment
Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0 1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD):
2016-03-07 Airbus: Amendment 39-18394. Docket No. FAA-2015-3149; Directorate Identifier 2015-NM-014-AD.
(a) Effective Date
This AD becomes effective April 13, 2016.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1) and (c)(2) of this AD, all manufacturer serial numbers; except those on which a gaseous system for all oxygen generators is installed.
(1) Airbus Model A330-201, -202, -203, -223, -223F, -243, -243F, -301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes.
(2) Airbus Model A340-211, -212, -213, -311, -312, -313, -541, and -642 airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Reason
This AD was prompted by reports of premature aging of certain chemical oxygen
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generators in the passenger compartment that resulted in failure of the generators to activate. We are issuing this AD to prevent failure of the chemical oxygen generator to activate during an emergency situation, which could result in unavailability of oxygen and possible incapacitation of the occupants.
(f) Compliance
Comply with this AD within the compliance times specified, unless already done.
(g) Inspection
Within 30 days after the effective date of this AD: Inspect each passenger chemical oxygen generator to identify the date of manufacture (refer to figures 1 and 2 to paragraph (g) of this AD for the location of the date) of each passenger chemical oxygen generator having any part number (P/N) listed in paragraphs (g)(1) through (g)(6) of this AD, in accordance with the Instructions of Airbus Alert Operators Transmission (AOT) A35L007-14, Revision 01, June 17, 2015, including Appendix A, Revision 01, dated June 17, 2015. A review of airplane maintenance records is acceptable in lieu of this inspection if the date of manufacture of the generator can be conclusively determined from that review.
(1) 117042-02 (15 minutes (min)--2 masks).
(2) 117042-03 (15 min--3 masks).
(3) 117042-04 (15 min--4 masks).
(4) 117042-22 (22 min--2 masks).
(5) 117042-23 (22 min--3 masks).
(6) 117042-24 (22 min--4 masks).
[GRAPHIC] [TIFF OMITTED] TR09MR16.000
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[GRAPHIC] [TIFF OMITTED] TR09MR16.001
(h) Replacement of Pre-2002 Passenger Oxygen Generators
If, during any inspection required by paragraph (g) of this AD, any passenger chemical oxygen generator having a date of manufacture of 1999, 2000, or 2001 is found: At the time specified in paragraph (h)(1), (h)(2), or (h)(3) of this AD, as applicable, replace the affected passenger chemical oxygen generator, in accordance with the Instructions of Airbus AOT A35L007-14, Revision 01, June 17, 2015; including Appendix A, Revision 01, dated June 17, 2015 (for 15- and 22-minute passenger chemical oxygen generators); or in accordance with the Accomplishment Instructions of B/E Aerospace Service Bulletin 117042-35-001, dated December 10, 2014 (for 15-minute passenger chemical oxygen generators).
(1) For units manufactured in 1999: Within 30 days after the effective date of this AD.
(2) For units manufactured in 2000: Within 6 months after the effective date of this AD.
(3) For units manufactured in 2001: Within 12 months after the effective date of this AD.
(i) Replacement of 2002 or Later Passenger Oxygen Generators
If, during any inspection required by paragraph (g) of this AD, any passenger chemical oxygen generator having a date of manufacture of 2002 or later is found: At the time specified in paragraph (i)(1), (i)(2), (i)(3), (i)(4), (i)(5), (i)(6), (i)(7), or (i)(8) of this AD, as applicable, replace the affected passenger chemical oxygen generator with a serviceable unit, in accordance with the Instructions of Airbus AOT A35L007-14, Revision 01, June 17, 2015; including Appendix A, Revision 01, dated June 17, 2015 (for 15- and 22-minute passenger chemical oxygen generators); or in accordance with the Accomplishment Instructions of B/E Aerospace Service Bulletin 117042-35-001, dated December 10, 2014 (for 15-minute passenger chemical oxygen generators).
(1) For units manufactured in 2002: Within 12 months after the effective date of this AD.
(2) For units manufactured in 2003: Within 16 months after the effective date of this AD.
(3) For units manufactured in 2004: Within 20 months after the effective date of this AD.
(4) For units manufactured in 2005: Within 24 months after the effective date of this AD.
(5) For units manufactured in 2006: Within 28 months after the effective date of this AD.
(6) For units manufactured in 2007: Within 32 months after the effective date of this AD.
(7) For units manufactured in 2008: Within 36 months after the effective date of this AD.
(8) For units manufactured in 2009 or later: Before the accumulation of 10 years since date of manufacture.
(j) Definition of a Serviceable Unit
A serviceable unit is an oxygen generator having P/N 117042-XX, with a manufacturing date not older than 10 years, or any other FAA- approved part number, provided that the generator has not exceeded
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the life limit established by the manufacturer for that generator.
(k) Credit for Previous Actions
This paragraph provides credit for the applicable actions required by paragraphs (g), (h), and (i) of this AD, if those actions were performed before the effective date of this AD using Airbus AOT A35L007-14, dated December 18, 2014.
(l) Parts Installation Limitation
As of the effective date of this AD, no person may install a passenger chemical oxygen generator on any airplane, unless the passenger chemical oxygen generator is determined to be a serviceable unit, as defined in paragraph (j) of this AD.
(m) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Branch, send it to ATTN: Vladimir Ulyanov, Aerospace Engineer, International Branch, ANM-116, Transport Airplane Directorate, FAA, 1601 Lind Avenue SW., Renton, WA 98057-3356; telephone 425-227-1138; fax 425-227-1149. Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. The AMOC approval letter must specifically reference this AD.
(2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA; or the European Aviation Safety Agency (EASA); or Airbus's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.
(n) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2015-0119, dated June24, 2015, correction January 12, 2016, for related information. This MCAI may be found in the AD docket on the Internet at http://www.regulations.gov by searching for and locating Docket No. FAA- 2015-3149.
(2) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (o)(3) and (o)(5) of this AD.
(o) Material Incorporated by Reference
(1) The Director of the Federal Register approved the incorporation by reference (IBR) of the 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) Airbus Alert Operators Transmission (AOT) A35L007-14, Revision 01, June 17, 2015; including Appendix A, Revision 01, dated June 17, 2015. The revision date is not shown on Appendix A.
(ii) B/E Aerospace Service Bulletin 117042-35-001, dated December 10, 2014.
(3) For Airbus service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email airworthiness.A330-A340@airbus.com; Internet http://www.airbus.com.
(4) For B/E Aerospace service information identified in this AD, contact B/E Aerospace Inc., 10800 Pflumm Road, Lenexa, KS 66215; telephone 913-338-9800; fax 913-469-8419; Internet http://beaerospace.com/home/globalsupport.
(5) You may view this service information at the FAA, Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221.
(6) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html.