AD 2011-18-20
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus SAS | A330-201 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-202 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-203 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-223 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-243 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-301 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-302 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-303 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-321 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-322 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-323 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-341 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-342 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A330-343 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A340-211 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A340-212 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A340-213 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A340-311 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A340-312 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
| aircraft | Airbus SAS | A340-313 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-200 and -300 Series Airplanes |
Unsafe Condition
The distance between wire harnesses 5376VB/2M and 5377VB/1M above doors 4 and the air conditioning duct is too small, potentially causing collision with the flexible air conditioning hose. This could lead to short circuit of oxygen-dedicated wires, resulting in passenger oxygen masks not being supplied with oxygen during emergencies.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Within 24 months after the effective date, modify the wire harness 5376VB/2M and 5377VB/1M attachments above doors 4, in accordance with Airbus Mandatory Service Bulletin A330-92-30.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 24 months after the effective date of this AD
AI-generated summary from the source AD text. Verify against the official source before acting.
Affected Aircraft
Airbus Model A330-200 and -300 Series airplanes (types A330-201, -202, -203, -223, -243, -301, -302, -303, -321, -322, -323, -341, -342, -343) and Model A340-200 and -300 Series airplanes (types A340-211, -212, -213, -311, -312, -313), all serial numbers, except those with modifications 57349 and 58924, or 201642, or 57562.
AI-generated summary from the source AD text. Verify against the official source before acting.
Federal Register Abstract
We are adopting a new airworthiness directive (AD) for the products listed above. This AD results from mandatory continuing airworthiness information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe condition on an aviation product. The MCAI describes the unsafe condition as:
Document Text
Show stored source text (verify against official source)
[Federal Register Volume 76, Number 177 (Tuesday, September 13, 2011)]
[Rules and Regulations]
[Pages 56284-56286]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2011-22380]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-0474; Directorate Identifier 2010-NM-213-AD;
Amendment 39-16802; AD 2011-18-20]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A330-200 and -300 Series
Airplanes, and Model A340-200 and -300 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for the
products listed above. This AD results from mandatory continuing
airworthiness information (MCAI) originated by an aviation authority of
another country to identify and correct an unsafe condition on an
aviation product. The MCAI describes the unsafe condition as:
It was noticed in production that the distance between the wire
harnesses 5376VB/2M and 5377VB/1M which are above the left-hand (LH)
and right-hand (RH) door 4, and the air conditioning duct could be
too small. This could result in collision between the flexible air
conditioning hose and wire harnesses.
This condition, if not corrected, could lead to the short
circuit of wires dedicated to oxygen, which, in case of emergency,
could result in a large number of passenger oxygen masks not being
supplied with oxygen, possibly causing personal injuries.
* * * * *
We are issuing this AD to require actions to correct the unsafe
condition on these products.
DATES: This AD becomes effective October 18, 2011.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of October 18,
2011.
ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer,
International Branch, ANM-116, Transport Airplane Directorate, FAA,
1601 Lind Avenue, SW., Renton, Washington 98057-3356; telephone (425)
227-1138; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 to include an AD that would apply to the specified products.
That NPRM was published in the Federal Register on May 23, 2011 (76 FR
29673). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
It was noticed in production that the distance between the wire
harnesses 5376VB/2M and 5377VB/1M which are above the left-hand (LH)
and right-hand (RH) door 4, and the air conditioning duct could be
too small. This could result in collision between the flexible air
conditioning hose and wire harnesses.
[[Page 56285]]
This condition, if not corrected, could lead to the short
circuit of wires dedicated to oxygen, which, in case of emergency,
could result in a large number of passenger oxygen masks not being
supplied with oxygen, possibly causing personal injuries.
For the reasons described above, this [EASA] AD requires the
installation of a protective sleeve and an additional bracket to
maintain the appropriate distance between wires.
Revision 1 of this [EASA] AD is issued to revise the
applicability section of this AD in order to take into account all
configurations of air conditioning duct and the associated solutions
embodied in production.
For certain airplanes, required actions include modifying the support
assembly of the air outlet. For other airplanes, required actions
include exchanging certain attachment screws of the air outlet box
assembly on each door. You may obtain further information by examining
the MCAI in the AD docket.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comment received.
Request To Clarify Applicability
Delta Air Lines (Delta) asked that the applicability in the NPRM
(76 FR 29673, May 23, 2011) be changed for clarification. Delta stated
that its interpretation of paragraph (c)(3) of the applicability is
that airplanes are exempt from the NPRM if Airbus Modification 201642
is embodied in production, or if Airbus Modification 57562 is embodied
in production, or if both Airbus Modifications 57349 and 58924 are
embodied in production. Delta noted that this interpretation does not
align with the applicability in the EASA AD, which was issued to revise
the applicability paragraph to take into account all configurations of
the air conditioning duct and associated solutions embodied in
production. Delta asked that paragraph (c) of the NPRM be changed to
eliminate the possibility of incorrect interpretation, and included
language for the clarification.
We agree for the reasons provided by the commenter. We have revised
the format and punctuation of paragraph (c) of this AD for clarity.
Conclusion
We reviewed the available data, including the comment received, and
determined that air safety and the public interest require adopting the
AD with the change described previously. We determined that this change
will not increase the economic burden on any operator or increase the
scope of the AD.
Differences Between This AD and the MCAI or Service Information
We have reviewed the MCAI and related service information and, in
general, agree with their substance. But we might have found it
necessary to use different words from those in the MCAI to ensure the
AD is clear for U.S. operators and is enforceable. In making these
changes, we do not intend to differ substantively from the information
provided in the MCAI and related service information.
We might also have required different actions in this AD from those
in the MCAI in order to follow our FAA policies. Any such differences
are highlighted in a Note within the AD.
Costs of Compliance
We estimate that this AD affects about 41 products of U.S.
registry. We also estimate that it will take up to 11 work-hours per
product to comply with the basic requirements of this AD. The average
labor rate is $85 per work-hour. Required parts will cost up to $503
per product. Where the service information lists required parts costs
that are covered under warranty, we have assumed that there will be no
charge for these costs. As we do not control warranty coverage for
affected parties, some parties may incur costs higher than estimated
here. Based on these figures, we estimate the cost of the AD on U.S.
operators to be up to $58,958, or up to $1,438 per product.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify this AD:
1. Is not a ''significant regulatory action'' under Executive Order
12866;
2. Is not a ''significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a>; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM (76 FR 29673, May 23, 2011),
the regulatory evaluation, any comments received, and other
information. The street address for the Docket Operations office
(telephone (800) 647-5527) is in the ADDRESSES section. Comments will
be available in the AD docket shortly after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
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 AD:
2011-18-20 Airbus: Amendment 39-16802. Docket No. FAA-2011-0474;
Directorate Identifier 2010-NM-213-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective October
18, 2011.
Affected ADs
(b) None.
[[Page 56286]]
Applicability
(c) This AD applies to Airbus Model A330-201, -202, -203, -223,
-243, -301, -302, -303, -321, -322, -323, -341, -342, and -343
airplanes; and Model A340-211, -212, -213, -311, -312, and -313
airplanes, all manufacturer serial numbers; certificated in any
category; except those airplanes embodied in production with the
modifications identified in paragraphs (c)(1) and (c)(2) of this AD.
(1) Modification 57349 and
(2) Modification 58924 or 201642 or 57562.
Subject
(d) Air Transport Association (ATA) of America Code 92.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
It was noticed in production that the distance between the wire
harnesses 5376VB/2M and 5377VB/1M which are above the left-hand (LH)
and right-hand (RH) door 4, and the air conditioning duct could be
too small. This could result in collision between the flexible air
conditioning hose and wire harnesses.
This condition, if not corrected, could lead to the short
circuit of wires dedicated to oxygen, which, in case of emergency,
could result in a large number of passenger oxygen masks not being
supplied with oxygen, possibly causing personal injuries.
* * * * *
Compliance
(f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Actions
(g) Within 24 months after the effective date of this AD: Modify
the wire harness 5376VB/2M and 5377VB/1M attachments above the LH
and RH door 4, in accordance with the Accomplishment Instructions of
Airbus Mandatory Service Bulletin A330-92-3077, Revision 01, dated
March 29, 2010; or Airbus Mandatory Service Bulletin A340-92-4078,
Revision 01, dated April 9, 2010; as applicable.
(h) For airplanes that have been modified before the effective
date of this AD in accordance with the Accomplishment Instructions
of Airbus Mandatory Service Bulletin A330-92-3077 or A340-92-4078,
both dated June 17, 2008: Within 24 months after the effective date
of this AD, perform the additional work identified in Airbus
Mandatory Service Bulletin A330-92-3077, Revision 01, dated March
29, 2010, or A340-92-4078, Revision 01, dated April 9, 2010; as
applicable (including modifying the support assembly of the air
outlet, or exchanging certain attachment screws of the air outlet
box assembly on each door, as applicable), in accordance with the
Accomplishment Instructions of Airbus Mandatory Service Bulletin
A330-92-3077, Revision 01, dated March 29, 2010; or Airbus Mandatory
Service Bulletin A340-92-4078, Revision 01, dated April 9, 2010; as
applicable.
FAA AD Differences
Note 1: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(i) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, ANM-116, 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, Washington 98057-3356; telephone (425)
227-1138; fax (425) 227-1149. Information may be e-mailed to: <a href="/cdn-cgi/l/email-protection#6851452926254559595e452925272b453a2d393d2d3b3c3b280e0909460f071e"><span class="__cf_email__" data-cfemail="bc8591fdf2f1918d8d8a91fdf1f3ff91eef9ede9f9efe8effcdadddd92dbd3ca">[email protected]</span></a>. 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) Airworthy Product: For any requirement in this AD to obtain
corrective actions from a manufacturer or other source, use these
actions if they are FAA-approved. Corrective actions are considered
FAA-approved if they are approved by the State of Design Authority
(or their delegated agent). You are required to assure the product
is airworthy before it is returned to service.
Related Information
(j) Refer to MCAI European Aviation Safety Agency Airworthiness
Directive 2010-0103R1, dated April 28, 2011; Airbus Mandatory
Service Bulletin A330-92-3077, Revision 01, dated March 29, 2010;
and Airbus Mandatory Service Bulletin A340-92-4078, Revision 01,
dated April 9, 2010; for related information.
Material Incorporated by Reference
(k) You must use Airbus Mandatory Service Bulletin A330-92-3077,
Revision 01, dated March 29, 2010; or Airbus Mandatory Service
Bulletin A340-92-4078, Revision 01, dated April 9, 2010; as
applicable; to do the actions required by this AD, unless the AD
specifies otherwise.
(1) The Director of the Federal Register approved the
incorporation by reference of this service information under 5
U.S.C. 552(a) and 1 CFR part 51.
(2) For 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; e-mail <a href="/cdn-cgi/l/email-protection#36575f44415944425e5f5853454518770505061b7705020676575f445443451855595b"><span class="__cf_email__" data-cfemail="a8c9c1dadfc7dadcc0c1c6cddbdb86e99b9b9885e99b9c98e8c9c1dacadddb86cbc7c5">[email protected]</span></a>;
Internet <a href="http://www.airbus.com">http://www.airbus.com</a>.
(3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton,
Washington. For information on the availability of this material at
the FAA, call 425-227-1221.
(4) You may also review copies of the 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: <a href="http://www.archives.gov/federal_register/_code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/_code_of_federal_regulations/ibr_locations.html</a>.
Issued in Renton, Washington, on August 25, 2011.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-22380 Filed 9-12-11; 8:45 am]
BILLING CODE 4910-13-P
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Retrieved: Apr 6, 2026
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