AD 2010-10-25
final rule
Applicability
| Type | Manufacturer | Model | Details |
|---|---|---|---|
| aircraft | Airbus | A330-201 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-202 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-203 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-223 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-243 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-301 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-302 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-303 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-321 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-322 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-323 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-341 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-342 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A330-343 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A340-211 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A340-212 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
| aircraft | Airbus | A340-213 | Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes, and Model A340-300 Series Airplanes |
Unsafe Condition
In the door 2 area, the hat-racks are supplied with a basic wire harness which includes 'Oxygen Masks' activation. In case of a monument installation, the respective non-used hat-rack connections between monument and outer skin are put on stow. The distance between the stowed wire harness and the monument could be too small, leading to a short circuit of wires dedicated to oxygen, which could result in a large number of passenger oxygen masks not being supplied with oxygen during an emergency.
AI-generated summary from the source AD text. Verify against the official source before acting.
Required Actions
Modify the hat rack connectors on stow and reroute the associated wire harness in case of monument installed in door 2 area. Refer to Airbus Mandatory Service Bulletin A340-92-4073, Revision 02, dated October 12, 2009, or A330-92-3070, Revision 02, dated August 19, 2009, for specific instructions.
AI-generated summary from the source AD text. Verify against the official source before acting.
Compliance Time
Within 24 months of the effective date for door-2 areas where a monument is installed.
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, and Model A340-300 Series Airplanes with monument installations in door 2 area.
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 75, Number 98 (Friday, May 21, 2010)]
[Rules and Regulations]
[Pages 28475-28478]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2010-11740]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0914; Directorate Identifier 2009-NM-122-AD;
Amendment 39-16304; AD 2010-10-25]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A330-200 and -300 Series
Airplanes, and Model A340-300 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:
In the door 2 area, the hat-racks are supplied with a basic wire
harness which includes ``Oxygen Masks'' activation.
In case of a monument installation, the respective non-used hat-
rack connections between monument and outer skin are put on stow. It
was noticed in production, that the distance between the stowed wire
harness and the monument could be too small. 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 June 25, 2010.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of June 25,
2010.
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 October 19, 2009 (74
FR 53440). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
[[Page 28476]]
In the door 2 area, the hat-racks are supplied with a basic wire
harness which includes ``Oxygen Masks'' activation.
In case of a monument installation, the respective non-used hat-
rack connections between monument and outer skin are put on stow. It
was noticed in production, that the distance between the stowed wire
harness and the monument could be too small. 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 AD requires the
modification of the hat rack connectors on stow, and the rerouting
of the associated wire harness in case of monument installed in door
2 area.
You may obtain further information by examining the MCAI in the AD
docket.
Relevant Service Information
Airbus has issued Mandatory Service Bulletin A340-92-4073, Revision
02, dated October 12, 2009. Revision 02 includes the following changes:
<bullet> Adds a note stating that the modification of cable harness
5302VB/5303VB is necessary only if the cable is installed; and
<bullet> Makes minor text corrections.
We referred to Airbus Mandatory Service Bulletin A340-92-4073,
Revision 01, dated January 13, 2009, as the appropriate source of
service information for accomplishing the actions specified in the NPRM
(for Model A340-300 series airplanes).
We have revised paragraphs (f)(1), (f)(2), and (h) of this AD to
cite Airbus Mandatory Service Bulletin A340-92-4073, Revision 02, dated
October 12, 2009. We have added paragraph (f)(3) of this AD to give
credit for accomplishment of the actions done in accordance with the
Airbus Mandatory Service Bulletin A340-92-4073, Revision 01, dated
January 13, 2009; or Airbus Mandatory Service Bulletin A340-92-4073,
dated July 10, 2008.
Airbus has also issued Mandatory Service Bulletin A330-92-3070,
Revision 02, dated August 19, 2009. Revision 02 includes the following
changes:
<bullet> Removes airplanes from the effectivity;
<bullet> Makes minor text changes;
<bullet> Changes the location of wire harness 5315VB/5316VB in
Figure 2; and
<bullet> Adds a note stating that modification of wire harness
5302VB/5303VB is only necessary if installed.
We referred to Airbus Mandatory Service Bulletin A330-92-3070,
Revision 01, dated January 12, 2009, as the appropriate source of
service information for accomplishing the actions specified in the NPRM
(for Model A330-200 and A330-300 series airplanes).
We have revised paragraphs (f)(1), (f)(2), and (h) of this AD to
cite Airbus Mandatory Service Bulletin A330-92-3070, Revision 02, dated
August 19, 2009. We have added paragraph (f)(3) to give credit for
accomplishment of the actions done in accordance with Airbus Mandatory
Service Bulletin A330-92-3070, dated July 10, 2008; or Airbus Mandatory
Service Bulletin A330-92-3070, Revision 01, dated January 12, 2009.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comments received.
Support for the NPRM
Air Line Pilots Association (ALPA), International supports the
NRPM.
Request To Extend Compliance Time
Northwest Airlines (NWA) requests that we extend the proposed
compliance time for the modification specified in paragraph (f) of the
NPRM from within 24 months to within 24 months for locations where
monuments are installed, and for other specified locations, to within
72 months or at the time of a new monument installation, whichever
occurs first. NWA explains that its Model A330 airplanes have a
monument installed in only one of the four locations specified in the
service information, and that according to paragraph (e) of the NPRM,
the unsafe condition only exists at locations where there is a monument
installed. NWA reasons that allowing a later compliance time for those
areas without monuments would allow operators to accomplish the
required actions while access is available to the monuments during
normally scheduled maintenance.
We do not agree to extend the compliance time specified in
paragraph (f) of the final rule for door-2 locations without an
installed monument. This AD requires modification of non-used hat-rack
connections between the monument and outer skin only for door-2 areas
where a monument is installed, as specified in the Accomplishment
Instructions of Airbus Mandatory Service Bulletin A330-92-3070,
Revision 02, dated August 19, 2009; or Airbus Mandatory Service
Bulletin A340-92-4073, Revision 02, dated October 12, 2009; which
ensures the clearance between the wire harnesses and the monument. The
service bulletins also specify airplane configurations and the actions
for each configuration. There are no actions required for those door-2
areas without monuments. We have clarified paragraph (f)(1) of this AD
by adding the phrase ``for airplanes on which a monument is installed
in the door-2 area, as specified in Airbus Mandatory Service Bulletin
A330-92-3070, Revision 02, dated August 19, 2009; or Airbus Mandatory
Service Bulletin A340-92-4073, Revision 02, dated October 12, 2009.''
Request To Revise Proposed Costs of Compliance
NWA requests that we revise the Cost of Compliance section of the
NPRM to portray the cost to operators as though all four locations
require a monument installation. NWA explains that airplanes configured
with only a single lavatory require 57 labor hours for removal,
installation, and testing. If an operator were to have a monument
installation at each of the four locations, NWA asserts that the labor
hours could be as high as 241 hours for an airplane configured with
three lavatories and a video control center.
We agree to revise the Cost of Compliance section of the final rule
to portray the cost to operators as though all four locations require a
monument installation. As the service information indicates, time to
get access to the modified area should be included in the cost, with
respect to operators having to perform a monument installation at all
four locations. We are adding 3 work-hours to NWA's estimate of 241
work-hours to account for the modification. Also, the number of
affected products of U.S. registry is now 32. We have revised the Costs
of Compliance section of the final rule accordingly.
Conclusion
We reviewed the available data, including the comments received,
and determined that air safety and the public interest require adopting
the AD with the changes described previously. We determined that these
changes 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
[[Page 28477]]
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.
Explanation of Change to Costs of Compliance
Since issuance of the NPRM, we have increased the labor rate used
in the Costs of Compliance from $80 per work-hour to $85 per work-hour.
The Costs of Compliance information, below, reflects this increase in
the specified hourly labor rate.
Costs of Compliance
We estimate that this AD will affect 32 products of U.S. registry.
We also estimate that it will take about 244 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts costs are negligible. Where the
service information lists required parts costs that are covered under
warranty, we have assumed that there will be no charge for these parts.
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 this AD to the U.S. operators to be
$663,680, or $20,740 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, 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
0
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:
2010-10-25 Airbus: Amendment 39-16304. Docket No. FAA-2009-0914;
Directorate Identifier 2009-NM-122-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective June 25,
2010.
Affected ADs
(b) None.
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 Airbus Model A340-311, -312, and -313 airplanes;
certificated in any category; all manufacturer serial numbers on
which Airbus Modification 48825 has been embodied in production,
except those on which Airbus Modification 57409 has been embodied in
production.
Subject
(d) Air Transport Association (ATA) of America Code 92.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
In the door 2 area, the hat-racks are supplied with a basic wire
harness which includes ``Oxygen Masks'' activation.
In case of a monument installation, the respective non-used hat-
rack connections between monument and outer skin are put on stow. It
was noticed in production, that the distance between the stowed wire
harness and the monument could be too small. 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 AD requires the
modification of the hat rack connectors on stow, and the rerouting
of the associated wire harness in case of monument installed in door
2 area.
Actions and Compliance
(f) Unless already done, do the following actions.
(1) For airplanes on which a monument is installed in the door 2
area, as specified in Airbus Mandatory Service Bulletin A330-92-
3070, Revision 02, dated August 19, 2009; or Airbus Mandatory
Service Bulletin A340-92-4073, Revision 02, dated October 12, 2009:
Within 24 months after the effective date of this AD, modify both
the left-hand (L/H) and right-hand (R/H) hat-rack connectors, in
accordance with the Accomplishment Instructions of Airbus Mandatory
Service Bulletin A330-92-3070, Revision 02, dated August 19, 2009;
or Airbus Mandatory Service Bulletin A340-92-4073, Revision 02,
dated October 12, 2009; as applicable; except as provided by
paragraphs (f)(2) and (f)(3) of this AD.
(2) Modifications done before the effective date of this AD, in
accordance with the Accomplishment Instructions of Airbus Mandatory
Service Bulletin A330-92-3070 or A340-92-4073, both dated July 10,
2008, as applicable, are acceptable for compliance with the
applicable requirements of paragraph (f)(1) of this AD, provided
that within 24 months after the effective date of this AD, the
``ADDITIONAL WORK'' specified in the Accomplishment Instructions of
Airbus Mandatory Service Bulletin A330-92-3070, Revision 01, dated
January 12, 2009, or Revision 02, dated August 19, 2009; or Airbus
Mandatory Service Bulletin A340-92-4073, Revision 01, dated January
13, 2009, or Revision 02, dated October 12, 2009; as applicable; is
accomplished.
(3) Modifying both the L/H and R/H hat-rack connectors is also
acceptable for
[[Page 28478]]
compliance with the requirements of paragraph (f)(1) of this AD if
done before the effective date of this AD in accordance with the
Accomplishment Instructions of Airbus Mandatory Service Bulletin
A330-92-3070, Revision 01, dated January 12, 2009; or Airbus
Mandatory Service Bulletin A340-92-4073, Revision 01, dated January
13, 2009.
FAA AD Differences
Note 1: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(g) 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. Send information 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.
Before using any approved AMOC on any airplane to which the AMOC
applies, notify your principal maintenance inspector (PMI) or
principal avionics inspector (PAI), as appropriate, or lacking a
principal inspector, your local Flight Standards 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.
(3) Reporting Requirements: For any reporting requirement in
this AD, under the provisions of the Paperwork Reduction Act (44
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has
approved the information collection requirements and has assigned
OMB Control Number 2120-0056.
Related Information
(h) Refer to MCAI European Aviation Safety Agency Airworthiness
Directive 2009-0077, dated April 6, 2009; Airbus Mandatory Service
Bulletin A330-92-3070, Revision 02, dated August 19, 2009; and
Airbus Mandatory Service Bulletin A340-92-4073, Revision 02, dated
October 12, 2009; for related information.
Material Incorporated by Reference
(i) You must use Airbus Mandatory Service Bulletin A330-92-3070,
Revision 02, dated August 19, 2009; or Airbus Mandatory Service
Bulletin A340-92-4073, Revision 02, dated October 12, 2009; 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#b3d2dac1c4dcc1c7dbdaddd6c0c09df28080839ef2808783f3d2dac1d1c6c09dd0dcde"><span class="__cf_email__" data-cfemail="7918100b0e160b0d1110171c0a0a57384a4a4954384a4d493918100b1b0c0a571a1614">[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 May 6, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraaft Certification
Service.
[FR Doc. 2010-11740 Filed 5-20-10; 8:45 am]
BILLING CODE 4910-13-P
Source: Official FAA Source ↗
Retrieved: Apr 6, 2026
Rights: U.S. Government Public Domain
This site is not affiliated with or endorsed by the FAA. Always verify with official sources.