[Federal Register Volume 75, Number 216 (Tuesday, November 9, 2010)]
[Rules and Regulations]
[Pages 68693-68695]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-28166]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-1102; Directorate Identifier 2010-NM-016-AD;
Amendment 39-16507; AD 2010-23-18]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A380-800 Series Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
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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:
During inspection in production and on in-service aircraft, a
number of OverHeat Detection System (OHDS) installation non-
conformities have been identified along the bleed air ducting.
Some installation issues which may lead to a degraded leak
detection capability have been reported. In case of hot air leakage,
the potential degradation of the OHDS would not allow preventing
damages to structure or components, and therefore could lead to an
unsafe condition.
* * * * *
Nonconforming installation or a failure of the OHDS could allow
undetected leakage of bleed air from the hot engine/auxiliary power
unit causing damage to the airplane structure and various airplane
components and systems. This AD requires actions that are intended to
address the unsafe condition described in the MCAI.
DATES: This AD becomes effective November 24, 2010.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in the AD as of November 24,
2010.
We must receive comments on this AD by December 27, 2010.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
Fax: (202) 493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590.
Hand Delivery: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-40, 1200 New
Jersey Avenue, SE., Washington, DC, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
Examining the AD Docket
You may examine the AD docket on the Internet at http://www.regulations.gov; 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 this AD, 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.
FOR FURTHER INFORMATION CONTACT: Todd Thompson, Aerospace Engineer,
Aerospace Engineer, International Branch, ANM-116, Transport Airplane
Directorate, FAA, 1601 Lind Avenue, SW., Renton, Washington 98057-3356;
telephone (425) 227-1175; fax (425) 227-1149.
SUPPLEMENTARY INFORMATION:
Discussion
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
Airworthiness Directive 2009-0265, dated December 16, 2009 (referred to
after this as ``the MCAI''), to correct an unsafe condition for the
specified products. The MCAI states:
During inspection in production and on in-service aircraft, a
number of OverHeat Detection System (OHDS) installation non-
conformities have been identified along the bleed air ducting.
Some installation issues which may lead to a degraded leak
detection capability have been reported. In case of hot air leakage,
the potential degradation of the OHDS would not allow preventing
damages to structure or components, and therefore could lead to an
unsafe condition.
To ensure that in-service aeroplanes are free of such non-
conformities, EASA AD 2009-0066 required an inspection of the OHDS
installation along the bleed air ducting and, in case of findings,
to bring back the installation into the compliant configuration.
That AD required a complete inspection for some MSN, and a partial
inspection for MSN 15, 20 and 22. This partial inspection has now
been assessed to be insufficient to cover the unsafe condition.
This [EASA] AD, which supersedes EASA AD 2009-0066, requires to
perform:
An additional inspection on MSN 15, 20 and 22 to render
it complete, and
A complete inspection on additional MSN.
Nonconforming installation or a failure of the OHDS could allow
undetected leakage of bleed air from the hot engine/auxiliary power
unit causing damage to the airplane structure and various airplane
components and systems. You may obtain further information by examining
the MCAI in the AD docket.
Relevant Service Information
Airbus has issued Mandatory Service Bulletin A380-36-8009,
including Service Bulletin Report Sheet, dated December 7, 2009. The
actions described in this service information are intended to correct
the unsafe condition identified in the MCAI.
FAA's Determination and Requirements of This AD
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to our bilateral agreement with the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are issuing this AD because we
evaluated all pertinent information and determined the unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
There are no products of this type currently registered in the
United States. However, this rule is necessary to ensure that the
described unsafe condition is addressed if any of these products are
placed on the U.S. Register in the future.
Differences Between the 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 FAA policies.
[[Page 68694]]
Any such differences are highlighted in a NOTE within the AD.
FAA's Determination of the Effective Date
Since there are currently no domestic operators of this product,
notice and opportunity for public comment before issuing this AD are
unnecessary.
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and we did not precede it by notice and opportunity for public
comment. We invite you to send any written relevant data, views, or
arguments about this AD. Send your comments to an address listed under
the ADDRESSES section. Include ``Docket No. FAA-2010-1102; Directorate
Identifier 2010-NM-016-AD'' at the beginning of your comments. We
specifically invite comments on the overall regulatory, economic,
environmental, and energy aspects of this AD. We will consider all
comments received by the closing date and may amend this AD because of
those comments.
We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this AD.
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.
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:
2010-23-18 Airbus: Amendment 39-16507. Docket No. FAA-2010-1102;
Directorate Identifier 2010-NM-016-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective November
24, 2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Airbus Model A380-841, -842, and -861
airplanes, certificated in any category, with serial numbers 15, 17,
19, 20, 21, and 22.
Subject
(d) Air Transport Association (ATA) of America Code 36:
Pneumatic.
Reason
(e) The mandatory continued airworthiness information (MCAI)
states:
During inspection in production and on in-service aircraft, a
number of OverHeat Detection System (OHDS) installation non-
conformities have been identified along the bleed air ducting.
Some installation issues which may lead to a degraded leak
detection capability have been reported. In case of hot air leakage,
the potential degradation of the OHDS would not allow preventing
damages to structure or components, and therefore could lead to an
unsafe condition.
* * * * *
Nonconforming installation or a failure of the OHDS could allow
undetected leakage of bleed air from the hot engine/auxiliary power
unit causing damage to the airplane structure and various airplane
components and systems.
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.
Inspection and Corrective Actions
(g) Within 3 months after the effective date of this AD: Do a
one-time detailed visual inspection to ensure the correct
installation of the OHDS sensing elements and insulation muffs, in
accordance with the Accomplishment Instructions of Airbus Mandatory
Service Bulletin A380-36-8009, including Service Bulletin Report
Sheet, dated December 7, 2009.
(h) If, during any inspection required by paragraph (g) of this
AD, any sensing element or insulation muff is found to have been
installed incorrectly, before further flight, bring the installation
into compliant configuration, in accordance with Airbus Mandatory
Service Bulletin A380-36-8009, dated December 7, 2009.
(i) Submit a report of the findings (both positive and negative)
of the inspection required by paragraph (g) of this AD to Airbus,
Customer Services Directorate, 1 Rond Point Maurice Bellonte, 31707
Blagnac Cedex, France; telephone +33 5 61 93 33 33; fax +33 5 61 93
28 06; e-mail [email protected]; Internet http://www.airbus.com, at the applicable time specified in paragraph (i)(1)
or (i)(2) of this AD. The report must include the inspection
results, a description of any discrepancies found, the airplane
serial number, and the number of landings and flight hours on the
airplane.
(1) If the inspection was done on or after the effective date of
this AD: Submit the report within 30 days after the inspection.
(2) If the inspection was done before the effective date of this
AD: Submit the report within 30 days after the effective date of
this AD.
FAA AD Differences
Note 1: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(j) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
International Branch, 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: Todd
Thompson, Aerospace Engineer, International Branch, ANM-116,
Transport Airplane Directorate, FAA, 1601 Lind
[[Page 68695]]
Avenue, SW., Renton, Washington 98057-3356; telephone (425) 227-
1175; 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
(k) Refer to Mandatory Continuing Airworthiness Information
(MCAI) European Aviation Safety Agency (EASA) Airworthiness
Directive 2009-0265, dated December 16, 2009, and Airbus Mandatory
Service Bulletin A380-36-8009, dated December 7, 2009, for related
information.
Material Incorporated by Reference
(l) You must use Airbus Mandatory Service Bulletin A380-36-8009,
including Service Bulletin Report Sheet, dated December 7, 2009, 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--EANA (Airworthiness Office); 1 Rond Point Maurice
Bellonte, 31707 Blagnac Cedex, France; telephone +33 562 110 253;
Fax +33 562 110 307; e-mail [email protected];
Internet http://www.airbus.com.
(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: http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Issued in Renton, Washington, on October 26, 2010.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-28166 Filed 11-8-10; 8:45 am]
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