[Federal Register Volume 75, Number 37 (Thursday, February 25, 2010)]
[Rules and Regulations]
[Pages 8471-8473]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2010-3472]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0131; Directorate Identifier 2009-NM-132-AD;
Amendment 39-16216; AD 2010-05-07]
RIN 2120-AA64
Airworthiness Directives; Airbus Model A340-200 and A340-300
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:
A review of A340 missions has demonstrated that CFM56-5C forward
engine mount thrust links fitted with oversized bearing[s] will not
reach the updated link fatigue life limit of 15,500 Flight Cycles
(FC) due to an increase in bore diameter.
* * * The consequent potential failure of the affected thrust
link would reduce the forward engine mounts' structural integrity
and could eventually lead to engine separation, constituting an
unsafe condition.
* * * * *
This AD requires actions that are intended to address the unsafe
condition described in the MCAI.
DATES: This AD becomes effective March 12, 2010.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in the AD as of March 12,
2010.
We must receive comments on this AD by April 12, 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: 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
The European Aviation Safety Agency (EASA), which is the Technical
Agent for the Member States of the European Community, has issued EASA
Airworthiness Directive 2009-0108, dated May 5, 2009 (referred to after
this as ``the MCAI''), to correct an unsafe condition for the specified
products. The MCAI states:
A review of A340 missions has demonstrated that CFM56-5C forward
engine mount thrust links fitted with oversized bearing[s] will not
reach the updated link fatigue life limit of 15,500 Flight Cycles
(FC) due to an increase in bore diameter.
Oversized bearing repairs have been possible through the
accomplishment of CMM 71-21-12 Repair 1. The consequent potential
failure of the affected thrust link would reduce the forward engine
mounts' structural integrity and could eventually lead to engine
separation, constituting an unsafe condition.
Consequently, this AD requires:
--The [detailed] inspection of the link assembly to identify a
possible oversized bearing repair and, in case of finding, the
application of the associated corrective actions, or
--The repetitive [detailed] inspection [for cracking, damage (e.g.,
dents), and missing fasteners] of the forward engine mounts until
accomplishment of the inspection of the link assembly for the
identification of a possible oversized bearing repair.
The corrective actions for finding oversized bearings in the forward
engine mount thrust link assembly include contacting Goodrich for
instructions and doing the repair. The corrective actions for finding
cracking, damage (e.g., dents), and missing fasteners in the forward
engine mounts include, depending on the findings, replacing cracked
parts and missing fasteners, and polishing damaged areas. You may
obtain further information by examining the MCAI in the AD docket.
Relevant Service Information
Airbus has issued Mandatory Service Bulletin A340-71-4007,
including Appendix 1, dated April 1, 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.
[[Page 8472]]
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. 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-2010-0131; Directorate
Identifier 2009-NM-132-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:
2010-05-07 Airbus: Amendment 39-16216. Docket No. FAA-2010-0131;
Directorate Identifier 2009-NM-132-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective March
12, 2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to all Airbus Model A340-211, -212, and -213
airplanes; and Model A340-311, -312, and -313 series airplanes;
certificated in any category.
Subject
(d) Air Transport Association (ATA) of America Code 71:
Powerplant.
Reason
(e) The mandatory continued airworthiness information (MCAI)
states:
A review of A340 missions has demonstrated that CFM56-5C forward
engine mount thrust links fitted with oversized bearing[s] will not
reach the updated link fatigue life limit of 15500 Flight Cycles
(FC) due to an increase in bore diameter.
Oversized bearing repairs have been possible through the
accomplishment of CMM 71-21-12 Repair 1. The consequent potential
failure of the affected thrust link would reduce the forward engine
mounts structural integrity and could eventually lead to engine
separation, constituting an unsafe condition.
Consequently, this AD requires:
--The [detailed] inspection of the link assembly to identify a
possible oversized bearing repair and, in case of finding, the
application of the associated corrective actions, or
--The repetitive [detailed] inspection [for cracking, damage (e.g.,
dents), and missing fasteners] of the forward engine mounts until
accomplishment of the inspection of the link assembly for the
identification of a possible oversized bearing repair.
The corrective actions for finding oversized bearings in the forward
engine mount thrust link assembly include contacting Goodrich for
instructions and doing the repair. The corrective actions for
finding cracking, damage (e.g., dents), and missing fasteners in the
forward engine mounts include, depending on the findings, replacing
cracked parts and missing fasteners, and polishing damaged areas.
Actions and Compliance
(f) Unless already done, do the following actions.
(1) Within 1,700 flight cycles or 24 months from the effective
date of this AD, whichever occurs first: Do the actions required by
paragraph (f)(1)(i) or (f)(1)(ii) of this AD.
(i) Perform a detailed inspection for oversized bearing repair
of the forward engine mount thrust link assembly, in accordance with
the Accomplishment Instructions of Airbus Mandatory Service Bulletin
A340-71-4007, dated April 1, 2009. If oversized bearings are found,
before further flight, contact Goodrich for instructions, and do the
repair.
(ii) Perform a detailed inspection of the forward engine mounts
for cracking, damage (e.g., dents), and missing fasteners, in
accordance with Task 71-21-11-210-801-0 of the Airbus A340 Aircraft
Maintenance Manual, Revision 68, dated October 1, 2009. Do all
applicable corrective actions before further flight in accordance
with Task 71-21-11-210-801-0 of the Airbus A340 Aircraft Maintenance
Manual, Revision 68, dated October 1, 2009. Repeat the inspection
thereafter at intervals not to exceed 1,700 flight cycles or 24
months, whichever occurs
[[Page 8473]]
first, until the inspection required by paragraph (f)(2) of this AD
is done.
(2) For airplanes on which the inspection specified in paragraph
(f)(1)(ii) of this AD is done: Within 4,500 flight cycles from the
effective date of this AD, do the inspection and applicable
corrective actions required by paragraph (f)(1)(i) of this AD. Doing
the inspection and applicable corrective actions required by
paragraph (f)(1)(i) of this AD terminates the repetitive inspections
required by paragraph (f)(1)(ii) of this AD.
FAA AD Differences
Note 1: This AD differs from the MCAI and/or service
information as follows:
Airbus Mandatory Service Bulletin A340-71-4007, dated April 1,
2009; does not contain corrective actions if damage is found during
the inspection of the forward engine mounts. The corrective actions
are specified in Task 71-21-11-210-801-0 of the Airbus A340 Aircraft
Maintenance Manual, Revision 68, dated October 1, 2009. Therefore,
this AD refers to Task 71-21-11-210-801-0 of the Airbus A340
Aircraft Maintenance Manual, Revision 68, dated October 1, 2009, for
the inspection and corrective actions.
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 2009-0108, dated May 5, 2009; Airbus Mandatory Service
Bulletin A340-71-4007, dated April 1, 2009; and Task 71-21-11-210-
801-0 of the Airbus A340 Aircraft Maintenance Manual, Revision 68,
dated October 1, 2009; for related information.
Material Incorporated by Reference
(i) You must use Airbus Mandatory Service Bulletin A340-71-4007,
including Appendix 1, dated April 1, 2009; and Task 71-21-11-210-
801-0 of the Airbus A340 Aircraft Maintenance Manual, Revision 68,
dated October 1, 2009; as applicable; to do the actions required by
this AD, unless the AD specifies otherwise. The Airbus aircraft
maintenance manual contains the following effective pages:
List of Effective Pages
----------------------------------------------------------------------------------------------------------------
Page title/description Page Nos. Revision No. Date shown on page(s)
----------------------------------------------------------------------------------------------------------------
AMM Title Page................. None shown............... 68....................... October 1, 2009.
AMM Introduction--Description 1-6...................... None shown*.............. None shown.*
and Operation.
Chapter 71--Table of Contents.. 1, 3, 5.................. None shown*.............. January 1, 2009.
Chapter 71--Effective Pages.... 2, 4, 6-11............... None shown*.............. January 1, 2008.
Task 71-21-11-210-801-0........ 1-5...................... None shown*.............. None shown.*
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*The revision level and date is indicated only on the title page of this document.
(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 [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 or 425-227-1152.
(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 February 16, 2010.
Stephen P. Boyd,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-3472 Filed 2-24-10; 8:45 am]
BILLING CODE 4910-13-P