E7-3658. Airworthiness Directives; Airbus Model A330 and A340 Airplanes  

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    AGENCY:

    Federal Aviation Administration (FAA), Department of Transportation (DOT).

    ACTION:

    Final rule.

    SUMMARY:

    The FAA is adopting a new airworthiness directive (AD) for all Airbus Model A330 and A340 airplanes. This AD requires revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness by incorporating new and revised certification maintenance requirements (CMRs). This AD results from the manufacturer's determination that additional and revised CMRs are necessary in order to ensure continued operational safety of the affected airplanes. We are issuing this AD to prevent safety-significant latent failures that would, in combination with one or more other specific failures or events, result in a hazardous or catastrophic failure condition.

    DATES:

    This AD becomes effective April 9, 2007.

    The Director of the Federal Register approved the incorporation by reference of certain publications listed in the AD as of April 9, 2007.

    ADDRESSES:

    You may examine the AD docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility, U.S. Department of Transportation, 400 Seventh Street, SW., Nassif Building, Room PL-401, Washington, DC.

    Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France, for service information identified in this AD.

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    FOR FURTHER INFORMATION CONTACT:

    Tim Backman, Aerospace Engineer, International Branch, ANM-116, FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington Start Printed Page 965998057-3356; telephone (425) 227-2797; fax (425) 227-1149.

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    SUPPLEMENTARY INFORMATION:

    Examining the Docket

    You may examine the airworthiness directive (AD) docket on the Internet at http://dms.dot.gov or in person at the Docket Management Facility office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The Docket Management Facility office (telephone (800) 647-5227) is located on the plaza level of the Nassif Building at the street address stated in the ADDRESSES section.

    Discussion

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to include an AD that would apply to all Airbus Model A330 and A340 airplanes. That NPRM was published in the Federal Register on December 27, 2006 (71 FR 77632). That NPRM proposed to require revising the Airworthiness Limitations section of the Instructions for Continued Airworthiness by incorporating new and revised certification maintenance requirements (CMRs).

    Comments

    We provided the public the opportunity to participate in the development of this AD. We received no comments on the NPRM or on the determination of the cost to the public.

    Conclusion

    We have carefully reviewed the available data and determined that air safety and the public interest require adopting the AD as proposed.

    Costs of Compliance

    This AD affects about 27 Model A330 airplanes of U.S. registry. The required actions take about 1 work hour per airplane, at an average labor rate of $80 per work hour. Based on these figures, the estimated cost of this AD for U.S. operators is $2,160, or $80 per airplane.

    Currently there are no affected Model A340 airplanes on the U.S. Register. However, if an affected airplane is imported and placed on the U.S. Register in the future, the required actions would take about 1 work hour per airplane, at an average labor rate of $80 per work hour. Based on these figures, the estimated cost of this AD to U.S. operators is $80 per airplane.

    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 have 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 that this AD:

    (1) Is not a “significant regulatory action” under Executive Order 12866;

    (2) Is not a “significant rule” under 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. See the ADDRESSES section for a location to examine the regulatory evaluation.

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    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Incorporation by reference
    • Safety
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    Adoption of the Amendment

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    Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

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    PART 39—AIRWORTHINESS DIRECTIVES

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    1. The authority citation for part 39 continues to read as follows:

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    Authority: 49 U.S.C. 106(g), 40113, 44701.

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    [Amended]
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    2. The Federal Aviation Administration (FAA) amends § 39.13 by adding the following new airworthiness directive (AD):

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    2007-05-08  Airbus: Amendment 39-14969. Docket No. FAA-2006-26684; Directorate Identifier 2006-NM-193-AD.

    Effective Date

    (a) This AD becomes effective April 9, 2007.

    Affected ADs

    (b) None.

    Applicability

    (c) This AD applies to all Airbus Model A330 and A340 airplanes.

    Note 1:

    This AD requires revisions to certain operator maintenance documents to include new inspections. Compliance with these inspections is required by 14 CFR 91.403(c). For airplanes that have been previously modified, altered, or repaired in the areas addressed by these inspections, the operator may not be able to accomplish the inspections described in the revisions. In this situation, to comply with 14 CFR 91.403(c), the operator must request approval for an alternative method of compliance according to paragraph (g) of this AD. The request should include a description of changes to the required inspections that will ensure the continued damage tolerance of the affected structure. The FAA has provided guidance for this determination in Advisory Circular (AC) 25-1529-1.

    Unsafe Condition

    (d) This AD results from the manufacturer's determination that additional and revised certification maintenance requirements (CMRs) are necessary in order to ensure continued operational safety of the affected airplanes. We are issuing this AD to prevent safety-significant latent failures that would, in combination with one or more other specific failures or events, result in a hazardous or catastrophic failure condition.

    Compliance

    (e) You are responsible for having the actions required by this AD performed within the compliance times specified, unless the actions have already been done.

    Revise the Airworthiness Limitations Section of the Instructions for Continued Airworthiness

    (f) Within 3 months after the effective date of this AD: Revise the Airworthiness Limitations section of the Instructions for Continued Airworthiness by incorporating Airbus A330 Certification Maintenance Requirements, Document 955.2074/93, Issue 19, dated March 22, 2006 (for all Model A330 airplanes); or Airbus A340 Certification Maintenance Requirements, Document 955.3019/92, Issue 14, dated December 19, 2005 (for all Model A340 airplanes). Accomplish the actions specified in the applicable CMR at the times specified in the applicable CMR and in accordance with the applicable CMR, except as provided by paragraphs (f)(1), (f)(2), (f)(3), and (f)(4) of this AD. Start Printed Page 9660

    (1) The associated interval for any new task is to be counted from the effective date of this AD.

    (2) The associated interval for any revised task is to be counted from the previous performance of the task.

    (3) For Model A340 airplanes that have exceeded the more restrictive limitations of Airbus A340 Certification Maintenance Requirements, Document 955.3019/92, Issue 14, Maintenance Significant Items (MSI) 21.28.00 and 21.43.00: Do the task within 2,500 flight hours after the previous accomplishment. Repeat the task thereafter at the applicable interval in the Airbus A340 Certification Maintenance Requirements, Document 955.3019/92, Issue 14.

    (4) For Model A340 airplanes that have accumulated more than 2,700 flight hours since the last maintenance done in accordance with Airbus A340 Certification Maintenance Requirements, Document 955.3019/92, Issue 14, MSI 28.24.00: Do the next task within 800 flight hours after the effective date of this AD. Repeat the task thereafter at the applicable interval in the Airbus A340 Certification Maintenance Requirements, Document 955.3019/92, Issue 14.

    Alternative Methods of Compliance (AMOCs)

    (g)(1) The Manager, International Branch, ANM-116, Transport Airplane Directorate, FAA, has the authority to approve AMOCs for this AD, if requested in accordance with the procedures found in 14 CFR 39.19.

    (2) Before using any AMOC approved in accordance with § 39.19 on any airplane to which the AMOC applies, notify the appropriate principal inspector in the FAA Flight Standards Certificate Holding District Office.

    Related Information

    (h) The European Aviation Safety Agency airworthiness directives 2006-0224, dated July 27, 2006, and 2006-0225, dated July 21, 2006, also address the subject of this AD.

    Material Incorporated by Reference

    (i) You must use Airbus A330 Certification Maintenance Requirements, Document 955.2074/93, Issue 19, dated March 22, 2006; or Airbus A340 Certification Maintenance Requirements, Document 955.3019/92, Issue 14, dated December 19, 2005; as applicable, to perform the actions that are required by this AD, unless the AD specifies otherwise. The Director of the Federal Register approved the incorporation by reference of these documents in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France, for a copy of this service information. You may review copies at the FAA, Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton, Washington; or 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.

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    Issued in Renton, Washington, on February 22, 2007.

    Ali Bahrami,

    Manager, Transport Airplane Directorate, Aircraft Certification Service.

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    [FR Doc. E7-3658 Filed 3-2-07; 8:45 am]

    BILLING CODE 4910-13-P

Document Information

Effective Date:
4/9/2007
Published:
03/05/2007
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule.
Document Number:
E7-3658
Dates:
This AD becomes effective April 9, 2007.
Pages:
9658-9660 (3 pages)
Docket Numbers:
Docket No. FAA-2006-26684, Directorate Identifier 2006-NM-193-AD, Amendment 39-14969, AD 2007-05-08
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
Topics:
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
PDF File:
e7-3658.pdf
CFR: (1)
14 CFR 39.13