Airworthiness Directives; Airbus Model A310 Series Airplanes

[Federal Register Volume 70, Number 5 (Friday, January 7, 2005)]
[Rules and Regulations]
[Pages 1335-1336]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-163]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2004-19560; Directorate Identifier 2004-NM-121-AD; 
Amendment 39-13930; AD 2005-01-06]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A310 Series Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Airbus Model A310 series airplanes. This AD requires modifying the wire 
routing of electrical harness 636VB in the right-hand wing. This AD is 
prompted by the manufacturer's analysis for compliance with Special 
Federal Aviation Regulation No. 88, which has shown that wiring 2M of 
the 115V anti-collision white strobe lights and wiring 2S of the fuel 
quantity indication system (FQIS) should be rerouted into separate 
conduits. We are issuing this AD to prevent chafing damage to wiring 2M 
and 2S, which could result in a short circuit and consequently 
introduce an electrical current into the wiring of the FQIS and create 
an ignition source in the fuel tank.

DATES: This AD becomes effective February 11, 2005.
    The incorporation by reference of a certain publication listed in 
the AD is approved by the Director of the Federal Register as of 
February 11, 2005.

ADDRESSES: For service information identified in this AD, contact 
Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France. You 
can examine this information 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.
    You can examine the contents of this 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., room PL-401, 
on the plaza level of the Nassif Building, Washington, DC. This docket 
number is FAA-2004-19560; the directorate identifier for this docket is 
2004-NM-121-AD.

FOR FURTHER INFORMATION CONTACT: Tim Backman, Aerospace Engineer, 
International Branch, ANM-116, FAA, Transport Airplane Directorate, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-2797; fax (425) 227-1149.

Examining the Docket

    The AD docket contains the proposed AD, comments, and any final 
disposition. You can examine the 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 DOT 
street address stated in the ADDRESSES section.

SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39 
with an AD for all Airbus Model A310 series airplanes. That action, 
published in the Federal Register on November 9, 2004 (69 FR 64871), 
proposed to require modifying the wire routing of electrical harness 
636VB in the right-hand wing.

Comments

    We provided the public the opportunity to participate in the 
development of this AD. No comments have been submitted on the proposed 
AD 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 will affect about 51 airplanes of U.S. registry. The 
required actions will take about 34 work hours per airplane, at an 
average labor rate of $65 per work hour. Required parts will cost about 
$356 per airplane. Based on these figures, the estimated cost of the AD 
for U.S. operators is $130,866 or $2,566 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. See the ADDRESSES section for a location to 
examine the regulatory evaluation.

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.

[[Page 1336]]

Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2005-01-06 Airbus: Amendment 39-13930. Docket No. FAA-2004-19560; 
Directorate Identifier 2004-NM-121-AD.

Effective Date

    (a) This AD becomes effective February 11, 2005.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to all Airbus Model A310-203, -204, -221, -
222, -304, -322, -324, and -325 series airplanes, certificated in 
any category.

Unsafe Condition

    (d) This AD was prompted by the manufacturer's analysis for 
compliance with Special Federal Aviation Regulation No. 88, which 
has shown that wiring 2M of the 115V anti-collision white strobe 
lights and wiring 2S of the fuel quantity indication system (FQIS) 
should be rerouted into separate conduits. We are issuing this AD to 
prevent chafing damage to wiring 2M and 2S, which could result in a 
short circuit and consequently introduce an electrical current into 
the wiring of the FQIS and create an ignition source in the fuel 
tank.

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.

Modification

    (f) Within 72 months after the effective date of this AD, modify 
the routing of electrical harness 636VB in the right-hand wing by 
accomplishing all of the actions in the Accomplishment Instructions 
of Airbus Service Bulletin A310-28-2140, Revision 04, dated March 
31, 2004.

Credit for Previously Accomplished Service Bulletins

    (g) Modification of the routing of electrical harness 636VB 
accomplished before the effective date of this AD in accordance with 
Airbus Service Bulletin A310-28-2140, Revision 02, dated May 24, 
2002; or Revision 03, dated November 21, 2002; is acceptable for 
compliance with the requirements of paragraph (f) of this AD.

Alternative Methods of Compliance (AMOCs)

    (h) 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.

Related Information

    (i) French airworthiness directive F-2004-005, dated January 7, 
2004, also addresses the subject of this AD.

Material Incorporated by Reference

    (j) You must use Airbus Service Bulletin A310-28-2140, Revision 
04, dated March 31, 2004, to perform the actions that are required 
by this AD, unless the AD specifies otherwise. The Director of the 
Federal Register approves the incorporation by reference of this 
document in accordance with 5 U.S.C. 552(a) and 1 CFR part 51. For 
copies of the service information, contact Airbus, 1 Rond Point 
Maurice Bellonte, 31707 Blagnac Cedex, France. For information on 
the availability of this material at the National Archives and 
Records Administration (NARA), call (202) 741-6030, or go to http://www.archives.gov/federal_ register/code--of --federal--regulations/
ibr--locations.html.
    You may view the AD docket at the Docket Management Facility, 
U.S. Department of Transportation, 400 Seventh Street SW, room PL-
401, Nassif Building, Washington, DC.

    Issued in Renton, Washington, on December 27, 2004.
Kevin M. Mullin,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 05-163 Filed 1-6-05; 8:45 am]
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