Airworthiness Directives; Airbus Model A330-200 and -300 Series Airplanes and Model A340-200, -300, -500, and -600 Series Airplanes, 10230-10233 [2011-4041]

Download as PDF 10230 Federal Register / Vol. 76, No. 37 / Thursday, February 24, 2011 / Rules and Regulations material at an NARA facility, call 202–741– 6030, or go to https://www.archives.gov/ federal_register/code_of_federal_regulations/ ibr_locations.html. Issued in Renton, Washington, on February 14, 2011. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2011–4013 Filed 2–23–11; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2010–0859; Directorate Identifier 2010–NM–113–AD; Amendment 39–16614; AD 2011–05–05] RIN 2120–AA64 Airworthiness Directives; Airbus Model A330–200 and –300 Series Airplanes and Model A340–200, –300, –500, and –600 Series Airplanes Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. AGENCY: 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: * * * * * SUMMARY: * * * [T]here is a possible path for fluid ingress, resulting in connector internal arcing and hydraulic system malfunction. In addition, as the connectors are located in areas adjacent to fuel tanks, such arcing associated with the presence of a fuel leakage could lead to an uncontrolled fire. * * * * * We are issuing this AD to require actions to correct the unsafe condition on these products. DATES: This AD becomes effective March 31, 2011. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of March 31, 2011. ADDRESSES: You may examine the AD docket on the Internet at https:// www.regulations.gov 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 September 29, 2010 (75 FR 60010). That NPRM proposed to correct an unsafe condition for the specified products. The MCAI states: Several A330 and A340 operators have reported in service occurrences of hydraulic pump electrical motor connector internal arcing, resulting in: —Either false hydraulic system overheat Electronic Centralized Aircraft Monitoring (ECAM) warnings —and/or hydraulic pump electrical motor malfunction. Investigations have shown that, due to the manufacturing tolerances of the cables and the connectors rear grommet, there is a possible path for fluid ingress, resulting in connector internal arcing and hydraulic system malfunction. In addition, as the connectors are located in areas adjacent to fuel tanks, such arcing associated with the presence of a fuel leakage could lead to an uncontrolled fire. In order to protect the hydraulic pump electrical motor connectors against fluid ingress from the rear of the connector grommet and prevent false hydraulic system overheat ECAM warnings and/or hydraulic pump electrical motor malfunction, this AD requires modification of the three hydraulic pump electrical motor connectors associated to the Blue, Yellow and Green hydraulic systems. This Revision 1 is issued to delete Airbus modifications 55923S18878 and 55924S19452 from the applicability of this AD. The modification adds heat shrink sleeves to certain cable contacts and a sealing plug to the connector free cavity. You may obtain further information by examining the MCAI in the AD docket. Relevant Service Information The NPRM referred to the service information in the following table as the applicable sources of service information. TABLE—SERVICE INFORMATION CITED IN THE NPRM Airplane model— Airbus Mandatory Service Bulletin— A330 ................. A340 ................. A340 ................. A330–92–3088, including Appendix 01 ........................................................................ A340–92–4081, including Appendix 01 ........................................................................ A340–92–5053, including Appendix 01 ........................................................................ Airbus has released the service information in the following table. No additional work is necessary for airplanes on which earlier revisions of Revision— the service information are done. We have updated Tables 1 and 3 of the final rule to refer to these sources of service information. We have also updated Dated— 01 01 01 February 22, 2010. February 22, 2010. February 22, 2010. Table 2 of the final rule to give credit for using Revision 01 of the service information. jlentini on DSKJ8SOYB1PROD with RULES TABLE—REVISED SERVICE INFORMATION Airplane model— Airbus Mandatory Service Bulletin— A330 ................. A340 ................. A340 ................. A330–92–3088, including Appendix 01 ........................................................................ A340–92–4081, including Appendix 01 ........................................................................ A340–92–5053, including Appendix 01 ........................................................................ VerDate Mar<15>2010 16:10 Feb 23, 2011 Jkt 223001 PO 00000 Frm 00026 Revision— Fmt 4700 Sfmt 4700 E:\FR\FM\24FER1.SGM Dated— 02 02 02 24FER1 September 1, 2010. September 1, 2010. September 1, 2010. Federal Register / Vol. 76, No. 37 / Thursday, February 24, 2011 / Rules and Regulations Comments We gave the public the opportunity to participate in developing this AD. We considered the comment received. Support for the NPRM Delta stated that it agreed with the intent of the rule. jlentini on DSKJ8SOYB1PROD with RULES Request To Revise Compliance Times Delta requested that we revise the compliance time from within 3,600flight-hours to 10,000 flight hours or 24 months after the effective date of the AD to allow operators the flexibility to schedule the task during routine maintenance opportunities. Delta stated that revising the compliance times would be more congruous with AD 2008–06–25, Amendment 39–15437 (73 FR 14659). Delta stated that it reviewed its maintenance records for Model A330 airplanes, and it has not experienced a single failure of a hydraulic electric motor pump electrical connector in approximately 738,000 hours of operation. Furthermore, Delta stated that there have been no cases of fire as a result of arcing within the hydraulic electric motor pump connectors and that arcing within the connectors without the presence of flammable fluid does not constitute a safety issue. We do not agree with the commenter’s request to extend the compliance time. In developing an appropriate compliance time for this action, we considered the safety implications, parts availability, and normal maintenance schedules for the timely accomplishment of the modification. In consideration of these items, we have determined that a 3,600-flight-hour compliance time will ensure an acceptable level of safety and allow the modifications to be done during scheduled maintenance intervals for most affected operators. However, under the provisions of paragraph (i)(1) of the final rule, we will consider requests for approval of an extension of the compliance time if sufficient data are submitted to substantiate that the change would provide an acceptable level of safety. We have not changed the final rule in regard to this issue. Request To Include Reference for Additional Tooling Delta requested that we revise the NPRM to include Airbus Service Bulletin Information Telex (SBIT) 10– 0039, dated October 14, 2010, or that we delay issuing the final rule until Revision 03 of Airbus Mandatory Service Bulletin A330–92–3088 is released. Delta stated that Airbus has informed operators that Airbus Mandatory Service Bulletin A330–92– VerDate Mar<15>2010 16:10 Feb 23, 2011 Jkt 223001 3088 is being revised to include direct references to the adequate tool part numbers. We disagree with the request to include the SBIT and with the request to delay the final rule until Revision 03 of Airbus Mandatory Service Bulletin A330–92–3088 is released. Although the SBIT does contain tooling information, this AD does not mandate which tooling to use. We did not revise the final rule in this regard. Conclusion We reviewed the available data, including the comment 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 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. Costs of Compliance We estimate that this AD will affect 43 products of U.S. registry. We also estimate that it will take about 13 workhours per product to comply with the basic requirements of this AD. The average labor rate is $85 per work-hour. Required parts will cost about $877 per product. 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 $85,226 or $1,982 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: PO 00000 Frm 00027 Fmt 4700 Sfmt 4700 10231 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 https:// 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 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 Accordingly, under the authority delegated to me by the Administrator, E:\FR\FM\24FER1.SGM 24FER1 10232 Federal Register / Vol. 76, No. 37 / Thursday, February 24, 2011 / Rules and Regulations the FAA amends 14 CFR part 39 as follows: PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new AD: ■ 2011–05–05 Airbus: Amendment 39–16614. Docket No. FAA–2010–0859; Directorate Identifier 2010–NM–113–AD. Effective Date (a) This airworthiness directive (AD) becomes effective March 31, 2011. Applicability (c) This AD applies to the airplanes identified in paragraphs (c)(1) and (c)(2) of this AD. (1) Airbus Model A330–201, –202, –203, –223, –243, –301, –302, –303, –321, –322, –323, –341, –342, and –343 airplanes; certificated in any category; all serial numbers; except those on which Airbus modifications 58773 and 45968 have been embodied in production. (2) Airbus Model A340–211, –212, –213, –311, –312, –313, –541, and –642 airplanes; certificated in any category; all serial numbers; except those on which Airbus modifications 58773 and 45968 have been embodied in production. * * * [T]here is a possible path for fluid ingress, resulting in connector internal arcing and hydraulic system malfunction. In addition, as the connectors are located in areas adjacent to fuel tanks, such arcing associated with the presence of a fuel leakage could lead to an uncontrolled fire. Subject (d) Air Transport Association (ATA) of America Code 92. (g) Within 3,600 flight hours after the effective date of this AD, modify the hydraulic pump electrical motor connectors of the blue, yellow, and green electric pumps, in accordance with the Accomplishment Instructions of the applicable service information specified in Table 1 of this AD. Reason (e) The mandatory continuing airworthiness information (MCAI) states: Affected ADs * (b) None. * * * * * * * * 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. Actions * TABLE 1—APPLICABLE SERVICE INFORMATION Airplane model— Airbus Mandatory Service Bulletin— A330 ................. A340 ................. A340 ................. A330–92–3088 ............................................................................................................. A340–92–4081 ............................................................................................................. A340–92–5053 ............................................................................................................. Credit for Actions Accomplished in Accordance with Previous Issue of Service Information (h) Modifications accomplished before the effective date of this AD in accordance with Revision— Dated— 02 02 02 September 1, 2010. September 1, 2010. September 1, 2010. the service information specified in Table 2 of this AD are considered acceptable for compliance with the requirements of paragraph (g) of this AD. TABLE 2—CREDIT SERVICE INFORMATION Airplane model— Airbus Mandatory Service Bulletin— Revision— Dated— A330 A330 A340 A340 A340 A340 A330–92–3088 A330–92–3088 A340–92–4081 A340–92–4081 A340–92–5053 A340–92–5053 Original ....................................... 01 ................................................ Original ....................................... 01 ................................................ Original ....................................... 01 ................................................ September 2, 2009. February 22, 2010. September 2, 2009. February 22, 2010. September 2, 2009. February 22, 2010. ................. ................. ................. ................. ................. ................. ................................................................................ ................................................................................ ................................................................................ ................................................................................ ................................................................................ ................................................................................ FAA AD Differences jlentini on DSKJ8SOYB1PROD with RULES Note 1: This AD differs from the MCAI and/or service information as follows: No differences. Other FAA AD Provisions (i) 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. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International VerDate Mar<15>2010 16:10 Feb 23, 2011 Jkt 223001 Branch, send it 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. Information may be e-mailed to: 9-ANM-116-AMOCREQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding 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. PO 00000 Frm 00028 Fmt 4700 Sfmt 4700 Corrective actions are considered FAAapproved 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: A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120–0056. Public reporting for this collection of information is estimated to be approximately 5 minutes per response, E:\FR\FM\24FER1.SGM 24FER1 Federal Register / Vol. 76, No. 37 / Thursday, February 24, 2011 / Rules and Regulations including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW., Washington, DC 20591, Attn: Information Collection Clearance Officer, AES–200. 10233 Related Information (j) Refer to MCAI EASA Airworthiness Directive 2010–0086R1, dated June 16, 2010, and the service information specified in Table 3 of this AD, as applicable, for related information. TABLE 3—RELATED SERVICE INFORMATION Airplane model— Airbus Mandatory Service Bulletin— A330 ................. A340 ................. A340 ................. A330–92–3088, including Appendix 01 ........................................................................ A340–92–4081, including Appendix 01 ........................................................................ A340–92–5053, including Appendix 01 ........................................................................ Material Incorporated by Reference (k) You must use the service information contained in Table 4 of this AD, 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. Revision— (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 airworthiness.A330-A340@airbus.com; Internet https://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 Dated— 02 02 02 September 1, 2010. September 1, 2010. September 1, 2010. 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: https://www.archives.gov/federal_register/ code_of_federal_regulations/ibr_ locations.html. TABLE 4—MATERIAL INCORPORATED BY REFERENCE Airplane model— Airbus Mandatory Service Bulletin— A330 ................. A340 ................. A340 ................. A330–92–3088, including Appendix 01 ........................................................................ A340–92–4081, including Appendix 01 ........................................................................ A340–92–5053, including Appendix 01 ........................................................................ Issued in Renton, Washington, on February 14, 2011. Kalene C. Yanamura, Acting Manager, Transport Airplane Directorate, Aircraft Certification Service. [FR Doc. 2011–4041 Filed 2–23–11; 8:45 am] BILLING CODE 4910–13–P DELAWARE RIVER BASIN COMMISSION 18 CFR Part 420 Schedule of Water Charges Delaware River Basin Commission. ACTION: Final rule. AGENCY: By Resolution No. 2010–9 on September 15, 2010, the Delaware River Basin Commission (DRBC or ‘‘Commission’’) approved amendments to its Administrative Manual, Part III, Basin Regulations—Water Supply Charges. Accordingly, the Commission’s water charging rates for consumptive use and non-consumptive use, as codified, are hereby amended. DATES: Applicability date: This rule is applicable beginning January 1, 2011, to first quarter 2011 payments due by jlentini on DSKJ8SOYB1PROD with RULES SUMMARY: VerDate Mar<15>2010 16:10 Feb 23, 2011 Jkt 223001 Revision— April 30, 2011. Effective Date: February 24, 2011. FOR FURTHER INFORMATION CONTACT: For questions about the water charging program, please contact Ms. Amy Shallcross at 609–477–7201. SUPPLEMENTARY INFORMATION: The Delaware River Basin Commission is a state and federal compact agency charged with managing the water resources of the Delaware River Basin without regard to political boundaries. Its members are the governors of the four basin states—Delaware, New Jersey, New York, and Pennsylvania—and the North Atlantic Division Commander of the U.S. Army Corps of Engineers, representing the President of the United States and all Federal agencies. In order to fund certain water supply storage facility projects in the Basin, the Commission between 1964 and 1974 established a system of water supply charges consistent with section 3.7 of the Delaware River Basin Compact. DRBC Resolution No. 71–4 established a schedule of rates for water withdrawals and provided that ‘‘the charges for water supplied will include all costs associated with making basin water supply available and maintaining its continued availability in adequate PO 00000 Frm 00029 Fmt 4700 Sfmt 4700 Dated— 02 02 02 September 1, 2010. September 1, 2010. September 1, 2010. quantity and quality over time.’’ Res. No. 71–4, Apr. 7, 1971, par. A.2. Revenues from the sale of water in accordance with the rule are placed in a ‘‘Water Supply Storage Facilities Fund,’’ from which payments are made to meet the annual cost of the Commission’s water storage projects—including ‘‘debt service, operation, maintenance, replacement, reserves and associated administrative costs.’’ Id., par. A.2.b. The schedule of water charges in effect from 1978 through 2010 was established by Resolution No. 78–14 in October of 1978, based on the unit cost of water storage owned by the Commission in the Federal government’s Beltzville and Blue Marsh reservoirs. The rates established in 1978—$60 per million gallons for consumptive use and $.60 per million for non-consumptive use— remained unchanged for over 30 years. Notice of the proposed amendments appeared in the Federal Register on February 19, 2010 (75 FR 7411), as well as in the Delaware Register of Regulations on March 1, 2010 (13 DE Reg. 1144), the New Jersey Register on March 15, 2010 (42 N.J.R. 667(a)), the New York State Register on March 3, 2010 (p. 5) and the Pennsylvania Bulletin on March 6, 2010 (40 Pa. B. E:\FR\FM\24FER1.SGM 24FER1

Agencies

[Federal Register Volume 76, Number 37 (Thursday, February 24, 2011)]
[Rules and Regulations]
[Pages 10230-10233]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-4041]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-0859; Directorate Identifier 2010-NM-113-AD;
Amendment 39-16614; AD 2011-05-05]
RIN 2120-AA64

Airworthiness Directives; Airbus Model A330-200 and -300 Series
Airplanes and Model A340-200, -300, -500, and -600 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:
* * * * *

* * * [T]here is a possible path for fluid ingress, resulting in
connector internal arcing and hydraulic system malfunction. In
addition, as the connectors are located in areas adjacent to fuel
tanks, such arcing associated with the presence of a fuel leakage
could lead to an uncontrolled fire.
* * * * *
We are issuing this AD to require actions to correct the unsafe
condition on these products.

DATES: This AD becomes effective March 31, 2011.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of March 31,
2011.

ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov 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 September 29, 2010
(75 FR 60010). That NPRM proposed to correct an unsafe condition for
the specified products. The MCAI states:

Several A330 and A340 operators have reported in service
occurrences of hydraulic pump electrical motor connector internal
arcing, resulting in:

--Either false hydraulic system overheat Electronic Centralized
Aircraft Monitoring (ECAM) warnings
--and/or hydraulic pump electrical motor malfunction.

Investigations have shown that, due to the manufacturing
tolerances of the cables and the connectors rear grommet, there is a
possible path for fluid ingress, resulting in connector internal
arcing and hydraulic system malfunction. In addition, as the
connectors are located in areas adjacent to fuel tanks, such arcing
associated with the presence of a fuel leakage could lead to an
uncontrolled fire.
In order to protect the hydraulic pump electrical motor
connectors against fluid ingress from the rear of the connector
grommet and prevent false hydraulic system overheat ECAM warnings
and/or hydraulic pump electrical motor malfunction, this AD requires
modification of the three hydraulic pump electrical motor connectors
associated to the Blue, Yellow and Green hydraulic systems.
This Revision 1 is issued to delete Airbus modifications
55923S18878 and 55924S19452 from the applicability of this AD.

The modification adds heat shrink sleeves to certain cable contacts and
a sealing plug to the connector free cavity. You may obtain further
information by examining the MCAI in the AD docket.

Relevant Service Information

The NPRM referred to the service information in the following table
as the applicable sources of service information.

Table--Service Information Cited in the NPRM
----------------------------------------------------------------------------------------------------------------
Airbus Mandatory Service
Airplane model-- Bulletin-- Revision-- Dated--
----------------------------------------------------------------------------------------------------------------
A330........................... A330-92-3088, including 01 February 22, 2010.
Appendix 01.
A340........................... A340-92-4081, including 01 February 22, 2010.
Appendix 01.
A340........................... A340-92-5053, including 01 February 22, 2010.
Appendix 01.
----------------------------------------------------------------------------------------------------------------

Airbus has released the service information in the following table. No
additional work is necessary for airplanes on which earlier revisions
of the service information are done. We have updated Tables 1 and 3 of
the final rule to refer to these sources of service information. We
have also updated Table 2 of the final rule to give credit for using
Revision 01 of the service information.

Table--Revised Service Information
----------------------------------------------------------------------------------------------------------------
Airbus Mandatory Service
Airplane model-- Bulletin-- Revision-- Dated--
----------------------------------------------------------------------------------------------------------------
A330........................... A330-92-3088, including 02 September 1, 2010.
Appendix 01.
A340........................... A340-92-4081, including 02 September 1, 2010.
Appendix 01.
A340........................... A340-92-5053, including 02 September 1, 2010.
Appendix 01.
----------------------------------------------------------------------------------------------------------------

[[Page 10231]]

Comments

We gave the public the opportunity to participate in developing
this AD. We considered the comment received.

Support for the NPRM

Delta stated that it agreed with the intent of the rule.

Request To Revise Compliance Times

Delta requested that we revise the compliance time from within
3,600-flight-hours to 10,000 flight hours or 24 months after the
effective date of the AD to allow operators the flexibility to schedule
the task during routine maintenance opportunities. Delta stated that
revising the compliance times would be more congruous with AD 2008-06-
25, Amendment 39-15437 (73 FR 14659). Delta stated that it reviewed its
maintenance records for Model A330 airplanes, and it has not
experienced a single failure of a hydraulic electric motor pump
electrical connector in approximately 738,000 hours of operation.
Furthermore, Delta stated that there have been no cases of fire as a
result of arcing within the hydraulic electric motor pump connectors
and that arcing within the connectors without the presence of flammable
fluid does not constitute a safety issue.
We do not agree with the commenter's request to extend the
compliance time. In developing an appropriate compliance time for this
action, we considered the safety implications, parts availability, and
normal maintenance schedules for the timely accomplishment of the
modification. In consideration of these items, we have determined that
a 3,600-flight-hour compliance time will ensure an acceptable level of
safety and allow the modifications to be done during scheduled
maintenance intervals for most affected operators. However, under the
provisions of paragraph (i)(1) of the final rule, we will consider
requests for approval of an extension of the compliance time if
sufficient data are submitted to substantiate that the change would
provide an acceptable level of safety. We have not changed the final
rule in regard to this issue.

Request To Include Reference for Additional Tooling

Delta requested that we revise the NPRM to include Airbus Service
Bulletin Information Telex (SBIT) 10-0039, dated October 14, 2010, or
that we delay issuing the final rule until Revision 03 of Airbus
Mandatory Service Bulletin A330-92-3088 is released. Delta stated that
Airbus has informed operators that Airbus Mandatory Service Bulletin
A330-92-3088 is being revised to include direct references to the
adequate tool part numbers.
We disagree with the request to include the SBIT and with the
request to delay the final rule until Revision 03 of Airbus Mandatory
Service Bulletin A330-92-3088 is released. Although the SBIT does
contain tooling information, this AD does not mandate which tooling to
use. We did not revise the final rule in this regard.

Conclusion

We reviewed the available data, including the comment 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
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.

Costs of Compliance

We estimate that this AD will affect 43 products of U.S. registry.
We also estimate that it will take about 13 work-hours per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Required parts will cost about $877 per product.
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 $85,226 or $1,982 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 https://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 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

Accordingly, under the authority delegated to me by the
Administrator,

[[Page 10232]]

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:

2011-05-05 Airbus: Amendment 39-16614. Docket No. FAA-2010-0859;
Directorate Identifier 2010-NM-113-AD.

Effective Date

(a) This airworthiness directive (AD) becomes effective March
31, 2011.

Affected ADs

(b) None.

Applicability

(c) This AD applies to the airplanes identified in paragraphs
(c)(1) and (c)(2) of this AD.
(1) Airbus Model A330-201, -202, -203, -223, -243, -301, -302, -
303, -321, -322, -323, -341, -342, and -343 airplanes; certificated
in any category; all serial numbers; except those on which Airbus
modifications 58773 and 45968 have been embodied in production.
(2) Airbus Model A340-211, -212, -213, -311, -312, -313, -541,
and -642 airplanes; certificated in any category; all serial
numbers; except those on which Airbus modifications 58773 and 45968
have been embodied in production.

Subject

(d) Air Transport Association (ATA) of America Code 92.

Reason

(e) The mandatory continuing airworthiness information (MCAI)
states:
* * * * *
* * * [T]here is a possible path for fluid ingress, resulting in
connector internal arcing and hydraulic system malfunction. In
addition, as the connectors are located in areas adjacent to fuel
tanks, such arcing associated with the presence of a fuel leakage
could lead to an uncontrolled fire.
* * * * *

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.

Actions

(g) Within 3,600 flight hours after the effective date of this
AD, modify the hydraulic pump electrical motor connectors of the
blue, yellow, and green electric pumps, in accordance with the
Accomplishment Instructions of the applicable service information
specified in Table 1 of this AD.

Table 1--Applicable Service Information
----------------------------------------------------------------------------------------------------------------
Airbus Mandatory Service
Airplane model-- Bulletin-- Revision-- Dated--
----------------------------------------------------------------------------------------------------------------
A330........................... A330-92-3088............. 02 September 1, 2010.
A340........................... A340-92-4081............. 02 September 1, 2010.
A340........................... A340-92-5053............. 02 September 1, 2010.
----------------------------------------------------------------------------------------------------------------

Credit for Actions Accomplished in Accordance with Previous Issue of
Service Information

(h) Modifications accomplished before the effective date of this
AD in accordance with the service information specified in Table 2
of this AD are considered acceptable for compliance with the
requirements of paragraph (g) of this AD.

Table 2--Credit Service Information
----------------------------------------------------------------------------------------------------------------
Airbus Mandatory
Airplane model-- Service Bulletin-- Revision-- Dated--
----------------------------------------------------------------------------------------------------------------
A330........................ A330-92-3088........... Original.............. September 2, 2009.
A330........................ A330-92-3088........... 01.................... February 22, 2010.
A340........................ A340-92-4081........... Original.............. September 2, 2009.
A340........................ A340-92-4081........... 01.................... February 22, 2010.
A340........................ A340-92-5053........... Original.............. September 2, 2009.
A340........................ A340-92-5053........... 01.................... February 22, 2010.
----------------------------------------------------------------------------------------------------------------

FAA AD Differences

Note 1: This AD differs from the MCAI and/or service
information as follows: No differences.

Other FAA AD Provisions

(i) 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. In accordance with 14 CFR 39.19,
send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the manager of the International Branch, send it 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. Information may be e-mailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. Before using any approved AMOC, notify your
appropriate principal inspector, or lacking a principal inspector,
the manager of the local flight standards district office/
certificate holding 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: A federal agency may not conduct or
sponsor, and a person is not required to respond to, nor shall a
person be subject to a penalty for failure to comply with a
collection of information subject to the requirements of the
Paperwork Reduction Act unless that collection of information
displays a current valid OMB Control Number. The OMB Control Number
for this information collection is 2120-0056. Public reporting for
this collection of information is estimated to be approximately 5
minutes per response,

[[Page 10233]]

including the time for reviewing instructions, completing and
reviewing the collection of information. All responses to this
collection of information are mandatory. Comments concerning the
accuracy of this burden and suggestions for reducing the burden
should be directed to the FAA at: 800 Independence Ave. SW.,
Washington, DC 20591, Attn: Information Collection Clearance
Officer, AES-200.

Related Information

(j) Refer to MCAI EASA Airworthiness Directive 2010-0086R1,
dated June 16, 2010, and the service information specified in Table
3 of this AD, as applicable, for related information.

Table 3--Related Service Information
----------------------------------------------------------------------------------------------------------------
Airbus Mandatory Service
Airplane model-- Bulletin-- Revision-- Dated--
----------------------------------------------------------------------------------------------------------------
A330........................... A330-92-3088, including 02 September 1, 2010.
Appendix 01.
A340........................... A340-92-4081, including 02 September 1, 2010.
Appendix 01.
A340........................... A340-92-5053, including 02 September 1, 2010.
Appendix 01.
----------------------------------------------------------------------------------------------------------------

Material Incorporated by Reference

(k) You must use the service information contained in Table 4 of
this AD, 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 airworthiness.A330-A340@airbus.com;
Internet https://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: https://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.

Table 4--Material Incorporated by Reference
----------------------------------------------------------------------------------------------------------------
Airbus Mandatory Service
Airplane model-- Bulletin-- Revision-- Dated--
----------------------------------------------------------------------------------------------------------------
A330........................... A330-92-3088, including 02 September 1, 2010.
Appendix 01.
A340........................... A340-92-4081, including 02 September 1, 2010.
Appendix 01.
A340........................... A340-92-5053, including 02 September 1, 2010.
Appendix 01.
----------------------------------------------------------------------------------------------------------------

Issued in Renton, Washington, on February 14, 2011.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-4041 Filed 2-23-11; 8:45 am]
BILLING CODE 4910-13-P

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