AD 2006-12-05

[Federal Register Volume 71, Number 109 (Wednesday, June 7, 2006)]
[Rules and Regulations]
[Pages 32815-32818]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 06-5122]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2006-24200; Directorate Identifier 2006-NM-012-AD; 
Amendment 39-14630; AD 2006-12-05]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A300 B4 Series Airplanes; 
Model A300 B4-600 Series Airplanes; Model A300 C4-605R Variant F 
Airplanes; Model A310-200 Series Airplanes; and Model A310-300 Series 
Airplanes

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

ACTION: Final rule.

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SUMMARY: The FAA is superseding an existing airworthiness directive 
(AD), which applies to certain Airbus Model A300 B4-600 and A300 C4-600 
series airplanes. That AD currently requires a one-time inspection to 
detect damage of the pump diffuser guide slots (bayonet) of the center 
tank fuel pumps, the pump diffuser housings, and the pump canisters; 
repetitive inspections to detect damage of the fuel pumps and the fuel 
pump canisters; and corrective action, if necessary. This new AD adds, 
for new airplanes, repetitive inspections of the pump bodies for 
cracking, damage, and missing and broken fasteners; repetitive 
inspections of the fuel pump canisters for a cracked flange web; and 
corrective actions if necessary. For all airplanes, this new AD also 
adds replacement of the fuel pump canisters with new reinforced fuel 
pump canisters, which ends the repetitive inspections. This AD results 
from fuel system reviews conducted by the manufacturer. We are issuing 
this AD to detect and correct damage of the center tank fuel pumps and 
fuel pump canisters, which could result in separation of a pump from 
its electrical motor housing, loss of flame trap capability, and a 
possible fuel ignition source in the center fuel tank.

DATES: This AD becomes effective July 12, 2006.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in the AD as of July 12, 2006.
    On May 19, 2004 (69 FR 19756, April 14, 2004), the Director of the 
Federal Register approved the incorporation by reference of Airbus All 
Operators Telex A300-600-28A6075, dated February 20, 2003.

ADDRESSES: You may examine the AD docket on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> 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.

FOR FURTHER INFORMATION CONTACT: Thomas Stafford, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98055-4056; telephone (425) 
227-1622; fax (425) 227-1149.

SUPPLEMENTARY INFORMATION:

Examining the Docket

    You may examine the airworthiness directive (AD) docket on the 
Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a> 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 supersedes AD 2004-08-03, amendment 
39-13572 (69 FR 19756, April 14, 2004). The existing AD applies to 
certain Airbus Model A300 B4-600 and A300 C4-600 series airplanes. That 
NPRM was published in the Federal Register on March 27, 2006 (71 FR 
15079). That NPRM proposed to require a one-time inspection to detect 
damage of the pump diffuser guide slots (bayonet) of the center tank 
fuel pumps, the pump diffuser housings, and the pump canisters; 
repetitive inspections to detect damage of the fuel pumps and the fuel 
pump canisters; and corrective action, if necessary. That NPRM proposed 
to add, for new airplanes, repetitive inspections of the pump

[[Page 32816]]

bodies for cracking, damage, and missing and broken fasteners; 
repetitive inspections of the fuel pump canisters for a cracked flange 
web; and corrective actions if necessary. For all airplanes, that NPRM 
also proposed to add replacement of the fuel pump canisters with new 
reinforced fuel pump canisters, which ends the repetitive inspections.

Comments

    We provided the public the opportunity to participate in the 
development of this AD. No comments have been received 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 will affect about 74 airplanes of U.S. registry. The 
following table provides the estimated costs, at an average labor rate 
of $80 per hour, for U.S. operators to comply with this AD.

                                                                     Estimated Costs
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                                                                                                                    Number U.S.-
            Airbus Model--                      Action            Work hours     Parts        Cost per airplane      registered         Fleet cost
                                                                                                                     airplanes
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A300 B4-600 series airplanes and       Detailed inspection                 2         None  $160...................            2  $320.
 Model A300 C4-605R Variant F           (required by AD 2004-08-
 airplanes.                             03).
                                       Eddy current inspection             5         None  $400, per inspection               2  $800, per inspection
                                        (required by AD 2004-08-                            cycle.                                cycle.
                                        03).
                                       Replacements (new                   7          $70  $630...................            2  1,260.
                                        action).
A300 B4 series airplanes.............  Repetitive inspection               2         None  $160, per inspection              16  $2,560, per inspection
                                        (new action).                                       cycle.                                cycle.
                                       Replacements (new                  10          $80  $880...................           16  $14,080.
                                        action).
A310-200 and -300 series airplanes...  Repetitive inspection               2         None  $160, per inspection              56  $8,960, per inspection
                                        (new action).                                       cycle.                                cycle.
                                       Replacements (new                  10          $50  $850...................           56  $47,600.
                                        action).
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runAuthority 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.

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 Federal Aviation Administration (FAA) amends Sec.  39.13 by 
removing amendment 39-13572 (69 FR 19756, April 14, 2004) and by adding 
the following new airworthiness directive (AD):

2006-12-05 Airbus: Amendment 39-14630. Docket No. FAA-2006-24200; 
Directorate Identifier 2006-NM-012-AD.

Effective Date

    (a) This AD becomes effective July 12, 2006.

Affected ADs

    (b) This AD supersedes AD 2004-08-03.

Applicability

    (c) This AD applies to the Airbus airplanes identified in 
paragraphs (c)(1) and (c)(2) of this AD, certificated in any 
category.
    (1) Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes; and 
Model A300 C4-605R Variant F airplanes; except those airplanes 
equipped with a fuel trim tank system (that have incorporated Airbus 
Modification 4801).

[[Page 32817]]

    (2) All Model A300 B4-2C, B4-103, and B4-203 airplanes; Model 
A310-203, -204, -221, and -222 airplanes; and Model A310-304, -322, 
-324, and -325 airplanes.

Unsafe Condition

    (d) This AD results from fuel system reviews conducted by the 
manufacturer. We are issuing this AD to detect and correct damage of 
the center tank fuel pumps and fuel pump canisters, which could 
result in separation of a pump from its electrical motor housing, 
loss of flame trap capability, and a possible fuel ignition source 
in the center 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.

Restatement of Requirements of AD 2004-08-03

Detailed Inspections

    (f) For Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes 
and Model A300 C4-605R Variant F airplanes: Within 15 days after May 
19, 2004 (the effective date of AD 2004-08-03) (unless accomplished 
previously), perform detailed inspections as specified in paragraphs 
(f)(1) and (f)(2) of this AD, in accordance with paragraph 4.2 of 
Airbus All Operators Telex (AOT) A300-600-28A6075, dated February 
20, 2003; or Revision 01, dated October 24, 2005.

    Note 1: For the purposes of this AD, a detailed inspection is: 
``An intensive examination of a specific item, installation, or 
assembly to detect damage, failure, or irregularity. Available 
lighting is normally supplemented with a direct source of good 
lighting at an intensity deemed appropriate. Inspection aids such as 
mirror, magnifying lenses, etc., may be necessary. Surface cleaning 
and elaborate procedures may be required.''

    (1) Inspect the lower part of the pump diffuser guide slots 
(bayonet) of the center tank fuel pumps and the bottom of the pump 
diffuser housings to detect cracks, fretting, and other damage. 
Replace any damaged pump and the corresponding fuel pump canister 
with new parts before further flight in accordance with the AOT.
    (2) Inspect the center tank fuel pump canisters to detect 
cracks. Replace any cracked fuel pump canister and the corresponding 
fuel pump with new parts before further flight in accordance with 
the AOT.

Repetitive Inspections With New Repetitive Intervals

    (g) For Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes 
and Model A300 C4-605R Variant F airplanes: Within 600 flight hours 
after May 19, 2004, perform a detailed inspection of the fuel pumps, 
and an eddy current inspection of the fuel pump canisters, to detect 
damage. Do the inspections in accordance with paragraph 4.3 of 
Airbus AOT A300-600-28A6075, dated February 20, 2003; or Revision 
01, dated October 24, 2005. Replace any damaged part with a new part 
before further flight in accordance with the AOT. Repeat the 
inspections at intervals not to exceed 3,000 flight cycles.
    (h) For Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes 
and Model A300 C4-605R Variant F airplanes: Within 7,000 flight 
cycles after canister replacement as specified in paragraph (g) of 
this AD, perform an eddy current inspection of the fuel pump 
canisters to detect damage in accordance with Airbus AOT A300-600-
28A6075, dated February 20, 2003; or Revision 01, dated October 24, 
2005. Replace any damaged part with a new part before further flight 
in accordance with the AOT. Thereafter repeat the inspection at 
intervals not to exceed 3,000 flight cycles.

    Note 2: Airbus AOT A300-600-28A6075 refers to Airbus Alert 
Service Bulletin A300-28A6061, Revision 04, dated August 1, 2002, as 
an additional source of service information for accomplishment of 
the eddy current inspection required by paragraphs (g) and (h) of 
this AD.

Reporting Requirement

    (i) For Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes 
and Model A300 C4-605R Variant F airplanes: At the applicable time 
specified in paragraph (i)(1) or (i)(2) of this AD, submit a report 
of findings (both positive and negative) of each inspection required 
by this AD, in accordance with Airbus AOT A300-600-28A6075, dated 
February 20, 2003. Information collection requirements contained in 
this AD have been approved by the Office of Management and Budget 
(OMB) under the provisions of the Paperwork Reduction Act of 1980 
(44 U.S.C. 3501 et seq.) and have been assigned OMB Control Number 
2120-0056.
    (1) For any inspection accomplished after May 19, 2004: Submit 
the report within 10 days after performing that inspection.
    (2) For any inspection accomplished before May 19, 2004: Submit 
the report within 10 days after May 19, 2004.

Requirements of This AD

Repetitive Inspections for New Airplanes

    (j) For Model A300 B4-2C, B4-103, and B4-203 airplanes; Model 
A310-203, -204, -221, and -222 airplanes; and Model A310-304, -322, 
-324, and -325 airplanes: At the applicable compliance time 
specified in paragraphs (j)(1) and (j)(2) of this AD, do a detailed 
inspection of the pump bodies for cracking, damage, and missing and 
broken fasteners; and do a high frequency eddy current (HFEC) 
inspection of the fuel pump canisters for a cracked flange web, in 
accordance with the Accomplishment Instructions of Airbus Service 
Bulletin A300-28-0084, excluding Appendix 01, dated June 28, 2005 
(for Model A300 B4-2C, B4-103, and B4-203 airplanes); or Airbus 
Service Bulletin A310-28-2159, excluding Appendix 01, dated June 28, 
2005 (for Model A310-203, -204, -221, and -222 airplanes and Model 
A310-304, -322, -324, and -325 airplanes), as applicable. If any 
crack or damage to the pump bodies is found or any missing or broken 
fastener is found, before further flight, replace the fuel pump with 
a new fuel pump in accordance with the applicable service bulletin. 
Repeat the detailed inspection of the pump bodies thereafter at 
intervals not to exceed 3,000 flight cycles. If no cracked flange 
web is found, repeat the HFEC inspection of the fuel pump canisters 
thereafter at intervals not to exceed 3,000 flight cycles. 
Accomplishing the replacements specified in paragraph (1) of this AD 
terminates the repetitive detailed and HFEC inspections.
    (1) For Model A300 B4-2C, B4-103, and B4-203 airplanes: Inspect 
before the airplane has accumulated 19,600 total flight cycles, or 
within 1,000 flight cycles after the effective date of this AD, 
whichever is later.
    (2) For Model A310-203, -204, -221, and -222 airplanes and Model 
A310-304, -322, -324, and -325 airplanes: Inspect before the 
airplane has accumulated 27,000 total flight cycles, or within 1,000 
flight cycles after the effective date of this AD, whichever is 
later.

Corrective Action for Cracked Flange Web

    (k) For Model A300 B4-2C, B4-103, and B4-203; Model A310-203, -
204, -221, and -222 airplanes; and Model A310-304, -322, -324, and -
325 airplanes: If any flange web is found cracked during any HFEC 
inspection required by paragraph (j) of this AD, before further 
flight after the inspection, replace the fuel pump canister with a 
new fuel pump canister in accordance with the Accomplishment 
Instructions of Airbus Service Bulletin A300-28-0084, dated June 28, 
2005; or Airbus Service Bulletin A310-28-2159, dated June 28, 2005, 
as applicable. Repeat the HFEC inspection at the applicable 
compliance times specified in paragraph (k)(1) or (k)(2) of this AD, 
until the replacements specified in paragraph (l) of this AD are 
accomplished.
    (1) For Model A300 B4-2C, B4-103, and B4-203 airplanes: Inspect 
within 19,600 flight cycles after replacing the fuel pump canisters 
and thereafter at intervals not to exceed 3,000 flight cycles.
    (2) For Model A310-203, -204, -221, and -222 airplanes and Model 
A310-304, -322, -324, and -325 airplanes: Inspect within 27,000 
flight cycles after replacing the fuel pump canisters and thereafter 
at intervals not to exceed 3,000 flight cycles.

Terminating Action: Replacement of Fuel Pump Canisters

    (1) For all airplanes: Within 66 months after the effective date 
of this AD, replace the fuel pump canisters with new reinforced fuel 
pump canisters, in accordance with the Accomplishment Instructions 
of Airbus Service Bulletin A300-28-0085, dated July 18, 2005 (for 
Model A300 B4-2C, B4-103, and B4-203 airplanes); Airbus Service 
Bulletin A300-28-6089, Revision 01, dated November 28, 2005 (for 
Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes and Model 
A300 C4-605R Variant F airplanes); or Airbus Service Bulletin A310-
28-2160, dated July 18, 2005 (for Model A310-203, -204, -221, and -
222 airplanes and Model A310-304, -322, -324, and -325 airplanes), 
as applicable. Replacement of a fuel pump canister terminates the 
repetitive inspections required by paragraphs (f), (g), (h), (j) and 
(k), as applicable, for that fuel pump canister only.

[[Page 32818]]

Credit for Previous Service Bulletin

    (m) For Model A300 B4-601, B4-603, B4-620, and B4-622 airplanes 
and Model A300 C4-605R Variant F airplanes: Actions done before the 
effective date of this AD in accordance with Airbus Service Bulletin 
A300-28-6089, dated July 18, 2005, are acceptable for compliance 
with the requirements of paragraph (l) of this AD.

Alternative Methods of Compliance (AMOCs)

    (n)(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 Sec.  
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

    (o) French airworthiness directive F-2005-199, dated December 7, 
2005, also addresses the subject of this AD.

Material Incorporated by Reference

    (p) You must use the Airbus service information identified in 
Table 1 of this AD to perform the actions that are required by this 
AD, as applicable, unless the AD specifies otherwise.

                                  Table 1.--Material Incorporated by Reference
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        Airbus service information                 Revision level                           Date
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All Operators Telex A300-600-28A6075.....  Original......................  February 20, 2003.
All Operators Telex A300-28A6075.........  01............................  October 24, 2005.
Service Bulletin A300-28-0084, excluding   Original......................  June 28, 2005.
 Appendix 01.
Service Bulletin A300-28-0085............  Original......................  July 18, 2005.
Service Bulletin A300-28-6089............  01............................  November 28, 2005.
Service Bulletin A310-28-2159, excluding   Original......................  June 28, 2005.
 Appendix 01.
Service Bulletin A310-28-2160............  Original......................  July 18, 2005.
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    (1) The Director of the Federal Register approved the 
incorporation by reference of the Airbus service information 
identified in Table 2 of this AD in accordance with 5 U.S.C. 552(a) 
and 1 CFR part 51.

                                Table 2.--New Material Incorporated by Reference
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        Airbus service information                 Revision level                           Date
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All Operators Telex A300-28A6075.........  01............................  October 24, 2005.
Service Bulletin A300-28-0084, excluding   Original......................  June 28, 2005.
 Appendix 01.
Service Bulletin A300-28-0085............  Original......................  July 18, 2005.
Service Bulletin A300-28-6089............  01............................  November 28, 2005.
Service Bulletin A310-28-2159, excluding   Original......................  June 28, 2005.
 Appendix 01.
Service Bulletin A310-28-2160............  Original......................  July 18, 2005.
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(Only the first page of Airbus All Operators Telex A300-28A6075, 
Revision 01, dated October 24, 2005, contains the document number 
and issue date; no other page of this document contains this 
information.)

    (2) On May 19, 2004 (69 FR 19756, April 14, 2004), the Director 
of the Federal Register approved the incorporation by reference of 
Airbus All Operators Telex A300-600-28A6075, dated February 20, 
2003.
    (3) Contact Airbus, 1 Rond Point Maurice Bellonte, 31707 Blagnac 
Cedex, France, for a copy of this service information. You may 
review copies at the Docket Management Facility, U.S. Department of 
Transportation, 400 Seventh Street, SW., Room PL-401, Nassif 
Building, Washington, DC; on the Internet at <a href="http://dms.dot.gov">http://dms.dot.gov</a>; or 
at the National Archives and Records Administration (NARA). For 
information on the availability of this material at the NARA, call 
(202) 741-6030, or go to <a href="http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html">http://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html</a>.

    Issued in Renton, Washington, on May 30, 2006.
Jeffrey E. Duven,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 06-5122 Filed 6-6-06; 8:45 am]
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