AD 2011-06-09

[Federal Register Volume 76, Number 55 (Tuesday, March 22, 2011)]
[Rules and Regulations]
[Pages 15805-15808]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2011-5938]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2010-1162; Directorate Identifier 2010-NM-099-AD; 
Amendment 39-16634; AD 2011-06-09]
RIN 2120-AA64


Airworthiness Directives; Airbus Model A310 Series Airplanes, and 
Airbus Model A300 B4-600, B4-600R, and F4-600R Series Airplanes, and 
Model C4-605R Variant F Airplanes (Collectively Called A300-600 Series 
Airplanes)

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

ACTION: Final rule.

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SUMMARY: We are superseding an existing airworthiness directive (AD) 
that applies to 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:

    Prompted by a reported in-service event, EASA issued AD 2009-
0084 to prevent unwanted movement of pilot- or co-pilot seat in the 
horizontal direction which is considered as potentially unsafe, 
especially during the takeoff phase when the speed of the aeroplane 
is greater than 100 knots and until landing gear retraction.

* * * * *
Uncommanded movement of the pilot and co-pilot seats during takeoff or 
landing could interfere with the operation of the airplane and, as a 
result, could cause loss of control of the airplane. We are issuing 
this AD to require actions to correct the unsafe condition on these 
products.

DATES: This AD becomes effective April 26, 2011.
    The Director of the Federal Register approved the incorporation by 
reference of certain other publications listed in this AD as of April 
26, 2011.
    The Director of the Federal Register approved the incorporation by 
reference of certain other publications listed in this AD as of June 
12, 2009 (74 FR 25399, May 28, 2009).

ADDRESSES: You may examine the AD docket on the Internet at <a href="http://www.regulations.gov">http://www.regulations.gov</a> 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: Dan Rodina, Aerospace Engineer, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
1601 Lind Avenue, SW., Renton, Washington 98057-3356; phone: 425-227-
2125; 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 December 1, 2010 (75 
FR 74665), and proposed to supersede AD 2009-11-09, Amendment 39-15919 
(74 FR 25399, May 28, 2009). That NPRM proposed to correct an unsafe 
condition for the specified products. The MCAI states:

    Prompted by a reported in-service event, EASA issued AD 2009-
0084 [which corresponds to FAA AD 2009-11-09] to prevent unwanted 
movement of pilot- or co-pilot seat in the horizontal direction 
which is considered as potentially unsafe, especially during the 
takeoff phase when the speed of the aeroplane is greater than 100 
knots and until landing gear retraction.
    AD 2009-0084 required the deactivation of the electrical power 
of SOGERMA pilot seats P/N 2510112 series and co-pilot seats P/N 
2510113 series. Optional intermediate actions were also provided by 
AD 2009-0084 to allow partial or full restoration of seat adjustment 
functionality.
    Since AD 2009-0084 was issued, a permanent solution has been 
developed that terminates the de-activation requirement and 
invalidates the intermediate actions.
    Consequently, this AD retains requirements of EASA AD 2009-0084, 
which is superseded, and requires implementing the terminating 
action. In addition, this AD prohibits the (re)installation of 
unmodified pilot- and co-pilot seats on any aeroplane that has been 
modified in accordance with the requirements of this AD.

Uncommanded movement of the pilot and co-pilot seats during takeoff or 
landing could interfere with the operation of the airplane and, as a 
result, could cause loss of control of the airplane. You may obtain 
further information by examining the MCAI in the AD docket.

Relevant Service Information

    Since issuance of the NPRM, Airbus has issued Mandatory Service 
Bulletin A310-25-2205, Revision 01, dated November 19, 2010. This 
revision does not require any additional work. The actions described in 
this service information are intended to correct the unsafe condition 
identified in the MCAI. We have updated this final rule to refer to 
Airbus Mandatory Service Bulletin A310-25-2205, Revision 01, dated 
November 19, 2010. We added a new paragraph (n) of this AD to provide 
credit for doing actions before the effective date of this AD in 
accordance with Airbus Mandatory Service Bulletin A310-25-2205, dated 
August 31, 2009, for Airbus Model A310 series airplanes.

Comments

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

Conclusion

    We reviewed the available data, and determined that air safety and 
the public interest require adopting the AD with the changes described 
previously.

[[Page 15806]]

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

    Based on the service information, we estimate that this AD affects 
about 132 products of U.S. registry.
    The actions that are required by AD 2009-11-09 and retained in this 
AD take about 2 work-hours per product, at an average labor rate of $85 
per work hour. Based on these figures, the estimated cost of the 
currently required actions is $170 per product.
    We estimate that it would take about 2 work-hours per product to 
comply with the new basic requirements of this AD. The average labor 
rate is $85 per work-hour. Required parts would cost about $5,000 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 costs. 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 the AD on U.S. 
operators to be $704,880, or $5,340 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 <a href="http://www.regulations.gov">http://www.regulations.gov</a>; 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, 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 removing Amendment 39-15919 (74 FR 
25399, May 28, 2009) and adding the following new AD:

2011-06-09 Airbus: Amendment 39-16634. Docket No. FAA-2010-1162; 
Directorate Identifier 2010-NM-099-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective April 
26, 2011.

Affected ADs

    (b) This AD supersedes AD 2009-11-09, Amendment 39-15919.

Applicability

    (c) This AD applies to the airplanes identified in paragraphs 
(c)(1) and (c)(2) of this AD, certificated in any category; all 
serial numbers having SOGERMA 2510112 series pilot electrical seats 
or SOGERMA 2510113 series co-pilot electrical seats installed.
    (1) Airbus Model A300 B4-601, A300 B4-603, A300 B4-620, and A300 
B4-622, A300 B4-605R and A300 B4-622R; A300 F4-605R and A300 F4-
622R; and A300 C4-605R Variant F airplanes.
    (2) Airbus Model A310-203, -204, -221, -222, -304, -322, -324, 
and -325 airplanes.

Subject

    (d) Air Transport Association (ATA) of America Code 25: 
Equipment/Furnishings.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    Prompted by a reported in-service event, EASA issued AD 2009-
0084 to prevent unwanted movement of pilot or co-pilot seat in the 
horizontal direction which is considered as potentially unsafe, 
especially during the takeoff phase when the speed of the aeroplane 
is greater than 100 knots and until landing gear retraction.
* * * * *
Uncommanded movement of the pilot and co-pilot seats during takeoff 
or landing could interfere with the operation of the airplane and, 
as a result, could cause loss of control of the airplane.

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.

Restatement of Requirements of AD 2009-11-09, With No Changes

    (g) Within 15 days after June 12, 2009 (the effective date of AD 
2009-11-09): Deactivate the electrical supply of SOGERMA 2510112 
series pilot seats and SOGERMA 2510113 series co-pilot seats, in 
accordance with the instructions of Airbus All Operators Telex (AOT) 
A310-25A2203, Revision 02, dated March 2, 2009; or Airbus AOT A300-
25A6215, Revision 02, dated March 2, 2009; as applicable.
    (h) For optional intermediate action for restoration of the 
electrical adjustment of the vertical seat movement only: 
Deactivating the

[[Page 15807]]

electrical powered horizontal movement of SOGERMA 2510112 series 
pilot seats or SOGERMA 2510113 series co-pilot seats, in accordance 
with the instructions of EADS SOGERMA Alert Service Bulletin 
A2510112-25-764, Revision 1, dated February 17, 2009, allows 
restoration of the vertical adjustment only.
    (i) For optional intermediate action for restoration of the 
electrical adjustment of the vertical seat and horizontal seat 
movement: Inspecting the position of switch `S4' and the related 
shim of SOGERMA 2510112 series pilot seats or SOGERMA 2510113 series 
co-pilot seats, in accordance with EADS SOGERMA Inspection Service 
Bulletin 2510112-25-807, dated February 20, 2009, allows 
reactivation of both horizontal and vertical electrical movements, 
provided the measurement results of the inspection are within the 
acceptable value indicated in that service bulletin, and provided 
that the inspection is repeated thereafter at intervals not to 
exceed 2 months. If the measurement result of any inspection is not 
within the acceptable value indicated in EADS SOGERMA Inspection 
Service Bulletin 2510112-25-807, dated February 20, 2009, the 
horizontal movement must be deactivated before further flight.
    (j) At the applicable time specified in paragraph (j)(1) or 
(j)(2) of this AD: Submit a report of the findings for the first 
inspection done in accordance with paragraph (i) of this AD to 
Airbus SAS-EAW (Airworthiness Office), 1 Rond Point Maurice 
Bellonte, 31707 Blagnac Cedex, France. The report must include a 
detailed fleet inspection report, including measurement values, and 
pin and serial numbers for each seat.
    (1) If the inspection was done on or after June 12, 2009: Submit 
the report within 30 days after the inspection.
    (2) If the inspection was accomplished prior to June 12, 2009: 
Submit the report within 30 days after June 12, 2009.
    (k) Modifications made prior to June 12, 2009, in accordance 
with EADS SOGERMA Alert Service Bulletin A2510112-25-764, dated 
December 19, 2008, are considered acceptable for compliance with the 
applicable action specified in this AD.

New Requirements of This AD

    (l) Within 12 months after the effective date of this AD: 
Install an enlarged shim for the horizontal switch actuation on each 
affected seat, in accordance with the Accomplishment Instructions of 
Airbus Mandatory Service Bulletin A300-25-6217, dated August 31, 
2009 (for Model A300-600 series airplanes) or A310-25-2205, Revision 
01, dated November 19, 2010 (for Model A310 series airplanes). Doing 
the installation required by paragraph (l) of this AD terminates the 
requirements of paragraphs (g), (h), and (i) of this AD.
    (m) As of the effective date of this AD, no person may install 
any SOGERMA 2510112 series pilot seat or SOGERMA 2510113 series co-
pilot seat, on any airplane, unless that seat has been modified in 
accordance with the Accomplishment Instructions of Airbus Mandatory 
Service Bulletin A300-25-6217, dated August 31, 2009 (for Model 
A300-600 series airplanes) or A310-25-2205, Revision 01, dated 
November 19, 2010 (for Model A310 series airplanes).
    (n) Actions accomplished before the effective date of this AD 
according to Airbus Mandatory Service Bulletin A310-25-2205, dated 
August 31, 2009 (for Model A310 airplanes), are considered 
acceptable for compliance with the corresponding actions required by 
paragraphs (l) and (m) of this AD.

FAA AD Differences

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

Other FAA AD Provisions

    (o) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Branch, ANM-116, Transport Airplane Directorate, FAA, 
has the authority to approve AMOCs for this AD, if requested using 
the procedures found in 14 CFR 39.19. 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: Dan Rodina, Aerospace Engineer, International Branch, ANM-116, 
Transport Airplane Directorate, FAA, 1601 Lind Avenue, SW., Renton, 
Washington 98057-3356; phone: 425-227-2125; fax: 425-227-1149. 
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, 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

    (p) Refer to MCAI European Aviation Safety Agency (EASA) 
Airworthiness Directive 2010-0070, dated April 14, 2010, and the 
service information specified in table 1 of this AD, for related 
information.

                  Table 1--Related Service Information
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            Document                 Revision               Date
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Airbus All Operators Telex A300- 02..............  March 2, 2009.
 25A6215.
Airbus All Operators Telex A310- 02..............  March 2, 2009.
 25A2203.
Airbus Mandatory Service         Original........  August 31, 2009.
 Bulletin A300-25-6217.
Airbus Mandatory Service         01..............  November 19, 2010.
 Bulletin A310-25-2205.
EADS SOGERMA Alert Service       1...............  February 17, 2009.
 Bulletin A2510112-25-764.
EADS SOGERMA Inspection Service  Original........  February 20, 2009.
 Bulletin 2510112-25-807.
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Material Incorporated by Reference

    (q) You must use the service information contained in table 2 of 
this AD to do the actions required by this AD, unless the AD 
specifies otherwise. If you do the optional actions specified in 
this AD, you must use EADS SOGERMA Alert Service Bulletin A2510112-
25-764, Revision 1, dated February 17, 2009; or EADS SOGERMA 
Inspection Service Bulletin 2510112-25-807, dated February 20, 2009; 
as applicable; to perform those actions, unless the AD specifies 
otherwise.

[[Page 15808]]



                      Table 2--All Material Incorporated by Reference for Required Actions
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                Document                           Revision                              Date
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Airbus All Operators Telex A300-25A6215.  02.......................  March 2, 2009.
Airbus All Operators Telex A310-25A2203.  02.......................  March 2, 2009.
Airbus Mandatory Service Bulletin A300-   Original.................  August 31, 2009.
 25-6217.
Airbus Mandatory Service Bulletin A310-   01.......................  November 19, 2010.
 25-2205.
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     (1) The Director of the Federal Register approved the 
incorporation by reference of Airbus Mandatory Service Bulletin 
A300-25-6217, dated August 31, 2009; and Airbus Mandatory Service 
Bulletin A310-25-2205, Revision 01, dated November 19, 2010; under 5 
U.S.C. 552(a) and 1 CFR part 51.
    (2) The Director of the Federal Register previously approved the 
incorporation by reference of the service information contained in 
table 3 of this AD on June 12, 2009 (74 FR 25399, May 28, 2009).

                             Table 3--Material Previously Incorporated by Reference
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                Document                           Revision                              Date
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Airbus All Operators Telex A300-25A6215.  02.......................  March 2, 2009.
Airbus All Operators Telex A310-25A2203.  02.......................  March 2, 2009.
EADS SOGERMA Alert Service Bulletin       1........................  February 17, 2009.
 A2510112-25-764.
EADS SOGERMA Inspection Service Bulletin  Original.................  February 20, 2009.
 2510112-25-807.
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     (3) For Airbus service information identified in this AD, 
contact Airbus SAS--EAW (Airworthiness Office), 1 Rond Point Maurice 
Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; 
fax +33 5 61 93 44 51; e-mail: <a href="/cdn-cgi/l/email-protection#472624242832293369262e35302835332f6a22263407262e352532346924282a"><span class="__cf_email__" data-cfemail="107173737f657e643e717962677f6264783d757163507179627265633e737f7d">[email&#160;protected]</span></a>; 
Internet <a href="http://www.airbus.com">http://www.airbus.com</a>.
    (4) For EADS SOGERMA service information identified in this AD, 
contact EADS SOGERMA, Zone Industrielle de l'Arsenal, BP 60109, 
17303 Rochefort, Cedex France; phone: 33 5 49 82 84 84; fax: 33 5 46 
82 88 13; e-mail: <a href="/cdn-cgi/l/email-protection#7122323e354031021e1614031c105f141015025f1f1405"><span class="__cf_email__" data-cfemail="aefdede1ea9feeddc1c9cbdcc3cf80cbcfcadd80c0cbda">[email&#160;protected]</span></a>; Internet: <a href="http://www.sogerma.eads.net">http://www.sogerma.eads.net</a>.
    (5) 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.
    (6) 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: <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 March 7, 2011.
Kalene C. Yanamura,
Acting Manager, Transport Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2011-5938 Filed 3-21-11; 8:45 am]
BILLING CODE 4910-13-P