
[Federal Register Volume 76, Number 204 (Friday, October 21, 2011)]
[Proposed Rules]
[Pages 65419-65421]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-27264]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2011-1139; Directorate Identifier 2011-CE-021-AD]
RIN 2120-AA64


Airworthiness Directives; SOCATA Airplanes

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

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: We propose to adopt a new airworthiness directive (AD) for 
SOCATA Model TBM 700 airplanes. This proposed 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:

    A TBM 700 operator reported a case of inverted installation of 
aileron control cables in the wing. The shortest cable was found 
installed instead of the longest one on wing tip side, with left 
hand (LH) threaded end in upper section. This wrong installation 
could have been caused by mistaken maintenance data.
    This condition, if not detected and corrected, could lead to 
restricted movement of the aileron, resulting in reduced control of 
the aeroplane, particularly when operating under adverse flight 
conditions on landing and during avoidance manoeuvres.

    The proposed AD would require actions that are intended to address 
the unsafe condition described in the MCAI.

DATES: We must receive comments on this proposed AD by December 5, 
2011.

ADDRESSES: You may send comments by any of the following methods:
     Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: (202) 493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue, SE., Washington, DC 20590.
     Hand Delivery: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue, SE., Washington, DC 20590, between 9 a.m. and 5 p.m., 
Monday through Friday, except Federal holidays.
    For service information identified in this proposed AD, contact 
SOCATA--Direction des Services--65921 Tarbes Cedex 9--France; telephone 
+33 (0) 62 41 7300, fax +33 (0) 62 41 76 54, or for North America: 
SOCATA NORTH AMERICA, 7501 South Airport Road, North Perry Airport 
(HWO), Pembroke Pines, Florida 33023; telephone: (954) 893-1400; fax: 
(954) 964-4141; e-mail: mysocata@socata.daher.com; Internet: http://mysocata.com. You may review copies of the referenced service 
information at the FAA, Small Airplane Directorate, 901 Locust, Kansas 
City, Missouri 64106. For information on the availability of this 
material at the FAA, call (816) 329-4148.

Examining the AD Docket

    You may examine the AD docket on the Internet at http://www.regulations.gov; or in person at the Docket Management Facility 
between 9 a.m. and 5 p.m., Monday through Friday, except Federal 
holidays. The AD docket contains this proposed AD, the regulatory 
evaluation, any comments received, and other information. The street 
address for the Docket Office (telephone (800) 647-5527) is in the 
ADDRESSES section. Comments will be available in the AD docket shortly 
after receipt.

[[Page 65420]]


FOR FURTHER INFORMATION CONTACT: Albert Mercado, Aerospace Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090; e-mail: 
albert.mercado@faa.gov.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    We invite you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES section. Include ``Docket No. FAA-2011-1139; 
Directorate Identifier 2011-CE-021-AD'' at the beginning of your 
comments. We specifically invite comments on the overall regulatory, 
economic, environmental, and energy aspects of this proposed AD. We 
will consider all comments received by the closing date and may amend 
this proposed AD because of those comments.
    We will post all comments we receive, without change, to http://regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this proposed AD.

Discussion

    The European Aviation Safety Agency (EASA), which is the Technical 
Agent for the Member States of the European Community, has issued EASA 
AD No.: 2011-0101, dated May 25, 2011 (referred to after this as ``the 
MCAI''), to correct an unsafe condition for the specified products. The 
MCAI states:

    A TBM 700 operator reported a case of inverted installation of 
aileron control cables in the wing. The shortest cable was found 
installed instead of the longest one on wing tip side, with left 
hand (LH) threaded end in upper section. This wrong installation 
could have been caused by mistaken maintenance data.
    This condition, if not detected and corrected, could lead to 
restricted movement of the aileron, resulting in reduced control of 
the aeroplane, particularly when operating under adverse flight 
conditions on landing and during avoidance manoeuvres.
    For the reasons described above, this AD requires an inspection 
to verify the correct installation of the aileron control cables 
and, in case of discrepancies, proper re-installation of the cables 
in accordance with the approved design configuration.

    You may obtain further information by examining the MCAI in the AD 
docket.
    Even with potentially reduced aileron deflection, Socata's analysis 
shows that the airplane is still capable of achieving its published 
cross wind landing limits.

Relevant Service Information

    DAHER-SOCATA has issued Mandatory Service Bulletin SB 70-191-27, 
dated April 2011; SOCATA TBM 700 Model Maintenance Manual Temporary 
Revision No. TR040.27, dated April 2011; and SOCATA TBM 850 Maintenance 
Manual Temporary Revision No. TR015.27, dated April 2011. The actions 
described in this service information are intended to correct the 
unsafe condition identified in the MCAI.

FAA's Determination and Requirements of the Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to our bilateral agreement with this State of Design Authority, they 
have notified us of the unsafe condition described in the MCAI and 
service information referenced above. We are proposing this AD because 
we evaluated all information and determined the unsafe condition exists 
and is likely to exist or develop on other products of the same type 
design.

Differences Between This Proposed 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 proposed different actions in this AD from those 
in the MCAI in order to follow FAA policies. Any such differences are 
highlighted in a Note within the proposed AD.

Costs of Compliance

    We estimate that this proposed AD will affect 404 products of U.S. 
registry. We also estimate that it would take about .5 work-hour per 
product to comply with the basic requirements of this proposed AD. The 
average labor rate is $85 per work-hour. Required parts would cost 
about $0 per product.
    Based on these figures, we estimate the cost of the proposed AD on 
U.S. operators to be $17,170, or $43 per product.
    In addition, we estimate that any necessary follow-on actions would 
take about 16 work-hours and require parts costing $0, for a cost of 
$1,360 per product. We have no way of determining the number of 
products that may need these actions.
    According to the manufacturer, some of the costs of this proposed 
AD may be covered under warranty, thereby reducing the cost impact on 
affected individuals. We do not control warranty coverage for affected 
individuals. As a result, we have included all costs in our cost 
estimate.

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 proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 proposed 
regulation:
    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 proposed AD and placed it in the AD docket.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

[[Page 65421]]

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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.


Sec.  39.13  [Amended]

    2. The FAA amends Sec.  39.13 by adding the following new AD:

SOCATA: Docket No. FAA-2011-1139; Directorate Identifier 2011-CE-
021-AD.

Comments Due Date

    (a) We must receive comments by December 5, 2011.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to SOCATA Model TBM 700 airplanes, serial 
numbers (SN) 1 through 572, 574, and 576, certificated in any 
category.

Subject

    (d) Air Transport Association of America (ATA) Code 27: Flight 
Controls.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:
    A TBM 700 operator reported a case of inverted installation of 
aileron control cables in the wing. The shortest cable was found 
installed instead of the longest one on wing tip side, with left 
hand (LH) threaded end in upper section. This wrong installation 
could have been caused by mistaken maintenance data.
    This condition, if not detected and corrected, could lead to 
restricted movement of the aileron, resulting in reduced control of 
the aeroplane, particularly when operating under adverse flight 
conditions on landing and during avoidance manoeuvres.
    For the reasons described above, this AD requires an inspection 
to verify the correct installation of the aileron control cables 
and, in case of discrepancies, proper re-installation of the cables 
in accordance with the approved design configuration.
    Even with potentially reduced aileron deflection, Socata's 
analysis shows that the airplane is still capable of achieving its 
published cross wind landing limits.

Actions and Compliance

    (f) Unless already done, do the following actions:
    (1) Within 12 months after the effective date of this AD or 
within 100 hours time-in-service (TIS) after the effective date of 
this AD, whichever occurs first, inspect the aileron control cables 
in left and right wings for proper installation following the 
accomplishment instructions of DAHER-SOCATA Mandatory Service 
Bulletin SB 70-191-27, dated April 2011.
    (2) If during the inspection required by paragraph (f)(1) of 
this AD you find the cables are improperly installed, before further 
flight, remove the cables and correctly re-install the cables 
following the accomplishment instructions of DAHER-SOCATA Mandatory 
Service Bulletin SB 70-191-27, dated April 2011.
    (3) After the effective date of this AD, after each removal of 
the aileron control cables, you must re-install using the 
maintenance manual temporary revisions below:
    (i) For S/N 1 through 433: SOCATA TBM 700 Model Maintenance 
Manual Temporary Revision No. TR040.27, dated April 2011.
    (ii) For S/N 434 through 572, 574 and 576: SOCATA TBM 850 
Maintenance Manual Temporary Revision No. TR015.27, dated April 
2011.

FAA AD Differences

    Note: This AD differs from the MCAI and/or service information 
as follows: The compliance time of the MCAI is 12 months after the 
effective day of the AD. This differs from the service bulletin of 
12 months or 100 hours TIS, whichever occurs first. To assure that 
the unsafe condition is addressed on all airplanes in a timely 
manner, the FAA is using the compliance time from the service 
bulletin.

Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Office, FAA, has the authority to approve AMOCs for this 
AD, if requested using the procedures found in 14 CFR 39.19. Send 
information to ATTN: Albert Mercado, Aerospace Engineer, FAA, Small 
Airplane Directorate, 901 Locust, Room 301, Kansas City, Missouri 
64106; telephone: (816) 329-4119; fax: (816) 329-4090; e-mail: 
albert.mercado@faa.gov. Before using any approved AMOC on any 
airplane to which the AMOC applies, notify your appropriate 
principal inspector (PI) in the FAA Flight Standards District Office 
(FSDO), or lacking a PI, your local FSDO.
    (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: For any reporting requirement in 
this AD, 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

    (h) Refer to MCAI European Aviation Safety Agency (EASA) AD No.: 
2011-0101, dated May 25, 2011; DAHER-SOCATA Mandatory Service 
Bulletin SB 70-191-27, dated April 2011; SOCATA TBM 700 Model 
Maintenance Manual Temporary Revision No. TR040.27, dated April 
2011; and SOCATA TBM 850 Maintenance Manual Temporary Revision No. 
TR015.27, dated April 2011, for related information. For service 
information related to this AD, contact SOCATA--Direction des 
Services--65921 Tarbes Cedex 9--France; telephone +33 (0) 62 41 
7300, fax +33 (0) 62 41 76 54, or for North America: SOCATA NORTH 
AMERICA, 7501 South Airport Road, North Perry Airport (HWO), 
Pembroke Pines, Florida 33023; telephone: (954) 893-1400; fax: (954) 
964-4141; e-mail: mysocata@socata.daher.com; Internet: http://mysocata.com. You may review copies of the referenced service 
information at the FAA, Small Airplane Directorate, 901 Locust, 
Kansas City, Missouri 64106. For information on the availability of 
this material at the FAA, call (816) 329-4148.

    Issued in Kansas City, Missouri, on October 14, 2011.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification 
Service.
[FR Doc. 2011-27264 Filed 10-20-11; 8:45 am]
BILLING CODE 4910-13-P


