AD 2007-13-18

[Federal Register Volume 72, Number 129 (Friday, July 6, 2007)]
[Rules and Regulations]
[Pages 36866-36868]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: E7-12625]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2007-27432 Directorate Identifier 2007-CE-017-AD; 
Amendment 39-15122; AD 2007-13-18]
RIN 2120-AA64


Airworthiness Directives; SOCATA--Groupe Aerospatiale Models TB9, 
TB10, and TB200 Airplanes

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

ACTION: Final rule.

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SUMMARY: We are adopting a new airworthiness directive (AD) for the 
products listed above. This AD results from mandatory continuing 
airworthiness information (MCAI) issued 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:

    The aim of the Airworthiness Directive (AD) is to introduce a 
new life limit for engine and Nose Landing Gear (NLG) mounts 
installed on EADS SOCATA TB 9, TB 10 and TB 200 airplanes, as 
defined in the updated Airworthiness Limitations Section (ALS) of 
the relevant Aircraft Maintenance Manuals (AMM).

We are issuing this AD to require actions to correct the unsafe 
condition on these products.

DATES: This AD becomes effective August 10, 2007.
    On August 10, 2007, the Director of the Federal Register approved 
the incorporation by reference of certain publications listed in this 
AD.

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, U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue, SE., Washington, DC 20590.

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.

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 April 24, 2007 (72 
FR 20300). That NPRM proposed to correct an unsafe condition for the 
specified products. The MCAI states that:

    The aim of this Airworthiness Directive (AD) is to introduce a 
new life limit for engine and Nose Landing Gear (NLG) mounts 
installed on EADS SOCATA TB 9, TB 10 and TB 200 airplanes, as 
defined in the updated Airworthiness Limitations Section (ALS) of 
the relevant Aircraft Maintenance Manuals (AMM).
    This AD requires introduction of the new 10,000 Flight Hour life 
limit for engine and NLG mounts into the operator's maintenance 
program through the Revision 18 of the AMM.

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 as proposed.

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 FAA policies. Any such differences are 
highlighted in a NOTE within the AD.

Costs of Compliance

    We estimate that this AD will affect 146 products of U.S. registry. 
We also estimate that it will take about 0.5 work-hours per product to 
comply with basic requirements of this AD. The average labor rate is 
$80 per work-hour.
    Based on these figures, we estimate the cost of this AD to the U.S. 
operators to be $5,840 or $40 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

[[Page 36867]]

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 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://dms.dot.gov">http://dms.dot.gov</a>; 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 the NPRM, 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.

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

2007-13-18 SOCATA--Groupe Aerospatiale: Amendment 39-15122; Docket 
No. FAA-2007-27432; Directorate Identifier 2007-CE-017-AD.

Effective Date

    (a) This airworthiness directive (AD) becomes effective August 
10, 2007.

Affected ADs

    (b) None.

Applicability

    (c) This AD applies to Models TB 9, TB 10, and TB 200 airplanes, 
all serial numbers, certificated in any category.

Subject

    (d) Air Transport Association of America (ATA) Code 5: Time 
Limits.

Reason

    (e) The mandatory continuing airworthiness information (MCAI) 
states:

    The aim of this Airworthiness Directive (AD) is to introduce a 
new life limit for engine and Nose Landing Gear (NLG) mounts 
installed on EADS SOCATA TB 9, TB 10 and TB 200 airplanes, as 
defined in the updated Airworthiness Limitations Section (ALS) of 
the relevant Aircraft Maintenance Manuals (AMM).
    This AD requires introduction of the new 10,000 Flight Hour life 
limit for engine and NLG mounts into the operator's maintenance 
program through the Revision 18 of the AMM.

Actions and Compliance

    (f) Unless already done, within the next 30 days after August 
10, 2007 (the effective date of this AD), incorporate the life 
limits in the Airworthiness Limitations documents presented in 
paragraphs (f)(1), (f)(2), and (f)(3) of this AD into the FAA-
approved maintenance program, as applicable. This may be done by 
updating the Airworthiness Limitations Section of the airplane 
maintenance manual (AMM) and inserting the following applicable 
revision. The owner/operator holding at least a private pilot 
certificate as authorized by section 43.7 of the Federal Aviation 
Regulations (14 CFR 43.7) may do this action. Make an entry in the 
aircraft records showing compliance with this portion of the AD 
following section 43.9 of the Federal Aviation Regulations (14 CFR 
43.9).
    (1) For Model TB 9 airplanes: Use SOCATA TB 9 Model Maintenance 
Manual, 04, Airworthiness Limitations, Revision 18, dated September 
2006, or later revision that incorporates the same life limit for 
the engine mount and NLG mount as the above referenced Revision 18;
    (2) For Model TB 10 airplanes: Use SOCATA TB 10 Model 
Maintenance Manual, 04, Airworthiness Limitations, Revision 18, 
dated September 2006, or later revision that incorporates the same 
life limit for the engine mount and NLG mount as the above 
referenced Revision 18; or
    (3) For Model TB 200 airplanes: Use SOCATA TB 200 Model 
Maintenance Manual, 04, Airworthiness Limitations, Revision 18, 
dated September 2006, or later revision that incorporates the same 
life limit for the engine mount and NLG mount as the above 
referenced Revision 18.

FAA AD Differences

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

Other FAA AD Provisions

    (g) The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Standards Staff, 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 J. Mercado, Aerospace Safety Engineer, 
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City, 
Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090. 
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, under the provisions of the Paperwork Reduction Act (44 
U.S.C. 3501 et seq.), the Office of Management and Budget (OMB) has 
approved the information collection requirements and has assigned 
OMB Control Number 2120-0056.

Related Information

    (h) Refer to MCAI European Aviation Safety Agency (EASA) AD No. 
2007-0034, dated February 22, 2007; SOCATA TB 9 Model Maintenance 
Manual, 04, Airworthiness Limitations, Revision 18, dated September 
2006; SOCATA TB 10 Model Maintenance Manual, 04, Airworthiness 
Limitations, Revision 18, dated September 2006; and SOCATA TB 200 
Model Maintenance Manual, 04, Airworthiness Limitations, Revision 
18, dated September 2006, for related information.

Material Incorporated by Reference

    (i) You must use SOCATA TB 9 Model Maintenance Manual, 04, 
Airworthiness Limitations, Revision 18, dated September 2006; SOCATA 
TB 10 Model Maintenance

[[Page 36868]]

Manual, 04, Airworthiness Limitations, Revision 18, dated September 
2006; and SOCATA TB 200 Model Maintenance Manual, 04, Airworthiness 
Limitations, Revision 18, dated September 2006, 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 EADS 
SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France; 
telephone: 33 (0)5 62.41.73.00; fax: 33 (0)5 62.41.76.54; or SOCATA 
AIRCRAFT, INC., North Perry Airport, 7501 Airport Road, Pembroke 
Pines, Florida 33023; telephone: (954) 893-1400; fax (954) 964-4141.
    (3) You may review copies at the FAA, Central Region, Office of 
the Regional Counsel, 901 Locust, Room 506, Kansas City, Missouri 
64106; or 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/cfr/ibr-locations.html">http://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    Issued in Kansas City, Missouri, on June 22, 2007.
Kim Smith,
Manager, Small Airplane Directorate, Aircraft Certification Service.
 [FR Doc. E7-12625 Filed 7-5-07; 8:45 am]
BILLING CODE 4910-13-P