Airworthiness Directives; EADS SOCATA Model TBM 700 Airplanes, 12546-12548 [E7-4724]
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12546
Federal Register / Vol. 72, No. 51 / Friday, March 16, 2007 / Rules and Regulations
sroberts on PROD1PC70 with RULES
resources.1 As with other actions taken
by the Commission, dismissal of a
matter requires the vote of at least four
Commissioners.
Pursuant to the exercise of its
prosecutorial discretion, the
Commission will dismiss a matter when
the matter does not merit further use of
Commission resources, due to factors
such as the small amount or significance
of the alleged violation, the vagueness
or weakness of the evidence, or likely
difficulties with an investigation, or
when the Commission lacks majority
support for proceeding with a matter for
other reasons. For example, a dismissal
would be appropriate when:
• The seriousness of the alleged
conduct is not sufficient to justify the
likely cost and difficulty of an
investigation to determine whether a
violation in fact occurred; or
• The evidence is sufficient to
support a ‘‘reason to believe’’ finding,
but the violation is minor.
The Commission may also dismiss
when, based on the complaint,
response, and publicly available
information, the Commission concludes
that a violation of the Act did or very
probably did occur, but the size or
significance of the apparent violation is
not sufficient to warrant further pursuit
by the Commission. In this latter
circumstance, the Commission will send
a letter admonishing the respondent.
For example, a dismissal with
admonishment would be appropriate
when:
• A respondent admits to a violation,
but the amount of the violation is not
sufficient to warrant any monetary
penalty; or
• A complaint convincingly alleges a
violation, but the significance of the
violation is not sufficient to warrant
further pursuit by the Commission.
C. ‘‘No Reason To Believe’’
The Commission will make a
determination of ‘‘no reason to believe’’
a violation has occurred when the
available information does not provide
a basis for proceeding with the matter.
The Commission finds ‘‘no reason to
believe’’ when the complaint, any
response filed by the respondent, and
any publicly available information,
when taken together, fail to give rise to
a reasonable inference that a violation
has occurred, or even if the allegations
were true, would not constitute a
violation of the law. For example, a ‘‘no
reason to believe’’ finding would be
appropriate when:
• A violation has been alleged, but
the respondent’s response or other
evidence convincingly demonstrates
that no violation has occurred;
• A complaint alleges a violation but
is either not credible or is so vague that
an investigation would be effectively
impossible; or
• A complaint fails to describe a
violation of the Act.
If the Commission, with the vote of at
least four Commissioners, finds that
there is ‘‘no reason to believe’’ a
violation has occurred or is about to
occur with respect to the allegations in
the complaint, the Commission will
close the file and respondents and the
complainant will be notified.
D. Conclusion
This policy enunciates and describes
the Commission’s standards for actions
at the point of determining whether or
not to open an investigation or to enter
into conciliation with respondents prior
to a finding of probable cause to believe.
The policy does not confer any rights on
any person and does not in any way
limit the right of the Commission to
evaluate every case individually on its
own facts and circumstances.
This notice represents a general
statement of policy announcing the
general course of action that the
Commission intends to follow. This
policy statement does not constitute an
agency regulation requiring notice of
proposed rulemaking, opportunities for
public participation, prior publication,
and delay effective under 5 U.S.C. 553
of the Administrative Procedures Act
(‘‘APA’’). As such, it does not bind the
Commission or any member of the
general public. The provisions of the
Regulatory Flexibility Act, 5 U.S.C.
605(b), which apply when notice and
comment are required by the APA or
another statute, are not applicable.
Dated: March 7, 2007.
Robert D. Lenhard,
Chairman, Federal Election Commission.
[FR Doc. E7–4868 Filed 3–15–07; 8:45 am]
BILLING CODE 6715–01–P
15:23 Mar 15, 2007
Jkt 211001
PO 00000
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–26166; Directorate
Identifier 2006–CE–58–AD; Amendment 39–
14992; AD 2007–06–11]
RIN 2120–AA64
Airworthiness Directives; EADS
SOCATA Model TBM 700 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
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:
Cracks on a vertical stabilizer attachment
fitting due to corrosion, have been found on
an aircraft in service.
We are issuing this AD to require
actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective April
20, 2007.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of April 20, 2007.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, Room PL–401,
Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Albert J. 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:
Streamlined Issuance of AD
The FAA is implementing a new
process for streamlining the issuance of
ADs related to MCAI. The streamlined
process will allow us to adopt MCAI
safety requirements in a more efficient
manner and will reduce safety risks to
the public. This process continues to
follow all FAA AD issuance processes to
meet legal, economic, Administrative
Procedure Act, and Federal Register
requirements. We also continue to meet
1 The FECA and Commission regulations also
recognize the Commission’s authority to dismiss
enforcement matters. See 2 U.S.C. 437g(a)(1); 11
CFR 111.6(b) and 111.7(b).
VerDate Aug<31>2005
DEPARTMENT OF TRANSPORTATION
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Federal Register / Vol. 72, No. 51 / Friday, March 16, 2007 / Rules and Regulations
our technical decision-making
responsibilities to identify and correct
unsafe conditions on U.S.-certificated
products.
This AD references the MCAI and
related service information that we
considered in forming the engineering
basis to correct the unsafe condition.
The AD contains text copied from the
MCAI and for this reason might not
follow our plain language principles.
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 November 17, 2006 (71 FR
66889). That NPRM proposed to correct
an unsafe condition for the specified
products. The MCAI states that:
Cracks on a vertical stabilizer attachment
fitting due to corrosion, have been found on
an aircraft in service.
Comments
We gave the public the opportunity to
participate in developing this AD. We
considered the comments received.
EADS SOCATA gave comments
addressing the following:
sroberts on PROD1PC70 with RULES
Comment Issue No. 1: Costs of
Compliance
EADS SOCATA comments that the
proposed AD specifies it would take 4
work-hours per product to comply with
the proposed AD, but according to
EADS SOCATA, it would take 3.5 workhours.
The FAA agrees and will incorporate
that change into the final rule Costs of
Compliance section.
Comment Issue No. 2: Service Bulletin
Compliance
Quest Diagnostics comments that as
an operator of 4 TBM 700 aircraft with
over 25,000 hours time-in-service (TIS)
and more than 35,000 cycles of
operating experience they have been
performing the requirements of EADS
SOCATA Service Bulletin (SB) 70–104
since its publication in 2004. They have
found in their experience that step 5 of
the SB, which requires an additional
step to perform a ‘‘penetrante
inspection’’ to the bores of the fitting
and attachment on the rear fitting, is
impractical if not impossible to
complete. They found that because this
attachment area comprises a
‘‘sandwich’’ of attachment lugs any
penetrant applied to this area in situ is
absorbed between the layers and
becomes impossible to clean without
removing the fin completely. Further,
they found, since each assembly is
VerDate Aug<31>2005
15:23 Mar 15, 2007
Jkt 211001
nearly 1 inch thick, there is severely
limited visual access to the entire bore,
particularly in the middle section. They
contracted the services of a Level 3
Nondestructive Testing (NDT) inspector
to perform a Rotary Gun Eddy Current
Inspection of the fitting area. They
discussed this situation with the EADS
SOCATA Service Center in Pembroke
Pines, Florida; came to the conclusion
this is the only practical approach to
completing this inspection without
removal of the vertical fin; and feel the
published procedure is inadequate for
the purposes of detecting cracks in this
area.
EADS SOCATA has since released SB
70–104 Amendment 2, dated January
2007. The revised service bulletin
allows crack detection by penetrant
inspection or other equivalent process
(eddy current* * *) on the bores of the
vertical stabilizer fitting and
attachments. The revised service
bulletin Amendment 2 will be
incorporated into the AD, and the FAA
will give 100 percent credit for doing
the action with Amendment 1 of the
Service Bulletin.
Conclusion
We reviewed the available data,
including the comments 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 FAA policies.
Any such differences are highlighted in
a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect
205 products of U.S. registry. We also
estimate that it will take about 3.5 workhours per product to comply with basic
requirements of this AD. The average
labor rate is $80 per work-hour.
Required parts will cost about $3,000
per product. Where the service
PO 00000
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12547
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
$672,400, or $3,280 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
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://dms.dot.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 the
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Federal Register / Vol. 72, No. 51 / Friday, March 16, 2007 / Rules and Regulations
NPRM, the regulatory evaluation, any
comments received, and other
information. The street address for the
Docket Office (telephone (800) 647–
5227) is in the ADDRESSES section.
Comments will be available in the AD
docket shortly after receipt.
(2) Repeat the actions of paragraph (e)(1)
every 1,200 hours TIS or every 24 months,
whichever occurs first, following EADS
SOCATA Service Bulletin SB 70–104,
Amendment 1, dated August 2004 or EADS
SOCATA Service Bulletin SB 70–104,
Amendment 2, dated January 2007.
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: https://www.archives.gov/federal-register/
cfr/ibr-locations.html.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
FAA AD Differences
Note 2: This AD differs from the MCAI
and/or service information as follows: This
AD permits Amendment 2 of the SB to be
used.
Issued in Kansas City, Missouri, on March
7, 2007.
David R. Showers,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E7–4724 Filed 3–15–07; 8:45 am]
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
I
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
I
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
I
2007–06–11 EADS SOCATA Model TBM
700 Airplanes: Amendment 39–14992;
Docket No. FAA–2006–26166;
Directorate Identifier 2006–CE–58–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective April 20, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to SOCATA TBM 700
airplanes, serial numbers 1 through 308, plus
the serial number 310, certificated in any
category.
Note 1: This AD does not apply to
airplanes in which both modifications No.
MOD70–127–55 and MOD70–129–53 have
been factory installed.
sroberts on PROD1PC70 with RULES
Reason
(d) The mandatory continuing
airworthiness information (MCAI) states that:
Cracks on a vertical stabilizer attachment
fitting due to corrosion have been found on
an aircraft in service.
Actions and Compliance
(e) Unless already done, do the following
actions.
(1) Within the next 600 hours time-inservice (TIS) or the next 12 months,
whichever occurs first, after the effective date
of this AD, inspect the vertical stabilizer
attachment fittings and bolts for cracks or
corrosion, and, if necessary, repair or replace
the damaged part and then apply a corrosion
protection reinforcement, following EADS
SOCATA Service Bulletin SB 70–104,
Amendment 1, dated August 2004 or EADS
SOCATA TBM Aircraft Mandatory Service
Bulletin SB 70–104, Amendment 2, dated
January 2007.
VerDate Aug<31>2005
15:23 Mar 15, 2007
Jkt 211001
Other FAA AD Provisions
(f) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Standards Staff,
FAA, ATTN: Albert J. Mercado, Aerospace
Engineer, FAA, Small Airplane Directorate,
901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329–4119; fax: (816)
329–4090, has the authority to approve
AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. 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
´ ´
(g) Refer to Direction generale de l’aviation
civile (DGAC) AD No F–2003–366 R1, dated
November 24, 2004; EADS SOCATA TBM
Aircraft Mandatory Service Bulletin SB 70–
104, Amendment 1, dated August 2004; and
EADS SOCATA TBM Aircraft Mandatory
Service Bulletin SB 70–104, Amendment 2,
dated January 2007 for related information.
Material Incorporated by Reference
(h) You must use EADS SOCATA TBM
Aircraft Mandatory Service Bulletin No. SB
70–104, Amendment 1, dated August 2004,
or EADS SOCATA TBM Aircraft Mandatory
Service Bulletin No. SB 70–104, Amendment
2, dated January 2007 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.
(3) For service information identified in
this AD, contact EADS SOCATA, Direction
des Services, 65921 Tarbes Cedex 9, France.
(4) You may review copies at the FAA,
Central Region, Office of the Regional
PO 00000
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BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2006–26180; Directorate
Identifier 2006–CE–59–AD; Amendment 39–
14995; AD 2007–06–14]
RIN 2120–AA64
Airworthiness Directives; EADS
SOCATA Model TBM 700 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
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 discovery of propeller
control cables with a defective
crimping. Two cable ends were found
uncrimped at the factory after an engine
run-up test, and one cable end was also
found uncrimped on the first 100-hour
aircraft maintenance check. We are
issuing this AD to require actions to
correct the unsafe condition on these
products.
This AD becomes effective April
20, 2007.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of April 20, 2007.
ADDRESSES: You may examine the AD
docket on the Internet at https://
dms.dot.gov or in person at the Docket
Management Facility, U.S. Department
of Transportation, 400 Seventh Street,
SW., Nassif Building, Room PL–401,
Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Albert J. Mercado, Aerospace Engineer,
DATES:
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]]>Agencies
[Federal Register Volume 72, Number 51 (Friday, March 16, 2007)]
[Rules and Regulations]
[Pages 12546-12548]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E7-4724]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2006-26166; Directorate Identifier 2006-CE-58-AD;
Amendment 39-14992; AD 2007-06-11]
RIN 2120-AA64
Airworthiness Directives; EADS SOCATA Model TBM 700 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) 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:
Cracks on a vertical stabilizer attachment fitting due to
corrosion, have been found on an aircraft in service.
We are issuing this AD to require actions to correct the unsafe
condition on these products.
DATES: This AD becomes effective April 20, 2007.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of April 20,
2007.
ADDRESSES: You may examine the AD docket on the Internet at https://
dms.dot.gov or in person at the Docket Management Facility, U.S.
Department of Transportation, 400 Seventh Street, SW., Nassif Building,
Room PL-401, Washington, DC.
FOR FURTHER INFORMATION CONTACT: Albert J. 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:
Streamlined Issuance of AD
The FAA is implementing a new process for streamlining the issuance
of ADs related to MCAI. The streamlined process will allow us to adopt
MCAI safety requirements in a more efficient manner and will reduce
safety risks to the public. This process continues to follow all FAA AD
issuance processes to meet legal, economic, Administrative Procedure
Act, and Federal Register requirements. We also continue to meet
[[Page 12547]]
our technical decision-making responsibilities to identify and correct
unsafe conditions on U.S.-certificated products.
This AD references the MCAI and related service information that we
considered in forming the engineering basis to correct the unsafe
condition. The AD contains text copied from the MCAI and for this
reason might not follow our plain language principles.
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 November 17, 2006
(71 FR 66889). That NPRM proposed to correct an unsafe condition for
the specified products. The MCAI states that:
Cracks on a vertical stabilizer attachment fitting due to
corrosion, have been found on an aircraft in service.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comments received.
EADS SOCATA gave comments addressing the following:
Comment Issue No. 1: Costs of Compliance
EADS SOCATA comments that the proposed AD specifies it would take 4
work-hours per product to comply with the proposed AD, but according to
EADS SOCATA, it would take 3.5 work-hours.
The FAA agrees and will incorporate that change into the final rule
Costs of Compliance section.
Comment Issue No. 2: Service Bulletin Compliance
Quest Diagnostics comments that as an operator of 4 TBM 700
aircraft with over 25,000 hours time-in-service (TIS) and more than
35,000 cycles of operating experience they have been performing the
requirements of EADS SOCATA Service Bulletin (SB) 70-104 since its
publication in 2004. They have found in their experience that step 5 of
the SB, which requires an additional step to perform a ``penetrante
inspection'' to the bores of the fitting and attachment on the rear
fitting, is impractical if not impossible to complete. They found that
because this attachment area comprises a ``sandwich'' of attachment
lugs any penetrant applied to this area in situ is absorbed between the
layers and becomes impossible to clean without removing the fin
completely. Further, they found, since each assembly is nearly 1 inch
thick, there is severely limited visual access to the entire bore,
particularly in the middle section. They contracted the services of a
Level 3 Nondestructive Testing (NDT) inspector to perform a Rotary Gun
Eddy Current Inspection of the fitting area. They discussed this
situation with the EADS SOCATA Service Center in Pembroke Pines,
Florida; came to the conclusion this is the only practical approach to
completing this inspection without removal of the vertical fin; and
feel the published procedure is inadequate for the purposes of
detecting cracks in this area.
EADS SOCATA has since released SB 70-104 Amendment 2, dated January
2007. The revised service bulletin allows crack detection by penetrant
inspection or other equivalent process (eddy current* * *) on the bores
of the vertical stabilizer fitting and attachments. The revised service
bulletin Amendment 2 will be incorporated into the AD, and the FAA will
give 100 percent credit for doing the action with Amendment 1 of the
Service Bulletin.
Conclusion
We reviewed the available data, including the comments 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 FAA policies. Any such differences are
highlighted in a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect 205 products of U.S. registry.
We also estimate that it will take about 3.5 work-hours per product to
comply with basic requirements of this AD. The average labor rate is
$80 per work-hour. Required parts will cost about $3,000 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 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 $672,400, or $3,280 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 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://
dms.dot.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 the
[[Page 12548]]
NPRM, the regulatory evaluation, any comments received, and other
information. The street address for the Docket Office (telephone (800)
647-5227) 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
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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]
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2. The FAA amends Sec. 39.13 by adding the following new AD:
2007-06-11 EADS SOCATA Model TBM 700 Airplanes: Amendment 39-14992;
Docket No. FAA-2006-26166; Directorate Identifier 2006-CE-58-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective April
20, 2007.
Affected ADs
(b) None.
Applicability
(c) This AD applies to SOCATA TBM 700 airplanes, serial numbers
1 through 308, plus the serial number 310, certificated in any
category.
Note 1: This AD does not apply to airplanes in which both
modifications No. MOD70-127-55 and MOD70-129-53 have been factory
installed.
Reason
(d) The mandatory continuing airworthiness information (MCAI)
states that:
Cracks on a vertical stabilizer attachment fitting due to
corrosion have been found on an aircraft in service.
Actions and Compliance
(e) Unless already done, do the following actions.
(1) Within the next 600 hours time-in-service (TIS) or the next
12 months, whichever occurs first, after the effective date of this
AD, inspect the vertical stabilizer attachment fittings and bolts
for cracks or corrosion, and, if necessary, repair or replace the
damaged part and then apply a corrosion protection reinforcement,
following EADS SOCATA Service Bulletin SB 70-104, Amendment 1, dated
August 2004 or EADS SOCATA TBM Aircraft Mandatory Service Bulletin
SB 70-104, Amendment 2, dated January 2007.
(2) Repeat the actions of paragraph (e)(1) every 1,200 hours TIS
or every 24 months, whichever occurs first, following EADS SOCATA
Service Bulletin SB 70-104, Amendment 1, dated August 2004 or EADS
SOCATA Service Bulletin SB 70-104, Amendment 2, dated January 2007.
FAA AD Differences
Note 2: This AD differs from the MCAI and/or service information
as follows: This AD permits Amendment 2 of the SB to be used.
Other FAA AD Provisions
(f) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Standards Staff, FAA, ATTN: Albert J. Mercado, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4119; fax: (816) 329-4090, has
the authority to approve AMOCs for this AD, if requested using the
procedures found in 14 CFR 39.19. 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
(g) Refer to Direction generale de l'aviation civile (DGAC) AD
No F-2003-366 R1, dated November 24, 2004; EADS SOCATA TBM Aircraft
Mandatory Service Bulletin SB 70-104, Amendment 1, dated August
2004; and EADS SOCATA TBM Aircraft Mandatory Service Bulletin SB 70-
104, Amendment 2, dated January 2007 for related information.
Material Incorporated by Reference
(h) You must use EADS SOCATA TBM Aircraft Mandatory Service
Bulletin No. SB 70-104, Amendment 1, dated August 2004, or EADS
SOCATA TBM Aircraft Mandatory Service Bulletin No. SB 70-104,
Amendment 2, dated January 2007 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.
(3) For service information identified in this AD, contact EADS
SOCATA, Direction des Services, 65921 Tarbes Cedex 9, France.
(4) 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: https://www.archives.gov/federal-
register/cfr/ibr-locations.html.
Issued in Kansas City, Missouri, on March 7, 2007.
David R. Showers,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E7-4724 Filed 3-15-07; 8:45 am]
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