Airworthiness Directives; Empresa Brasileira de Aeronáutica S.A. (EMBRAER) Model EMB-500 Airplanes, 48028-48030 [E9-22642]
Download as PDF
48028
Federal Register / Vol. 74, No. 181 / Monday, September 21, 2009 / Proposed Rules
FAA AD Differences
DEPARTMENT OF TRANSPORTATION
Note 1: This AD differs from the MCAI
and/or service information as follows:
Although the MCAI/service information
allows further flight after cracks are found
during compliance with certain actions, this
AD requires that you repair the crack(s)
before further flight.
Federal Aviation Administration
Other FAA AD Provisions
Airworthiness Directives; Empresa
´
Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB–500 Airplanes
(g) 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.
Send information to ATTN: Dan Rodina,
Aerospace Engineer, International Branch,
ANM–116, Transport Airplane Directorate,
FAA, 1601 Lind Avenue, SW., Renton,
Washington 98057–3356; telephone (425)
227–2125; fax (425) 227–1149. Before using
any approved AMOC on any airplane to
which the AMOC applies, notify your
appropriate principal maintenance inspector
(PMI) or principal avionics inspector (PAI),
as appropriate, or lacking a principal
inspector, your local Flight Standards 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: For any
reporting requirement in this AD, under the
provisions of the Paperwork Reduction Act,
the Office of Management and Budget (OMB)
has approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
Related Information
srobinson on DSKHWCL6B1PROD with PROPOSALS
(h) Refer to MCAI European Aviation
Safety Agency (EASA) Airworthiness
Directive 2008–0181, dated October 1, 2008;
and the service bulletins identified in Table
2 of this AD; for related information.
Issued in Renton, Washington, on
September 11, 2009.
Stephen P. Boyd,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. E9–22667 Filed 9–18–09; 8:45 am]
BILLING CODE 4910–13–P
VerDate Nov<24>2008
18:23 Sep 18, 2009
Jkt 217001
14 CFR Part 39
[Docket No. FAA–2009–0870; Directorate
Identifier 2009–CE–049–AD]
RIN 2120–AA64
AGENCY: Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking
(NPRM).
SUMMARY: We propose to adopt a new
airworthiness directive (AD) for the
products listed above. 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: It has been found the
possibility of elevator mass balance
fasteners becoming slack under certain
conditions. The loose of at least two
fasteners may lead to an unbalance
condition, which may induce flutter on
airplane elevators.
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 November 5, 2009.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://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.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
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
PO 00000
Frm 00016
Fmt 4702
Sfmt 4702
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.
FOR FURTHER INFORMATION CONTACT: Karl
Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust,
Room 301, Kansas City, Missouri 64106;
telephone: (816) 329–4146; fax: (816)
329–4090.
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–2009–0870; Directorate Identifier
2009–CE–049–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 https://
www.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
ˆ
The Agencia Nacional de Aviacao
¸˜
Civil (ANAC), which is the aviation
authority for Brazil, has issued AD No.:
2009–09–01, dated September 3, 2009
(referred to after this as ‘‘the MCAI’’), to
correct an unsafe condition for the
specified products. The MCAI states:
It has been found the possibility of elevator
mass balance fasteners becoming slack under
certain conditions. The loose of at least two
fasteners may lead to an unbalance
condition, which may induce flutter on
airplane elevators.
The MCAI requires replacement of the
nuts of the right and left elevators mass
balance fasteners. You may obtain
further information by examining the
MCAI in the AD docket.
Relevant Service Information
Embraer—Empresa Brasileira de
Aeronautica S.A. has issued Phenom by
Embraer Service Bulletin No. 500–55–
0001, dated July 24, 2009. The actions
described in this service information are
intended to correct the unsafe condition
identified in the MCAI.
E:\FR\FM\21SEP1.SGM
21SEP1
Federal Register / Vol. 74, No. 181 / Monday, September 21, 2009 / Proposed Rules
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
srobinson on DSKHWCL6B1PROD with PROPOSALS
We estimate that this proposed AD
will affect 25 products of U.S. registry.
We also estimate that it would take
about 4 work-hours per product to
comply with the basic requirements of
this proposed AD. The average labor
rate is $80 per work-hour. Required
parts would cost about $150 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 proposed AD on U.S.
operators to be $11,750, or $470 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.
VerDate Nov<24>2008
18:23 Sep 18, 2009
Jkt 217001
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
48029
Comments Due Date
(a) We must receive comments by
November 5, 2009.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMB–500 airplanes,
serial numbers 50000005, 50000006,
50000008 through 50000036, 50000038
through 50000041, 50000043 through
50000046, 50000048, and 50000053,
certificated in any category.
Subject
(d) Air Transport Association of America
(ATA) Code 27: Flight Controls.
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.
Reason
(e) The mandatory continuing
airworthiness information (MCAI) states:
It has been found the possibility of elevator
mass balance fasteners becoming slack under
certain conditions. The loss of at least two
fasteners may lead to an unbalance
condition, which may induce flutter on
airplane elevators.
The MCAI requires replacement of the nuts
of the right and left elevators mass balance
fasteners.
List of Subjects in 14 CFR Part 39
FAA AD Differences
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Note: This AD differs from the MCAI and/
or service information as follows: No
differences.
The Proposed Amendment
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: Karl Schletzbaum, Aerospace
Engineer, FAA, Small Airplane Directorate,
901 Locust, Room 301, Kansas City, Missouri
64106; telephone: (816) 329–4146; 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
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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
´
Empresa Brasileira de Aeronautica S.A.
(EMBRAER): Docket No. FAA–2009–
0870; Directorate Identifier 2009–CE–
049–AD.
PO 00000
Frm 00017
Fmt 4702
Sfmt 4702
Actions and Compliance
(f) Unless already done, do the following
actions:
(1) Within the next 30 days after the
effective date of this AD, replace the nuts of
the right-hand (RH) and left-hand (LH)
elevators’ mass balance fasteners with new
ones of self-locking type bearing part number
(P/N) MS21043–4. Do the replacements
following Phenom by Embraer Service
Bulletin No. 500–55–0001, dated July 24,
2009.
(2) As of 30 days after the effective date of
this AD, only install self-locking type nuts,
P/N MS21043–4, on the RH and LH elevators
mass balance fasteners.
E:\FR\FM\21SEP1.SGM
21SEP1
48030
Federal Register / Vol. 74, No. 181 / Monday, September 21, 2009 / Proposed Rules
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
ˆ
(h) Refer to MCAI Agencia Nacional de
Aviacao Civil (ANAC) Brazilian
¸˜
Airworthiness Directive AD No.: 2009–09–
01, dated September 3, 2009, and Phenom by
Embraer Service Bulletin No. 500–55–0001,
dated July 24, 2009, for related information.
Issued in Kansas City, Missouri, on
September 15, 2009.
Scott A. Horn,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. E9–22642 Filed 9–18–09; 8:45 am]
BILLING CODE 4910–13–P
JOINT BOARD FOR THE
ENROLLMENT OF ACTUARIES
20 CFR Part 901
[REG–159704–03]
RIN 1545–BC82
Performance of Actuarial Services
Under the Employee Retirement
Income Security Act of 1974
srobinson on DSKHWCL6B1PROD with PROPOSALS
AGENCY: Joint Board for the Enrollment
of Actuaries.
ACTION: Notice of proposed rulemaking.
SUMMARY: This document contains
proposed amendments to 20 CFR part
901 relating to the enrollment of
actuaries under section 3042 of the
Employee Retirement Income Security
Act of 1974 (ERISA). The proposed
amendments would update the
eligibility requirements for performing
actuarial services for ERISA-covered
employee pension benefit plans,
including the continuing education
requirements, and the standards for
performing such actuarial services. The
proposed amendments would affect
employee pension benefit plans and the
actuaries providing actuarial services to
those plans.
DATES: Written or electronic comments
must be received by November 20, 2009.
ADDRESSES: Send written comments to:
CC:PA:LPD:PR (REG–159704–03), Room
5203, Internal Revenue Service, PO Box
7604, Ben Franklin Station, Washington,
DC 20044. Submissions may be hand-
VerDate Nov<24>2008
18:48 Sep 18, 2009
Jkt 217001
delivered Monday through Friday
between the hours of 8 a.m. and 4 p.m.
to CC:PA:LPD:PR (REG–159704–03),
Courier’s Desk, Internal Revenue
Service, 1111 Constitution Avenue,
NW., Washington, DC or sent
electronically via the Federal
eRulemaking Portal at https://
www.regulations.gov (IRS REG–159704–
03).
FOR FURTHER INFORMATION CONTACT:
Patrick McDonough, Executive Director,
Joint Board for the Enrollment of
Actuaries, (202) 622–8229 (not a tollfree number).
SUPPLEMENTARY INFORMATION:
Paperwork Reduction Act
The collections of information
referenced in this notice of proposed
rulemaking were previously reviewed
and approved by the Office of
Management and Budget in accordance
with the Paperwork Reduction Act of
1995 (44 U.S.C. 3507(d)) under control
number 1545–0951, relating to Enrolled
Actuaries under Employee Retirement
Income Security Act of 1974, published
on September 7, 1988, in the Federal
Register (53 FR 34484). There are no
proposals for substantive changes to this
collection of information.
An agency may not conduct or
sponsor, and a person is not required to
respond to, a collection of information
unless it displays a valid control
number assigned by the Office of
Management and Budget.
Books or records relating to a
collection of information must be
retained as long as their contents may
become material in the administration
of any internal revenue law. Generally,
tax returns and tax return information
are confidential, as required by 26
U.S.C. 6103.
Background
This document contains proposed
amendments to 20 CFR Part 901 under
section 3042 of the Employee
Retirement Income Security Act of 1974
(88 Stat. 829), Public Law 93–406
(ERISA). Section 3042 of ERISA
provides that the Joint Board for the
Enrollment of Actuaries (Joint Board)
shall, by regulations, establish
reasonable standards and qualifications
for persons performing actuarial
services with respect to plans subject to
ERISA and, upon application by any
individual, shall enroll such individual
if the Joint Board finds that such
individual satisfies such standards and
qualifications. Section 3042 also
provides that the Joint Board may, after
notice and an opportunity for a hearing,
suspend or terminate the enrollment of
PO 00000
Frm 00018
Fmt 4702
Sfmt 4702
an individual who fails to discharge his
duties under ERISA or who does not
satisfy the requirements for enrollment.
Consistent with section 3042, the
Joint Board has promulgated regulations
at 20 CFR part 901, addressing
eligibility for enrollment, requirements
for continuing education of enrolled
actuaries, professional standards for
performance of actuarial services under
ERISA, bases for disciplinary actions
and the procedures to be followed in
taking those actions. Comprehensive
regulations regarding section 3042 were
last issued in 1988 (53 FR 34484). The
Joint Board has determined that the
regulations need to be updated to reflect
changes in the law and in industry
practice. In addition to these proposed
regulations, final regulations relating to
user fees for the initial enrollment and
reenrollment as an enrolled actuary
were published in the Federal Register
on December 21, 2007 (72 FR 72606).
In anticipation of amending the Joint
Board regulations, the Joint Board
issued a Request for Information (RFI)
which was published in the Federal
Register on June 30, 2004 (69 FR 39376).
The RFI specifically requested
comments as to whether, and to what
extent, changes should be made to the
regulations in the following five areas:
1. Procedures and conditions for
enrollment and reenrollments;
2. Continuing professional education
(CPE) requirements;
3. Waivers of the CPE requirements;
4. Types of enrollment statuses
(active, inactive, and retired); and
5. Standards of conduct.
Eight comments were received.
The current regulations prescribe
various rules regarding the enrollment
and reenrollment of actuaries. Section
901.13 of the regulations provides that
an individual applying for enrollment
must satisfy requirements for: (1)
Qualifying experience; (2) basic
actuarial knowledge; and (3) pension
actuarial knowledge. Basic actuarial
knowledge may be demonstrated by
passing a Joint Board examination (or an
examination acceptable to the Joint
Board) regarding basic actuarial
mathematics and methodology, or by
earning a degree pertaining to actuarial
mathematics from an accredited college.
Pension actuarial knowledge must be
demonstrated by passing a Joint Board
examination (or an examination
acceptable to the Joint Board) in
actuarial mathematics related to pension
plans.
Under section 901.11, an enrolled
actuary must reenroll once every three
years. To qualify for reenrollment an
actuary must complete a minimum of 36
E:\FR\FM\21SEP1.SGM
21SEP1
Agencies
[Federal Register Volume 74, Number 181 (Monday, September 21, 2009)]
[Proposed Rules]
[Pages 48028-48030]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-22642]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-0870; Directorate Identifier 2009-CE-049-AD]
RIN 2120-AA64
Airworthiness Directives; Empresa Brasileira de
Aeron[aacute]utica S.A. (EMBRAER) Model EMB-500 Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for the
products listed above. 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: It has been found the possibility of elevator mass
balance fasteners becoming slack under certain conditions. The loose of
at least two fasteners may lead to an unbalance condition, which may
induce flutter on airplane elevators.
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 November 5,
2009.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Portal: Go to https://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.
Examining the AD Docket
You may examine the AD docket on the Internet at https://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.
FOR FURTHER INFORMATION CONTACT: Karl Schletzbaum, Aerospace Engineer,
FAA, Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; fax: (816) 329-4090.
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-2009-0870;
Directorate Identifier 2009-CE-049-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 https://www.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 Ag[ecirc]ncia Nacional de Avia[ccedil][atilde]o Civil (ANAC),
which is the aviation authority for Brazil, has issued AD No.: 2009-09-
01, dated September 3, 2009 (referred to after this as ``the MCAI''),
to correct an unsafe condition for the specified products. The MCAI
states:
It has been found the possibility of elevator mass balance
fasteners becoming slack under certain conditions. The loose of at
least two fasteners may lead to an unbalance condition, which may
induce flutter on airplane elevators.
The MCAI requires replacement of the nuts of the right and left
elevators mass balance fasteners. You may obtain further information by
examining the MCAI in the AD docket.
Relevant Service Information
Embraer--Empresa Brasileira de Aeronautica S.A. has issued Phenom
by Embraer Service Bulletin No. 500-55-0001, dated July 24, 2009. The
actions described in this service information are intended to correct
the unsafe condition identified in the MCAI.
[[Page 48029]]
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 25 products of U.S.
registry. We also estimate that it would take about 4 work-hours per
product to comply with the basic requirements of this proposed AD. The
average labor rate is $80 per work-hour. Required parts would cost
about $150 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 proposed AD on
U.S. operators to be $11,750, or $470 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 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.
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:
Empresa Brasileira de Aeron[aacute]utica S.A. (EMBRAER): Docket No.
FAA-2009-0870; Directorate Identifier 2009-CE-049-AD.
Comments Due Date
(a) We must receive comments by November 5, 2009.
Affected ADs
(b) None.
Applicability
(c) This AD applies to EMB-500 airplanes, serial numbers
50000005, 50000006, 50000008 through 50000036, 50000038 through
50000041, 50000043 through 50000046, 50000048, and 50000053,
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:
It has been found the possibility of elevator mass balance
fasteners becoming slack under certain conditions. The loss of at
least two fasteners may lead to an unbalance condition, which may
induce flutter on airplane elevators.
The MCAI requires replacement of the nuts of the right and left
elevators mass balance fasteners.
Actions and Compliance
(f) Unless already done, do the following actions:
(1) Within the next 30 days after the effective date of this AD,
replace the nuts of the right-hand (RH) and left-hand (LH)
elevators' mass balance fasteners with new ones of self-locking type
bearing part number (P/N) MS21043-4. Do the replacements following
Phenom by Embraer Service Bulletin No. 500-55-0001, dated July 24,
2009.
(2) As of 30 days after the effective date of this AD, only
install self-locking type nuts, P/N MS21043-4, on the RH and LH
elevators mass balance fasteners.
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 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: Karl Schletzbaum, Aerospace Engineer, FAA,
Small Airplane Directorate, 901 Locust, Room 301, Kansas City,
Missouri 64106; telephone: (816) 329-4146; 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
[[Page 48030]]
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 Ag[ecirc]ncia Nacional de
Avia[ccedil][atilde]o Civil (ANAC) Brazilian Airworthiness Directive
AD No.: 2009-09-01, dated September 3, 2009, and Phenom by Embraer
Service Bulletin No. 500-55-0001, dated July 24, 2009, for related
information.
Issued in Kansas City, Missouri, on September 15, 2009.
Scott A. Horn,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. E9-22642 Filed 9-18-09; 8:45 am]
BILLING CODE 4910-13-P