Airworthiness Directives; Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900) Airplanes, 68682-68684 [2010-28089]
Download as PDF
wwoods2 on DSK1DXX6B1PROD with RULES_PART 1
68682
Federal Register / Vol. 75, No. 216 / Tuesday, November 9, 2010 / Rules and Regulations
approximately $714,000, which is less
than $750,000, and thus would be
considered small business according to
the SBA definition. Although there is no
official data available to date, as these
states were recently added to the order
and have not completed one full crop
year for reporting purposes, the industry
estimates that the majority of producers
in Arizona and New Mexico would also
be considered small businesses.
This rule continues in effect the
action that modified the aflatoxin
sampling and testing regulations
currently prescribed under the
California, Arizona and New Mexico
pistachio order, as well as removed
unnecessary language and corrected
terminology. The changes to § 983.150
are expected to reduce handler
operating costs by providing a uniform
and consistent aflatoxin sampling and
testing procedure for pistachios shipped
to all market destinations. Authority for
the change in the order’s rules and
regulations is provided in § 983.50.
This action is expected to benefit
producers and handlers, regardless of
size and regardless of the market they
ship into, as it streamlines handler
operations and increases marketing
flexibility. Reducing the number of
required samples, the number of
aflatoxin analyses, and the total weight
of the lot samples, while increasing the
weight of the test samples for each lot
is expected to result in an estimated
annual savings to the industry of
approximately $18,000, including
reductions of $900 for sampling, $1,400
for testing, $12,750 for labor, and $3,750
in shipping costs for those small
handlers that do not do testing on site.
This action will not impose any
additional reporting or recordkeeping
requirements on either small or large
pistachio handlers. As with all Federal
marketing order programs, reports and
forms are periodically reviewed to
reduce information requirements and
duplication by industry and public
sector agencies. In addition, USDA has
not identified any relevant Federal rules
that duplicate, overlap or conflict with
this rule.
Further, the Committee’s meeting was
widely publicized throughout the
pistachio industry and all interested
persons were invited to attend the
meeting and participate in Committee
deliberations. Like all Committee
meetings, the meeting was a public
meeting and all entities, both large and
small, were able to express their views
on this issue.
Comments on the interim rule were
required to be received on or before
September 21, 2010. No comments were
received. Therefore, for the reasons
VerDate Mar<15>2010
14:45 Nov 08, 2010
Jkt 223001
given in the interim rule, we are
adopting the interim rule as a final rule,
without change.
To view the interim rule, go to: http:
//www.regulations.gov and type the
following docket number into the
keyword search section: FV10–983–1 IR.
Follow the link provided in the
‘‘Results’’ section of this page.
This action also affirms information
contained in the interim rule concerning
Executive Orders 12866 and 12988,
Paperwork Reduction Act (44 U.S.C.
chapter 35), and the E-Gov Act (44
U.S.C. 101).
After consideration of all relevant
material presented, it is found that
finalizing the interim rule, without
change, as published in the Federal
Register (75 FR 43045, July 23, 2010)
will tend to effectuate the declared
policy of the Act.
List of Subjects in 7 CFR Part 983
Marketing agreements and orders,
Pistachios, Reporting and recordkeeping
requirements.
PART 983—[AMENDED]
Accordingly, the interim rule that
amended 7 CFR part 983 that was
published at 75 FR 43045 on July 23,
2010, is adopted as a final rule, without
change.
■
Dated: November 3, 2010.
David R. Shipman,
Acting Administrator, Agricultural Marketing
Service.
[FR Doc. 2010–28240 Filed 11–8–10; 8:45 am]
BILLING CODE 3410–02–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–0700; Directorate
Identifier 2010–NM–123–AD; Amendment
39–16500; AD 2010–23–11]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc. Model CL–600–2C10 (Regional Jet
Series 700, 701, & 702), CL–600–2D15
(Regional Jet Series 705), and CL–600–
2D24 (Regional Jet Series 900)
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for the
products listed above. This AD results
SUMMARY:
PO 00000
Frm 00002
Fmt 4700
Sfmt 4700
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:
The manufacturer has informed Transport
Canada that a certain number of the resolver
stators, which were installed in the angle of
attack (AOA) transducers, were not cleaned
correctly. This condition can degrade the
AOA transducer performance at low
temperatures resulting in freezing of the AOA
transducer resolver, which may provide
inaccurate AOA data to the Stall Protection
System (SPS). If not corrected, this condition
can result in early or late activation of the
stick shaker and/or stick pusher.
These conditions could result in
reduced ability of the flight crew to
maintain a safe flight and landing of the
airplane. We are issuing this AD to
require actions to correct the unsafe
condition on these products.
DATES: This AD becomes effective
December 14, 2010.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of December 14, 2010.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov or in person at the
U.S. Department of Transportation,
Docket Operations, M–30, West
Building Ground Floor, Room W12–140,
1200 New Jersey Avenue, SE.,
Washington, DC.
FOR FURTHER INFORMATION CONTACT:
Joseph Licata, Aerospace Engineer,
Avionics and Flight Test Branch,
ANE–172, FAA, New York Aircraft
Certification Office (ACO), 1600 Stewart
Avenue, Suite 410, Westbury, New York
11590; telephone (516) 228–7361; fax
(516) 794–5531.
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 July 27, 2010 (75 FR 43882).
That NPRM proposed to correct an
unsafe condition for the specified
products. The MCAI states:
The manufacturer has informed Transport
Canada that a certain number of the resolver
stators, which were installed in the angle of
attack (AOA) transducers, were not cleaned
correctly. This condition can degrade the
AOA transducer performance at low
temperatures resulting in freezing of the AOA
transducer resolver, which may provide
inaccurate AOA data to the Stall Protection
System (SPS). If not corrected, this condition
E:\FR\FM\09NOR1.SGM
09NOR1
Federal Register / Vol. 75, No. 216 / Tuesday, November 9, 2010 / Rules and Regulations
can result in early or late activation of the
stick shaker and/or stick pusher.
These conditions could result in
reduced ability of the flight crew to
maintain a safe flight and landing of the
airplane. The required actions include
an inspection to determine if certain
AOA transducers are installed and
replacement of affected transducers.
You may obtain further information by
examining the MCAI in the AD docket.
Comments
We gave the public the opportunity to
participate in developing this AD. We
considered the comment received. Air
Line Pilots Association, International
(ALPA), supports the NPRM.
Conclusion
We reviewed the available data,
including the comment received, 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 our FAA
policies. Any such differences are
highlighted in a NOTE within the AD.
wwoods2 on DSK1DXX6B1PROD with RULES_PART 1
Costs of Compliance
We estimate that this AD will affect
380 products of U.S. registry. We also
estimate that it will take about 1 workhour per product to comply with the
basic requirements of this AD. The
average labor rate is $85 per work-hour.
Based on these figures, we estimate the
cost of this AD to the U.S. operators to
be $32,300, or $85 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
VerDate Mar<15>2010
14:45 Nov 08, 2010
Jkt 223001
section, Congress charges the FAA with
promoting safe flight of civil aircraft in
air commerce by prescribing regulations
for practices, methods, and procedures
the Administrator finds necessary for
safety in air commerce. This regulation
is within the scope of that authority
because it addresses an unsafe condition
that is likely to exist or develop on
products identified in this rulemaking
action.
Regulatory Findings
We determined that this AD will not
have federalism implications under
Executive Order 13132. This AD will
not have a substantial direct effect on
the States, on the relationship between
the national government and the States,
or on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify this AD:
1. Is not a ‘‘significant regulatory
action’’ under Executive Order 12866;
2. Is not a ‘‘significant rule’’ under the
DOT Regulatory Policies and Procedures
(44 FR 11034, February 26, 1979); and
3. Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
We prepared a regulatory evaluation
of the estimated costs to comply with
this AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Operations office between 9 a.m.
and 5 p.m., Monday through Friday,
except Federal holidays. The AD docket
contains the NPRM, the regulatory
evaluation, any comments received, and
other information. The street address for
the Docket Operations office (telephone
(800) 647–5527) is in the ADDRESSES
section. Comments will be available in
the AD docket shortly after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of the Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
■
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
68683
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
■
2010–23–11 Bombardier, Inc.: Amendment
39–16500. Docket No. FAA–2010–0700;
Directorate Identifier 2010–NM–123–AD.
Effective Date
(a) This airworthiness directive (AD)
becomes effective December 14, 2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Bombardier, Inc.
Model CL–600–2C10 (Regional Jet Series 700,
701, & 702), CL–600–2D15 (Regional Jet
Series 705), and CL–600–2D24 (Regional Jet
Series 900) airplanes, certificated in any
category, equipped with Thales angle of
attack transducers having part number (P/N)
C16258AA.
Subject
(d) Air Transport Association (ATA) of
America Code 27: Flight Controls.
Reason
(e) The mandatory continuing
airworthiness information (MCAI) states:
The manufacturer has informed Transport
Canada that a certain number of the resolver
stators, which were installed in the angle of
attack (AOA) transducers, were not cleaned
correctly. This condition can degrade the
AOA transducer performance at low
temperatures resulting in freezing of the AOA
transducer resolver, which may provide
inaccurate AOA data to the Stall Protection
System (SPS). If not corrected, this condition
can result in early or late activation of the
stick shaker and/or stick pusher.
These conditions could result in reduced
ability of the flight crew to maintain a safe
flight and landing of the airplane.
Compliance
(f) You are responsible for having the
actions required by this AD performed within
the compliance times specified, unless the
actions have already been done.
Inspection
(g) Within 750 flight hours after the
effective date of this AD, inspect the serial
number of each AOA transducer having P/N
C16258AA to determine if the serial number
is identified in paragraph 1.A. of Bombardier
Alert Service Bulletin A670BA–27–054,
Revision A, dated January 18, 2010, in
accordance with the Accomplishment
Instructions of Bombardier Alert Service
Bulletin A670BA–27–054, Revision A, dated
January 18, 2010. A review of airplane
maintenance records is acceptable in lieu of
this inspection if the serial number of the
AOA transducer can be conclusively
determined from that review.
(1) If the serial number is not listed in
paragraph 1.A. of Bombardier Alert Service
Bulletin A670BA–27–054, Revision A, dated
January 18, 2010, no further action is
E:\FR\FM\09NOR1.SGM
09NOR1
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Federal Register / Vol. 75, No. 216 / Tuesday, November 9, 2010 / Rules and Regulations
required by this AD other than compliance
with paragraph (h) of this AD.
(2) If the serial number is listed in
paragraph 1.A. of Bombardier Alert Service
Bulletin A670BA–27–054, Revision A, dated
January 18, 2010, and has the suffix ‘‘C’’, no
further action is required by this AD other
than compliance with paragraph (h) of this
AD.
(3) If the serial number is listed paragraph
1.A. of Bombardier Alert Service Bulletin
A670BA–27–054, Revision A, dated January
18, 2010, and does not have the suffix ‘‘C’’,
before further flight, replace the AOA
transducer with a new or serviceable
transducer, in accordance with Part C of the
Accomplishment Instructions of Bombardier
Alert Service Bulletin A670BA–27–054,
Revision A, dated January 18, 2010.
Note 1: To replace any AOA transducer,
the replacement AOA transducer must either
be outside of the affected serial numbers as
identified in paragraph 1.A. of Bombardier
Alert Service Bulletin A670BA–27–054,
Revision A, dated January 18, 2010, or have
the suffix ‘‘C’’.
(h) As of the effective date of this AD, no
AOA transducer having both a serial number
and P/N C16258AA as identified in
paragraph 1.A. of Bombardier Alert Service
Bulletin A670BA–27–054, Revision A, dated
January 18, 2010, may be installed on any
airplane unless the AOA transducer has been
inspected by the manufacturer and identified
with the suffix ‘‘C’’.
FAA AD Differences
wwoods2 on DSK1DXX6B1PROD with RULES_PART 1
Note 2: This AD differs from the MCAI
and/or service information as follows: No
differences.
Other FAA AD Provisions
(i) The following provisions also apply to
this AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York Aircraft
Certification Office (ACO), ANE–170, 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:
Program Manager, Continuing Operational
Safety, FAA, New York ACO, 1600 Stewart
Avenue, Suite 410, Westbury, New York
11590; telephone 516–228–7300; fax 516–
794–5531. Before using any approved AMOC
on any airplane to which the AMOC applies,
notify your 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
(44 U.S.C. 3501 et seq.), the Office of
Management and Budget (OMB) has
VerDate Mar<15>2010
14:45 Nov 08, 2010
Jkt 223001
approved the information collection
requirements and has assigned OMB Control
Number 2120–0056.
Related Information
(j) Refer to MCAI Canadian Airworthiness
Directive CF–2010–13, dated May 6, 2010;
and Bombardier Alert Service Bulletin
A670BA–27–054, Revision A, dated January
18, 2010; for related information.
Material Incorporated by Reference
(k) You must use Bombardier Alert Service
Bulletin A670BA–27–054,
Revision A, dated January 18, 2010, 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
ˆ
this AD, contact Bombardier, Inc., 400 Cote´
Vertu Road West, Dorval, Quebec H4S 1Y9,
Canada; telephone 514–855–5000; fax 514–
855–7401; e-mail
thd.crj@aero.bombardier.com; Internet https://
www.bombardier.com.
(3) You may review copies of the service
information at the FAA, Transport Airplane
Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the
availability of this material at the FAA, call
425–227–1221.
(4) You may also review copies of the
service information that is incorporated by
reference at the National Archives and
Records Administration (NARA). For
information on the availability of this
material at NARA, call 202–741–6030, or go
to: https://www.archives.gov/federal_register/
code_of_federal_regulations/ibr_locations.
html.
Issued in Renton, Washington, on October
21, 2010.
Michael Kaszycki,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2010–28089 Filed 11–8–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2010–0870; Directorate
Identifier 2010–CE–045–AD; Amendment
39–16505; AD 2010–23–16]
RIN 2120–AA64
Airworthiness Directives; Empresa
Brasileira de Aeronautica S.A.
(EMBRAER) Model EMB–500 Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for the
SUMMARY:
PO 00000
Frm 00004
Fmt 4700
Sfmt 4700
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:
It has been found the occurrences of failure
of the Flow Control Shutoff Valve (FCSOV)
in the closed position. Failure of the two
valves (left and right) can cause the loss of
the pneumatic source, and lead to loss of the
cabin pressurization.
Since this condition affects flight safety, a
corrective action is required. Thus, sufficient
reason exists to request compliance with this
AD.
We are issuing this AD to require
actions to correct the unsafe condition
on these products.
DATES: This AD becomes effective
December 14, 2010.
On December 14, 2010, 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 https://
www.regulations.gov or in person at
Document Management Facility, 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 service information identified in
this AD, contact EMBRAER Empresa
´
Brasileira de Aeronautica S.A., Phenom
Maintenance Support, Av. Brig. Farina
Lima, 2170, Sao Jose dos Campos—SP,
CEP: 12227–901—P.O. Box: 38/2,
BRASIL, telephone: ++55 12 3927–5383;
fax: ++55 12 3927–2610; E-mail:
reliability.executive@embraer.com.br;
Internet: https://www.embraer.com.br.
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.
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:
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 September 1, 2010 (75 FR
E:\FR\FM\09NOR1.SGM
09NOR1
Agencies
[Federal Register Volume 75, Number 216 (Tuesday, November 9, 2010)]
[Rules and Regulations]
[Pages 68682-68684]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-28089]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2010-0700; Directorate Identifier 2010-NM-123-AD;
Amendment 39-16500; AD 2010-23-11]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Model CL-600-2C10
(Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet Series
705), and CL-600-2D24 (Regional Jet Series 900) 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) 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:
The manufacturer has informed Transport Canada that a certain
number of the resolver stators, which were installed in the angle of
attack (AOA) transducers, were not cleaned correctly. This condition
can degrade the AOA transducer performance at low temperatures
resulting in freezing of the AOA transducer resolver, which may
provide inaccurate AOA data to the Stall Protection System (SPS). If
not corrected, this condition can result in early or late activation
of the stick shaker and/or stick pusher.
These conditions could result in reduced ability of the flight crew to
maintain a safe flight and landing of the airplane. We are issuing this
AD to require actions to correct the unsafe condition on these
products.
DATES: This AD becomes effective December 14, 2010.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 14,
2010.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov or in person at the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue, SE., Washington, DC.
FOR FURTHER INFORMATION CONTACT: Joseph Licata, Aerospace Engineer,
Avionics and Flight Test Branch, ANE-172, FAA, New York Aircraft
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury,
New York 11590; telephone (516) 228-7361; fax (516) 794-5531.
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 July 27, 2010 (75 FR
43882). That NPRM proposed to correct an unsafe condition for the
specified products. The MCAI states:
The manufacturer has informed Transport Canada that a certain
number of the resolver stators, which were installed in the angle of
attack (AOA) transducers, were not cleaned correctly. This condition
can degrade the AOA transducer performance at low temperatures
resulting in freezing of the AOA transducer resolver, which may
provide inaccurate AOA data to the Stall Protection System (SPS). If
not corrected, this condition
[[Page 68683]]
can result in early or late activation of the stick shaker and/or
stick pusher.
These conditions could result in reduced ability of the flight crew to
maintain a safe flight and landing of the airplane. The required
actions include an inspection to determine if certain AOA transducers
are installed and replacement of affected transducers. You may obtain
further information by examining the MCAI in the AD docket.
Comments
We gave the public the opportunity to participate in developing
this AD. We considered the comment received. Air Line Pilots
Association, International (ALPA), supports the NPRM.
Conclusion
We reviewed the available data, including the comment received, 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 our FAA policies. Any such differences
are highlighted in a NOTE within the AD.
Costs of Compliance
We estimate that this AD will affect 380 products of U.S. registry.
We also estimate that it will take about 1 work-hour per product to
comply with the basic requirements of this AD. The average labor rate
is $85 per work-hour. Based on these figures, we estimate the cost of
this AD to the U.S. operators to be $32,300, or $85 per product.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. ``Subtitle VII: Aviation
Programs,'' describes in more detail the scope of the Agency's
authority.
We are issuing this rulemaking under the authority described in
``Subtitle VII, Part A, Subpart III, Section 44701: General
requirements.'' Under that section, Congress charges the FAA with
promoting safe flight of civil aircraft in air commerce by prescribing
regulations for practices, methods, and procedures the Administrator
finds necessary for safety in air commerce. This regulation is within
the scope of that authority because it addresses an unsafe condition
that is likely to exist or develop on products identified in this
rulemaking action.
Regulatory Findings
We determined that this AD will not have federalism implications
under Executive Order 13132. This AD will not have a substantial direct
effect on the States, on the relationship between the national
government and the States, or on the distribution of power and
responsibilities among the various levels of government.
For the reasons discussed above, I certify this AD:
1. Is not a ``significant regulatory action'' under Executive Order
12866;
2. Is not a ``significant rule'' under the DOT Regulatory Policies
and Procedures (44 FR 11034, February 26, 1979); and
3. Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
We prepared a regulatory evaluation of the estimated costs to
comply with this AD and placed it in the AD docket.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov; or in person at the Docket Operations office
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays. The AD docket contains the NPRM, the regulatory evaluation,
any comments received, and other information. The street address for
the Docket Operations office (telephone (800) 647-5527) is in the
ADDRESSES section. Comments will be available in the AD docket shortly
after receipt.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of the Amendment
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:
2010-23-11 Bombardier, Inc.: Amendment 39-16500. Docket No. FAA-
2010-0700; Directorate Identifier 2010-NM-123-AD.
Effective Date
(a) This airworthiness directive (AD) becomes effective December
14, 2010.
Affected ADs
(b) None.
Applicability
(c) This AD applies to Bombardier, Inc. Model CL-600-2C10
(Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet
Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes,
certificated in any category, equipped with Thales angle of attack
transducers having part number (P/N) C16258AA.
Subject
(d) Air Transport Association (ATA) of America Code 27: Flight
Controls.
Reason
(e) The mandatory continuing airworthiness information (MCAI)
states:
The manufacturer has informed Transport Canada that a certain
number of the resolver stators, which were installed in the angle of
attack (AOA) transducers, were not cleaned correctly. This condition
can degrade the AOA transducer performance at low temperatures
resulting in freezing of the AOA transducer resolver, which may
provide inaccurate AOA data to the Stall Protection System (SPS). If
not corrected, this condition can result in early or late activation
of the stick shaker and/or stick pusher.
These conditions could result in reduced ability of the flight
crew to maintain a safe flight and landing of the airplane.
Compliance
(f) You are responsible for having the actions required by this
AD performed within the compliance times specified, unless the
actions have already been done.
Inspection
(g) Within 750 flight hours after the effective date of this AD,
inspect the serial number of each AOA transducer having P/N C16258AA
to determine if the serial number is identified in paragraph 1.A. of
Bombardier Alert Service Bulletin A670BA-27-054, Revision A, dated
January 18, 2010, in accordance with the Accomplishment Instructions
of Bombardier Alert Service Bulletin A670BA-27-054, Revision A,
dated January 18, 2010. A review of airplane maintenance records is
acceptable in lieu of this inspection if the serial number of the
AOA transducer can be conclusively determined from that review.
(1) If the serial number is not listed in paragraph 1.A. of
Bombardier Alert Service Bulletin A670BA-27-054, Revision A, dated
January 18, 2010, no further action is
[[Page 68684]]
required by this AD other than compliance with paragraph (h) of this
AD.
(2) If the serial number is listed in paragraph 1.A. of
Bombardier Alert Service Bulletin A670BA-27-054, Revision A, dated
January 18, 2010, and has the suffix ``C'', no further action is
required by this AD other than compliance with paragraph (h) of this
AD.
(3) If the serial number is listed paragraph 1.A. of Bombardier
Alert Service Bulletin A670BA-27-054, Revision A, dated January 18,
2010, and does not have the suffix ``C'', before further flight,
replace the AOA transducer with a new or serviceable transducer, in
accordance with Part C of the Accomplishment Instructions of
Bombardier Alert Service Bulletin A670BA-27-054, Revision A, dated
January 18, 2010.
Note 1: To replace any AOA transducer, the replacement AOA
transducer must either be outside of the affected serial numbers as
identified in paragraph 1.A. of Bombardier Alert Service Bulletin
A670BA-27-054, Revision A, dated January 18, 2010, or have the
suffix ``C''.
(h) As of the effective date of this AD, no AOA transducer
having both a serial number and P/N C16258AA as identified in
paragraph 1.A. of Bombardier Alert Service Bulletin A670BA-27-054,
Revision A, dated January 18, 2010, may be installed on any airplane
unless the AOA transducer has been inspected by the manufacturer and
identified with the suffix ``C''.
FAA AD Differences
Note 2: This AD differs from the MCAI and/or service information
as follows: No differences.
Other FAA AD Provisions
(i) The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York Aircraft Certification Office (ACO), ANE-170, 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: Program
Manager, Continuing Operational Safety, FAA, New York ACO, 1600
Stewart Avenue, Suite 410, Westbury, New York 11590; telephone 516-
228-7300; fax 516-794-5531. Before using any approved AMOC on any
airplane to which the AMOC applies, notify your 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 (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
(j) Refer to MCAI Canadian Airworthiness Directive CF-2010-13,
dated May 6, 2010; and Bombardier Alert Service Bulletin A670BA-27-
054, Revision A, dated January 18, 2010; for related information.
Material Incorporated by Reference
(k) You must use Bombardier Alert Service Bulletin A670BA-27-
054,
Revision A, dated January 18, 2010, 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
Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; telephone 514-855-5000; fax 514-855-
7401; e-mail thd.crj@aero.bombardier.com; Internet https://www.bombardier.com.
(3) You may review copies of the service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue, SW., Renton,
Washington. For information on the availability of this material at
the FAA, call 425-227-1221.
(4) You may also review copies of the service information that
is incorporated by reference at the National Archives and Records
Administration (NARA). For information on the availability of this
material at NARA, call 202-741-6030, or go to: https://www.archives.gov/federal_register/code_of_federal_regulations/ibr_locations.html.
Issued in Renton, Washington, on October 21, 2010.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-28089 Filed 11-8-10; 8:45 am]
BILLING CODE 4910-13-P