Airworthiness Directives; Bombardier, Inc. Airplanes, 27314-27315 [2013-11169]
Download as PDF
27314
Federal Register / Vol. 78, No. 91 / Friday, May 10, 2013 / Proposed Rules
DEPARTMENT OF TRANSPORTATION
Examining the AD Docket
Federal Aviation Administration
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 this proposed AD, 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.
14 CFR Part 39
[Docket No. FAA–2013–0370; Directorate
Identifier 2013–NM–034–AD]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc. Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for certain
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. This proposed AD was
prompted by a report that traces of oil
could be found in the crew oxygen
system due to the use of incorrect
pressure testing procedures during
manufacturing. This proposed AD
would require cleaning the crew oxygen
system. We are proposing this AD to
detect and correct oil contaminants,
which could cause an ignition and
result in a fire in the oxygen system.
DATES: We must receive comments on
this proposed AD by June 24, 2013.
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, between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For service information identified in
this proposed AD, contact Bombardier,
ˆ
Inc., 400 Cote-Vertu Road West, Dorval,
´
Quebec H4S 1Y9, Canada; telephone
514–855–5000; fax 514–855–7401; email
thd.crj@aero.bombardier.com; Internet
https://www.bombardier.com. You may
review copies of the referenced service
information at the FAA, Transport
Airplane Directorate, 1601 Lind Avenue
SW., Renton, WA. For information on
the availability of this material at the
FAA, call 425–227–1221.
rmajette on DSK2TPTVN1PROD with PROPOSALS-1
SUMMARY:
VerDate Mar<15>2010
14:33 May 09, 2013
Jkt 229001
FOR FURTHER INFORMATION CONTACT:
Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems
Branch, ANE–171, FAA, New York
Aircraft Certification Office, 1600
Stewart Avenue, Suite 410, Westbury,
New York 11590; telephone (516) 228–
7318; fax (516) 794–5531.
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–2013–0370; Directorate Identifier
2013–NM–034–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 based on 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 Transport Canada Civil Agency,
which is the aviation authority for
Canada, has issued Canadian
Airworthiness Directive CF–2013–01,
dated January 22, 2013 (referred to after
this as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for the specified products. The MCAI
states:
It was found that traces of oil could be
present in the crew oxygen system due to the
use of incorrect pressure testing procedures
during manufacturing. Field sampling of nine
aeroplanes have confirmed this condition.
When the oxygen system is used, oil
contaminants can cause an ignition and
result in a fire in the oxygen system.
PO 00000
Frm 00007
Fmt 4702
Sfmt 4702
This [TCCA] AD mandates the cleaning of
the crew oxygen system to reduce oil
contaminants to a safe level.
You may obtain further information by
examining the MCAI in the AD docket.
Relevant Service Information
Bombardier, Inc. has issued Service
Bulletin 670BA–35–012, Revision A,
dated November 26, 2012. The actions
described in this service information are
intended to correct the unsafe condition
identified in the MCAI.
FAA’s Determination and Requirements
of This 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 the State of
Design Authority, we have been notified
of the unsafe condition described in the
MCAI and service information
referenced above. We are proposing this
AD because we evaluated all pertinent
information and determined an unsafe
condition exists and is likely to exist or
develop on other products of the same
type design.
Costs of Compliance
Based on the service information, we
estimate that this proposed AD would
affect about 400 products of U.S.
registry. We also estimate that it would
take about 51 work-hours per product to
comply with the basic requirements of
this proposed AD. The average labor
rate is $85 per work-hour. Required
parts would cost about $827 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 the
proposed AD on U.S. operators to be
$2,064,800, or $5,162 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
E:\FR\FM\10MYP1.SGM
10MYP1
Federal Register / Vol. 78, No. 91 / Friday, May 10, 2013 / Proposed Rules
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);
3. Will not affect intrastate aviation in
Alaska; and
4. 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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new AD:
rmajette on DSK2TPTVN1PROD with PROPOSALS-1
■
Bombardier, Inc.: Docket No. FAA–2013–
0370; Directorate Identifier 2013–NM–
034–AD.
(a) Comments Due Date
We must receive comments by June 24,
2013.
(b) Affected ADs
None.
VerDate Mar<15>2010
14:33 May 09, 2013
Jkt 229001
(c) Applicability
This AD applies to Bombardier, Inc. Model
CL–600–2C10 (Regional Jet Series 700, 701,
& 702) airplanes, serial numbers 10002
through 10265 inclusive; and Model CL–600–
2D15 (Regional Jet Series 705) and CL–600–
2D24 (Regional Jet Series 900) airplanes,
serial numbers 15002 through 15153
inclusive, 15156 and 15157; certificated in
any category.
(d) Subject
Air Transport Association (ATA) of
America Code 35, Oxygen.
(e) Reason
This AD was prompted by a report that
traces of oil could be found in the crew
oxygen system due to the use of incorrect
pressure testing procedures during
manufacturing. We are issuing this AD to
detect and correct oil contaminants, which
could cause an ignition and result in a fire
in the oxygen system.
(f) Compliance
You are responsible for having the actions
required by this AD performed within the
compliance times specified, unless the
actions have already been done.
(g) Actions
Within 6,600 flight hours or 36 months
after the effective date of this AD, whichever
occurs first: Clean the crew oxygen system,
in accordance with the Accomplishment
Instructions of Bombardier Service Bulletin
670BA–35–012, Revision A, dated November
26, 2012.
(h) Credit for Previous Actions
This paragraph provides credit for actions
required by paragraph (g) of this AD, if those
actions were performed before the effective
date of this AD using Bombardier Service
Bulletin 670BA–35–012, dated August 3,
2012, which is not incorporated by reference.
(i) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, 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. In
accordance with 14 CFR 39.19, send your
request to your principal inspector or local
Flight Standards District Office, as
appropriate. If sending information directly
to the, send it to ATTN: Program Manager,
Continuing Operational Safety, FAA, New
York ACO, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516–228–
7300; fax 516–794–5531. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
inspector, the manager of the local flight
standards district office/certificate holding
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
PO 00000
Frm 00008
Fmt 4702
Sfmt 4702
27315
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.
(j) Related Information
Refer to Mandatory Continuing
Airworthiness Information (MCAI) Canadian
Airworthiness Directive CF–2013–01, dated
January 22, 2013, and Bombardier Service
Bulletin 670BA–35–012, Revision A, dated
November 26, 2012, for related information.
Issued in Renton, Washington, on May 2,
2013.
Ali Bahrami,
Manager, Transport Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2013–11169 Filed 5–9–13; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2013–0369; Directorate
Identifier 2012–NM–128–AD]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for all The
Boeing Company Model 757 airplanes.
This proposed AD was prompted by
reports of fractured rudder pedal
pushrod connecting bolts in a rudder
pedal assembly. This proposed AD
would require repetitive replacements
of the rudder pedal pushrod connecting
bolts and repetitive inspections of the
rudder pedal assembly bolt holes in
each of the captain and the first officer
rudder pedal assemblies, and if
necessary, repair or replacement of
worn rudder pedal assemblies. We are
proposing this AD to prevent fracture of
the rudder pedal pushrod connecting
bolts during pedal use, which could
result in a large involuntary input to the
rudder, nose-wheel steering, and
braking systems, leading to a runway
excursion.
DATES: We must receive comments on
this proposed AD by June 24, 2013.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
SUMMARY:
E:\FR\FM\10MYP1.SGM
10MYP1
Agencies
[Federal Register Volume 78, Number 91 (Friday, May 10, 2013)]
[Proposed Rules]
[Pages 27314-27315]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-11169]
[[Page 27314]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2013-0370; Directorate Identifier 2013-NM-034-AD]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: We propose to adopt a new airworthiness directive (AD) for
certain 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. This proposed AD was prompted by a
report that traces of oil could be found in the crew oxygen system due
to the use of incorrect pressure testing procedures during
manufacturing. This proposed AD would require cleaning the crew oxygen
system. We are proposing this AD to detect and correct oil
contaminants, which could cause an ignition and result in a fire in the
oxygen system.
DATES: We must receive comments on this proposed AD by June 24, 2013.
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, between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
For service information identified in this proposed 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; email
thd.crj@aero.bombardier.com; Internet https://www.bombardier.com. You
may review copies of the referenced service information at the FAA,
Transport Airplane Directorate, 1601 Lind Avenue SW., Renton, WA. For
information on the availability of this material at the FAA, call 425-
227-1221.
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 this proposed AD, 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.
FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office, 1600 Stewart Avenue, Suite 410, Westbury, New
York 11590; telephone (516) 228-7318; fax (516) 794-5531.
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-2013-0370;
Directorate Identifier 2013-NM-034-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 based on 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 Transport Canada Civil Agency, which is the aviation authority
for Canada, has issued Canadian Airworthiness Directive CF-2013-01,
dated January 22, 2013 (referred to after this as the Mandatory
Continuing Airworthiness Information, or ``the MCAI''), to correct an
unsafe condition for the specified products. The MCAI states:
It was found that traces of oil could be present in the crew
oxygen system due to the use of incorrect pressure testing
procedures during manufacturing. Field sampling of nine aeroplanes
have confirmed this condition. When the oxygen system is used, oil
contaminants can cause an ignition and result in a fire in the
oxygen system.
This [TCCA] AD mandates the cleaning of the crew oxygen system
to reduce oil contaminants to a safe level.
You may obtain further information by examining the MCAI in the AD
docket.
Relevant Service Information
Bombardier, Inc. has issued Service Bulletin 670BA-35-012, Revision
A, dated November 26, 2012. The actions described in this service
information are intended to correct the unsafe condition identified in
the MCAI.
FAA's Determination and Requirements of This 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 the State of Design Authority, we have
been notified of the unsafe condition described in the MCAI and service
information referenced above. We are proposing this AD because we
evaluated all pertinent information and determined an unsafe condition
exists and is likely to exist or develop on other products of the same
type design.
Costs of Compliance
Based on the service information, we estimate that this proposed AD
would affect about 400 products of U.S. registry. We also estimate that
it would take about 51 work-hours per product to comply with the basic
requirements of this proposed AD. The average labor rate is $85 per
work-hour. Required parts would cost about $827 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 the proposed AD on U.S. operators to
be $2,064,800, or $5,162 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
[[Page 27315]]
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);
3. Will not affect intrastate aviation in Alaska; and
4. 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
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:
Bombardier, Inc.: Docket No. FAA-2013-0370; Directorate Identifier
2013-NM-034-AD.
(a) Comments Due Date
We must receive comments by June 24, 2013.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model CL-600-2C10 (Regional
Jet Series 700, 701, & 702) airplanes, serial numbers 10002 through
10265 inclusive; and Model CL-600-2D15 (Regional Jet Series 705) and
CL-600-2D24 (Regional Jet Series 900) airplanes, serial numbers
15002 through 15153 inclusive, 15156 and 15157; certificated in any
category.
(d) Subject
Air Transport Association (ATA) of America Code 35, Oxygen.
(e) Reason
This AD was prompted by a report that traces of oil could be
found in the crew oxygen system due to the use of incorrect pressure
testing procedures during manufacturing. We are issuing this AD to
detect and correct oil contaminants, which could cause an ignition
and result in a fire in the oxygen system.
(f) Compliance
You are responsible for having the actions required by this AD
performed within the compliance times specified, unless the actions
have already been done.
(g) Actions
Within 6,600 flight hours or 36 months after the effective date
of this AD, whichever occurs first: Clean the crew oxygen system, in
accordance with the Accomplishment Instructions of Bombardier
Service Bulletin 670BA-35-012, Revision A, dated November 26, 2012.
(h) Credit for Previous Actions
This paragraph provides credit for actions required by paragraph
(g) of this AD, if those actions were performed before the effective
date of this AD using Bombardier Service Bulletin 670BA-35-012,
dated August 3, 2012, which is not incorporated by reference.
(i) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, 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. In accordance with 14 CFR
39.19, send your request to your principal inspector or local Flight
Standards District Office, as appropriate. If sending information
directly to the, send it to ATTN: Program Manager, Continuing
Operational Safety, FAA, New York ACO, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516-228-7300; fax 516-794-5531.
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
local flight standards district office/certificate holding 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.
(j) Related Information
Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian Airworthiness Directive CF-2013-01, dated January 22, 2013,
and Bombardier Service Bulletin 670BA-35-012, Revision A, dated
November 26, 2012, for related information.
Issued in Renton, Washington, on May 2, 2013.
Ali Bahrami,
Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2013-11169 Filed 5-9-13; 8:45 am]
BILLING CODE 4910-13-P