Airworthiness Directives; Bombardier, Inc. Airplanes, 73812-73813 [2014-28924]
Download as PDF
73812
Federal Register / Vol. 79, No. 239 / Friday, December 12, 2014 / Rules and Regulations
(6) You may view this 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.
(7) You may view this 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/cfr/ibrlocations.html.
Issued in Renton, Washington, on
November 28, 2014.
John P. Piccola, Jr.,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2014–28923 Filed 12–11–14; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2014–0567; Directorate
Identifier 2014–NM–124–AD; Amendment
39–18043; AD 2014–25–02]
RIN 2120–AA64
Airworthiness Directives; Bombardier,
Inc. Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
We are adopting a new
airworthiness directive (AD) for certain
Bombardier, Inc. Model CL–600–2B19
(Regional Jet Series 100 & 440)
airplanes. This AD was prompted by
issuance of revised certification
maintenance requirements for the
horizontal stabilizer trim actuator
(HSTA). This AD requires revising the
maintenance or inspection program. We
are issuing this AD to detect and correct
premature wear and cracking of the
HSTAs, which could result in reduced
structural integrity and reduced control
of the airplane due to the failure of
system components.
DATES: This AD becomes effective
January 16, 2015.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of January 16, 2015.
ADDRESSES: You may examine the AD
docket on the Internet at https://
www.regulations.gov/
#!documentDetail;D=FAA-2014-0567 or
in person at the Docket Management
Facility, U.S. Department of
Transportation, Docket Operations, M–
rljohnson on DSK3VPTVN1PROD with RULES
SUMMARY:
VerDate Sep<11>2014
14:38 Dec 11, 2014
Jkt 235001
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE.,
Washington, DC.
For service information identified in
this AD, contact Bombardier, Inc., 400
ˆ
´
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 view
this 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.
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,
NY 11590; telephone 516–228–7318; fax
516–794–5531.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Bombardier, Inc. Model
CL–600–2B19 (Regional Jet Series 100 &
440) airplanes. The NPRM published in
the Federal Register on August 14, 2014
(79 FR 47594).
Transport Canada Civil Aviation
(TCCA), which is the aviation authority
for Canada, has issued Canadian
Airworthiness Directive CF–2014–13,
dated April 17, 2014 (referred to after
this as the Mandatory Continuing
Airworthiness Information, or ‘‘the
MCAI’’), to correct an unsafe condition
for certain Bombardier, Inc. Model CL–
600–2B19 (Regional Jet Series 100 &
440) airplanes. The MCAI states:
A revision has been made to Part 2 of the
Canadair Regional Jet Maintenance
Requirements Manual (MRM), Appendix A—
Certification Maintenance Requirements
[CMR] which introduces a new task for the
HSTA. Failure to comply with the CMR task
could lead to an unsafe condition.
This [Canadian] AD is issued to ensure that
premature wear and cracking of the affected
components are detected and corrected. [This
condition could result in reduced structural
integrity and reduced control of the airplane
due to the failure of system components.]
You may examine the MCAI in the
AD docket on the Internet at https://
www.regulations.gov/
#!documentDetail;D=FAA-2014-05670002.
Comments
We gave the public the opportunity to
participate in developing this AD. We
received no comments on the NPRM (79
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
FR 47594, August 14, 2014) or on the
determination of the cost to the public.
Conclusion
We reviewed the relevant data and
determined that air safety and the
public interest require adopting this AD
as proposed except for minor editorial
changes. We have determined that these
minor changes:
• Are consistent with the intent that
was proposed in the NPRM (79 FR
47594, August 14, 2014) for correcting
the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM (79 FR 47594,
August 14, 2014).
Costs of Compliance
We estimate that this AD affects 416
airplanes 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. Required parts will cost
about $0 per product. Based on these
figures, we estimate the cost of this AD
on U.S. operators to be $35,360, 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 that this AD:
E:\FR\FM\12DER1.SGM
12DER1
Federal Register / Vol. 79, No. 239 / Friday, December 12, 2014 / Rules and Regulations
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.
(d) Subject
Air Transport Association (ATA) of
America Code 55, Stabilizers.
Examining the AD Docket
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
You may examine the AD docket on
the Internet at https://
www.regulations.gov/
#!docketDetail;D=FAA-2014-0567; 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
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.
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:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2014–25–02 Bombardier, Inc.: Amendment
39–18043. Docket No. FAA–2014–0567;
Directorate Identifier 2014–NM–124–AD.
(a) Effective Date
This AD becomes effective January 16,
2015.
rljohnson on DSK3VPTVN1PROD with RULES
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model
CL–600–2B19 (Regional Jet Series 100 & 440)
airplanes, certificated in any category,
equipped with horizontal stabilizer trim
actuator (HSTA) part number (P/N)
601R92305–7 (vendor P/N 8396–5).
VerDate Sep<11>2014
14:38 Dec 11, 2014
Jkt 235001
(e) Reason
This AD was prompted by issuance of
revised certification maintenance
requirements (CMR) for the HSTA. We are
issuing this AD to detect and correct
premature wear and cracking of certain
HSTAs, which could result in reduced
structural integrity and reduced control of
the airplane due to the failure of system
components.
(g) Maintenance or Inspection Program
Revision
Within 30 days after the effective date of
this AD, revise the maintenance or inspection
program, as applicable, to incorporate the
information specified in Task C27–40–103–
05, ‘‘Restoration (Overhaul) of the HSTA,’’ of
Bombardier Temporary Revision (TR) 2A–58,
dated January 31, 2014, into Appendix A—
Certification Maintenance Requirements
(CMR), of Part 2, of the Bombardier CL–600–
2B19 Maintenance Requirements Manual
(MRM). The initial compliance time for
accomplishing Task C27–40–103–05,
‘‘Restoration (Overhaul) of the HSTA,’’ of
Bombardier Temporary Revision (TR) 2A–58,
dated January 31, 2014, is at the applicable
phase-in time specified in Bombardier TR
2A–58, dated January 31, 2014, or within 30
days after the effective date of this AD,
whichever occurs later. The revision required
by paragraph (g) of this AD may be done by
inserting a copy of Bombardier TR 2A–58,
dated January 31, 2014, into Appendix A—
CMR, of Part 2 of the Bombardier CL–600–
2B19 MRM. When Bombardier TR 2A–58,
dated January 31, 2014, has been included in
the general revisions of the Bombardier CL–
600–2B19 MRM, the general revisions may be
inserted into the MRM, provided the relevant
information in the general revision is
identical to that in Bombardier TR 2A–58,
dated January 31, 2014.
(h) No Alternative Actions and Intervals
After accomplishing the revision required
by paragraph (g) of this AD, no alternative
actions (e.g., inspections) or intervals may be
used unless the actions or intervals are
approved as an alternative method of
compliance (AMOC) in accordance with the
procedures specified in paragraph (i)(1) of
this AD.
(i) Other FAA AD Provisions
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. 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
PO 00000
Frm 00013
Fmt 4700
Sfmt 9990
73813
directly to the ACO, send it to 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) Contacting the Manufacturer: For any
requirement in this AD to obtain corrective
actions from a manufacturer, the action must
be accomplished using a method approved
by the Manager, New York ACO, ANE–170,
Engine and Propeller Directorate, FAA; or
Transport Canada Civil Aviation (TCCA); or
Bombardier, Inc.’s TCCA Design Approval
Organization (DAO). If approved by the DAO,
the approval must include the DAOauthorized signature.
(j) Related Information
Refer to Mandatory Continuing
Airworthiness Information (MCAI) Canadian
Airworthiness Directive CF–2014–13, dated
April 17, 2014, for related information. This
MCAI may be found in the AD docket on the
Internet at https://www.regulations.gov by
searching for and locating Docket No. FAA–
2014–0567.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) Bombardier Temporary Revision 2A–58,
dated January 31, 2014, to Appendix A—
Certification Maintenance Requirements, of
Part 2 of the Bombardier CL–600–2B19
Maintenance Requirements Manual.
(ii) Reserved.
(3) 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; email thd.crj@
aero.bombardier.com; Internet https://
www.bombardier.com.
(4) You may view this 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.
(5) You may view this 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/cfr/ibrlocations.html.
Issued in Renton, Washington, on
November 28, 2014.
John P. Piccola, Jr.,
Acting Manager, Transport Airplane
Directorate, Aircraft Certification Service.
[FR Doc. 2014–28924 Filed 12–11–14; 8:45 am]
BILLING CODE 4910–13–P
E:\FR\FM\12DER1.SGM
12DER1
Agencies
[Federal Register Volume 79, Number 239 (Friday, December 12, 2014)]
[Rules and Regulations]
[Pages 73812-73813]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2014-28924]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-0567; Directorate Identifier 2014-NM-124-AD;
Amendment 39-18043; AD 2014-25-02]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc. Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: We are adopting a new airworthiness directive (AD) for certain
Bombardier, Inc. Model CL-600-2B19 (Regional Jet Series 100 & 440)
airplanes. This AD was prompted by issuance of revised certification
maintenance requirements for the horizontal stabilizer trim actuator
(HSTA). This AD requires revising the maintenance or inspection
program. We are issuing this AD to detect and correct premature wear
and cracking of the HSTAs, which could result in reduced structural
integrity and reduced control of the airplane due to the failure of
system components.
DATES: This AD becomes effective January 16, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 16,
2015.
ADDRESSES: You may examine the AD docket on the Internet at https://www.regulations.gov/#!documentDetail;D=FAA-2014-0567 or in person at
the Docket 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.
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; email
thd.crj@aero.bombardier.com; Internet https://www.bombardier.com. You
may view this 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.
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, NY
11590; telephone 516-228-7318; fax 516-794-5531.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would apply to certain Bombardier, Inc.
Model CL-600-2B19 (Regional Jet Series 100 & 440) airplanes. The NPRM
published in the Federal Register on August 14, 2014 (79 FR 47594).
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2014-13, dated April 17, 2014 (referred to after this as the Mandatory
Continuing Airworthiness Information, or ``the MCAI''), to correct an
unsafe condition for certain Bombardier, Inc. Model CL-600-2B19
(Regional Jet Series 100 & 440) airplanes. The MCAI states:
A revision has been made to Part 2 of the Canadair Regional Jet
Maintenance Requirements Manual (MRM), Appendix A--Certification
Maintenance Requirements [CMR] which introduces a new task for the
HSTA. Failure to comply with the CMR task could lead to an unsafe
condition.
This [Canadian] AD is issued to ensure that premature wear and
cracking of the affected components are detected and corrected.
[This condition could result in reduced structural integrity and
reduced control of the airplane due to the failure of system
components.]
You may examine the MCAI in the AD docket on the Internet at https://www.regulations.gov/#!documentDetail;D=FAA-2014-0567-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. We received no comments on the NPRM (79 FR 47594, August 14,
2014) or on the determination of the cost to the public.
Conclusion
We reviewed the relevant data and determined that air safety and
the public interest require adopting this AD as proposed except for
minor editorial changes. We have determined that these minor changes:
Are consistent with the intent that was proposed in the
NPRM (79 FR 47594, August 14, 2014) for correcting the unsafe
condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM (79 FR 47594, August 14, 2014).
Costs of Compliance
We estimate that this AD affects 416 airplanes 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. Required parts will cost about $0 per product.
Based on these figures, we estimate the cost of this AD on U.S.
operators to be $35,360, 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 that this AD:
[[Page 73813]]
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.
Examining the AD Docket
You may examine the AD docket on the Internet at https://www.regulations.gov/#!docketDetail;D=FAA-2014-0567; 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 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.
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
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 airworthiness
directive (AD):
2014-25-02 Bombardier, Inc.: Amendment 39-18043. Docket No. FAA-
2014-0567; Directorate Identifier 2014-NM-124-AD.
(a) Effective Date
This AD becomes effective January 16, 2015.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Bombardier, Inc. Model CL-600-2B19 (Regional
Jet Series 100 & 440) airplanes, certificated in any category,
equipped with horizontal stabilizer trim actuator (HSTA) part number
(P/N) 601R92305-7 (vendor P/N 8396-5).
(d) Subject
Air Transport Association (ATA) of America Code 55, Stabilizers.
(e) Reason
This AD was prompted by issuance of revised certification
maintenance requirements (CMR) for the HSTA. We are issuing this AD
to detect and correct premature wear and cracking of certain HSTAs,
which could result in reduced structural integrity and reduced
control of the airplane due to the failure of system components.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Maintenance or Inspection Program Revision
Within 30 days after the effective date of this AD, revise the
maintenance or inspection program, as applicable, to incorporate the
information specified in Task C27-40-103-05, ``Restoration
(Overhaul) of the HSTA,'' of Bombardier Temporary Revision (TR) 2A-
58, dated January 31, 2014, into Appendix A--Certification
Maintenance Requirements (CMR), of Part 2, of the Bombardier CL-600-
2B19 Maintenance Requirements Manual (MRM). The initial compliance
time for accomplishing Task C27-40-103-05, ``Restoration (Overhaul)
of the HSTA,'' of Bombardier Temporary Revision (TR) 2A-58, dated
January 31, 2014, is at the applicable phase-in time specified in
Bombardier TR 2A-58, dated January 31, 2014, or within 30 days after
the effective date of this AD, whichever occurs later. The revision
required by paragraph (g) of this AD may be done by inserting a copy
of Bombardier TR 2A-58, dated January 31, 2014, into Appendix A--
CMR, of Part 2 of the Bombardier CL-600-2B19 MRM. When Bombardier TR
2A-58, dated January 31, 2014, has been included in the general
revisions of the Bombardier CL-600-2B19 MRM, the general revisions
may be inserted into the MRM, provided the relevant information in
the general revision is identical to that in Bombardier TR 2A-58,
dated January 31, 2014.
(h) No Alternative Actions and Intervals
After accomplishing the revision required by paragraph (g) of
this AD, no alternative actions (e.g., inspections) or intervals may
be used unless the actions or intervals are approved as an
alternative method of compliance (AMOC) in accordance with the
procedures specified in paragraph (i)(1) of this AD.
(i) Other FAA AD Provisions
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. 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 ACO, send it to 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) Contacting the Manufacturer: For any requirement in this AD
to obtain corrective actions from a manufacturer, the action must be
accomplished using a method approved by the Manager, New York ACO,
ANE-170, Engine and Propeller Directorate, FAA; or Transport Canada
Civil Aviation (TCCA); or Bombardier, Inc.'s TCCA Design Approval
Organization (DAO). If approved by the DAO, the approval must
include the DAO-authorized signature.
(j) Related Information
Refer to Mandatory Continuing Airworthiness Information (MCAI)
Canadian Airworthiness Directive CF-2014-13, dated April 17, 2014,
for related information. This MCAI may be found in the AD docket on
the Internet at https://www.regulations.gov by searching for and
locating Docket No. FAA-2014-0567.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) of the service information listed
in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
(2) You must use this service information as applicable to do
the actions required by this AD, unless this AD specifies otherwise.
(i) Bombardier Temporary Revision 2A-58, dated January 31, 2014,
to Appendix A--Certification Maintenance Requirements, of Part 2 of
the Bombardier CL-600-2B19 Maintenance Requirements Manual.
(ii) Reserved.
(3) 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; email thd.crj@aero.bombardier.com; Internet https://www.bombardier.com.
(4) You may view this 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.
(5) You may view this 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/cfr/ibr-locations.html.
Issued in Renton, Washington, on November 28, 2014.
John P. Piccola, Jr.,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2014-28924 Filed 12-11-14; 8:45 am]
BILLING CODE 4910-13-P