Airworthiness Directives; Bombardier, Inc., Airplanes, 26352-26354 [2018-11827]
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26352
Federal Register / Vol. 83, No. 110 / Thursday, June 7, 2018 / Rules and Regulations
(2) Airworthy Product: 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, Small Airplane Standards
Branch, FAA; or the European Aviation
Safety Agency (EASA).
(h) Related Information
Refer to MCAI EASA AD No. 2018–0057,
dated March 14, 2018, for related
information. You may examine the MCAI on
the internet at https://www.regulations.gov by
searching for and locating Docket No. FAA–
2018–0462.
(i) 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 the AD specifies otherwise.
(i) LET Aircraft Industries Mandatory
Bulletin MB No. L410UVP–E/143a, Revision
2, dated March 7, 2018.
(ii) LET Aircraft Industries Documentation
Bulletin DB No. L410UVP–E/268d, dated
May 9, 2018.
(3) For service information identified in
this AD, contact Aircraft Industries, a.s., 686
04 Kunovice 1177, Czech Republic; phone:
+420 572 817 664; fax: +420 572 816 112;
email: pps@let.cz; internet: https://www.let.cz/
clanek_267_objednavka-bulletinovesluzby.html.
(4) You may view this service information
at FAA, Policy and Innovation Division, 901
Locust, Kansas City, Missouri 64106. For
information on the availability of this
material at the FAA, call (816) 329–4148. It
is also available on the internet at https://
www.regulations.gov by searching for
locating Docket No. FAA–2018–0462.
(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 Kansas City, Missouri, on May
11, 2018.
Melvin J. Johnson,
Aircraft Certification Service, Deputy
Director, Policy and Innovation Division,
AIR–601.
sradovich on DSK3GMQ082PROD with RULES
[FR Doc. 2018–11930 Filed 6–6–18; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2017–1175; Product
Identifier 2017–NM–087–AD; Amendment
39–19300; AD 2018–11–12]
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 all
Bombardier, Inc., Model CL–600–2C10
(Regional Jet Series 700, 701, & 702)
airplanes, Model CL–600–2D15
(Regional Jet Series 705) airplanes,
Model CL–600–2D24 (Regional Jet
Series 900) airplanes, and Model CL–
600–2E25 (Regional Jet Series 1000)
airplanes. This AD was prompted by a
report that Belleville washers installed
on the shimmy damper of the main
landing gear (MLG) may fail due to
fatigue. This AD requires revising the
maintenance or inspection program, as
applicable, to incorporate a repetitive
task specified in the maintenance
review board (MRB) report. We are
issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective July 12,
2018.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of July 12, 2018.
ADDRESSES: For service information
identified in this final rule, contact
ˆ
Bombardier, Inc., 400 Cote-Vertu Road
´
West, Dorval, Quebec H4S 1Y9, Canada;
Widebody Customer Response Center
North America toll-free telephone 1–
866–538–1247 or direct-dial telephone
1–514–855–2999; fax 514–855–7401;
email ac.yul@aero.bombardier.com;
internet https://www.bombardier.com.
You may view this referenced service
information at the FAA, Transport
Standards Branch, 2200 South 216th St.,
Des Moines, WA. For information on the
availability of this material at the FAA,
call 206–231–3195. It is also available
on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
1175.
SUMMARY:
Examining the AD Docket
You may examine the AD docket on
the internet at https://
VerDate Sep<11>2014
15:41 Jun 06, 2018
Jkt 244001
PO 00000
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Fmt 4700
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www.regulations.gov by searching for
and locating Docket No. FAA–2017–
1175; 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 Office (telephone 800–647–
5527) is 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 20590.
FOR FURTHER INFORMATION CONTACT:
Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems
Section, FAA, New York ACO Branch,
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 all Bombardier, Inc., Model
CL–600–2C10 (Regional Jet Series 700,
701, & 702) airplanes, Model CL–600–
2D15 (Regional Jet Series 705) airplanes,
Model CL–600–2D24 (Regional Jet
Series 900) airplanes, and Model CL–
600–2E25 (Regional Jet Series 1000)
airplanes. The NPRM published in the
Federal Register on January 2, 2018 (83
FR 83) (‘‘the NPRM’’).
Transport Canada Civil Aviation
(TCCA), which is the aviation authority
for Canada, has issued Canadian AD
CF–2017–14, dated April 21, 2017
(referred to after this as the Mandatory
Continuing Airworthiness Information,
or ‘‘the MCAI’’), to correct an unsafe
condition for all Bombardier, Inc.,
Model CL–600–2C10 (Regional Jet
Series 700, 701, & 702) airplanes, Model
CL–600–2D15 (Regional Jet Series 705)
airplanes, Model CL–600–2D24
(Regional Jet Series 900) airplanes, and
Model CL–600–2E25 (Regional Jet Series
1000) airplanes. The MCAI states:
It has been found that Belleville washers
installed on the Main Landing Gear (MLG)
Shimmy Damper may fail in fatigue. A failed
washer segment migrating into the piston
cavity may interfere with piston travel. As a
result, shimmy damper performance would
be compromised, MLG shimmy could occur
and potentially lead to a MLG failure.
As a result of this investigation, a
restoration task has been added for Belleville
washers’ replacement at 20,000 flight cycles,
during MLG overhaul. For aeroplanes that
have passed the 20,000 flight cycle threshold,
a phase-in period is defined.
This [Canadian] AD is issued to mandate
the Maintenance Review Board (MRB)
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Federal Register / Vol. 83, No. 110 / Thursday, June 7, 2018 / Rules and Regulations
revised task for the affected aeroplanes
models.
You may examine the MCAI in the AD
docket on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2017–
1175.
Comments
We gave the public the opportunity to
participate in developing this AD. The
following presents the comment
received on the NPRM and the FAA’s
response to that comment.
Request to the Contact Manufacturer
for Service Information
Bombardier stated that task number
320100–229, Restoration (Belleville
Washer Replacement) of the MLG
Shimmy Damper, of the MRB Report of
the Bombardier CRJ700/900/1000
Maintenance Requirements Manual
(MRM)—Part 1, Volume 1, CSP B–053,
Revision 17, dated June 25, 2017, is
currently specified in paragraph (g) of
the proposed AD. Bombardier
commented that it is planning to issue
Revision 18 of the service information
by June 25, 2018. Bombardier stated to
contact Bombardier for the latest service
information should the AD be published
after June 25, 2018.
We expect to issue this AD prior to
the anticipated date of release of new
service information, and we do not
agree to delay issuance of this AD until
new service information is released.
However, if new service information is
released after this AD is issued,
operators may request approval of an
alternative method of compliance
(AMOC) under the provisions of
paragraph (j)(1) of this AD. We have not
changed this AD regarding this issue.
sradovich on DSK3GMQ082PROD with RULES
Conclusion
We reviewed the relevant data,
considered the comment received, 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 for
correcting the unsafe condition; and
• Do not add any additional burden
upon the public than was already
proposed in the NPRM.
Related Service Information Under 1
CFR Part 51
Bombardier has issued MRB report
task number 320100–229, Restoration
(Belleville Washer Replacement) of the
MLG Shimmy Damper, of the MRB
Report of the Bombardier CRJ700/900/
1000 Maintenance Requirements
VerDate Sep<11>2014
15:41 Jun 06, 2018
Jkt 244001
Manual (MRM)—Part 1, Volume 1, CSP
B–053, Revision 17, dated June 25,
2017. This service information describes
the restoration (Belleville Washer
Replacement) of the MLG shimmy
damper. This service information is
reasonably available because the
interested parties have access to it
through their normal course of business
or by the means identified in the
ADDRESSES section.
Costs of Compliance
We estimate that this AD affects 544
airplanes of U.S. registry.
We estimate the following costs to
comply with this AD:
We have determined that revising the
maintenance or inspection program
takes an average of 90 work-hours per
operator, although we recognize that
this number may vary from operator to
operator. In the past, we have estimated
that this action takes 1 work-hour per
airplane. Since operators incorporate
maintenance or inspection program
changes for their affected fleet(s), we
have determined that a per-operator
estimate is more accurate than a perairplane estimate. Therefore, we
estimate the total cost per operator to be
$7,650 (90 work-hours x $85 per workhour).
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.
This AD is issued in accordance with
authority delegated by the Executive
Director, Aircraft Certification Service,
as authorized by FAA Order 8000.51C.
In accordance with that order, issuance
of ADs is normally a function of the
Compliance and Airworthiness
Division, but during this transition
period, the Executive Director has
delegated the authority to issue ADs
applicable to transport category
PO 00000
Frm 00007
Fmt 4700
Sfmt 4700
26353
airplanes to the Director of the System
Oversight Division.
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:
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.
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):
■
2018–11–12 Bombardier, Inc., Airplanes:
Amendment 39–19300; Docket No.
FAA–2017–1175; Product Identifier
2017–NM–087–AD.
(a) Effective Date
This AD is effective July 12, 2018.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Bombardier, Inc.,
Model CL–600–2C10 (Regional Jet Series 700,
701, & 702) airplanes, Model CL–600–2D15
(Regional Jet Series 705) airplanes, Model
CL–600–2D24 (Regional Jet Series 900)
airplanes, and Model CL–600–2E25 (Regional
Jet Series 1000) airplanes, certificated in any
category.
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Federal Register / Vol. 83, No. 110 / Thursday, June 7, 2018 / Rules and Regulations
(d) Subject
Air Transport Association (ATA) of
America Code 32, Landing gear.
(e) Reason
This AD was prompted by a report
indicating that Belleville washers installed
on the shimmy damper of the main landing
gear (MLG) may fail due to fatigue. We are
issuing this AD to prevent a failed washer
segment migrating into the piston cavity and
interfering with piston travel. As a result, the
shimmy damper performance could be
compromised, and an MLG shimmy could
occur, potentially leading to an MLG failure
and affecting the airplane’s safe flight and
landing.
(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 airplane maintenance or
inspection program, as applicable, by
incorporating maintenance review board
(MRB) report task number 320100–229,
Restoration (Belleville Washer Replacement)
of the MLG Shimmy Damper, of the MRB
Report of the Bombardier CRJ700/900/1000
Maintenance Requirements Manual (MRM)—
Part 1, Volume 1, CSP B–053, Revision 17,
dated June 25, 2017. The initial compliance
time for MRB report task number 320100–229
is specified in paragraphs (g)(1) and (g)(2) of
this AD, as applicable.
(1) For any shimmy damper with 20,000
total accumulated flight cycles or fewer as of
the effective date of this AD, the initial
compliance time is before the accumulation
of 26,000 total flight cycles.
(2) For any shimmy damper with 20,000
total accumulated flight cycles or more as of
the effective date of this AD, the initial
compliance time is specified in paragraph
(g)(2)(i) or (g)(2)(ii), whichever occurs later.
(i) Within 6,000 flight cycles after the
effective date of this AD, but prior to the
accumulation of 30,000 total flight cycles.
(ii) Within 30 days after effective date of
this AD.
sradovich on DSK3GMQ082PROD with RULES
(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 Temporary
Revision MRB–0070, dated October 20, 2015.
(i) No Alternative Actions and/or Intervals
After the airplane maintenance or
inspection program has been revised, as
required by paragraph (g) of this AD, no
alternative actions (e.g., inspections) and/or
intervals may be used unless the actions and/
or intervals are approved as an alternative
method of compliance (AMOC) in
accordance with the procedures specified in
paragraph (j)(1) of this AD.
(j) Other FAA AD Provisions
The following provisions also apply to this
AD:
VerDate Sep<11>2014
15:41 Jun 06, 2018
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(1) Alternative Methods of Compliance
(AMOCs): The Manager, New York ACO
Branch, 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 manager of the certification office,
send it to ATTN: Program Manager,
Continuing Operational Safety, FAA, New
York ACO Branch, 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.
(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 Branch,
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.
ac.yul@aero.bombardier.com; internet https://
www.bombardier.com.
(4) You may view this service information
at the FAA, Transport Standards Branch,
2200 South 216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
(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.
(k) Related Information
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) Canadian
Airworthiness Directive CF–2017–14, dated
April 21, 2017, 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–
2017–1175.
(2) For more information about this AD,
contact Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Section,
FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590;
telephone 516–228–7318; fax 516–794–5531.
(3) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (l)(3) and (l)(4) of this AD.
Regulatory Program Fees and Water
Charges Rates
(l) 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) Maintenance review board (MRB) report
task number 320100–229, Restoration
(Belleville Washer Replacement) of the MLG
Shimmy Damper, of the MRB Report of the
Bombardier CRJ700/900/1000 Maintenance
Requirements Manual (MRM)—Part 1,
Volume 1, CSP B–053, Revision 17, dated
June 25, 2017.
(ii) Reserved.
(3) For service information identified in
ˆ
this AD, contact Bombardier, Inc., 400 Cote´
Vertu Road West, Dorval, Quebec H4S 1Y9,
Canada; Widebody Customer Response
Center North America toll-free telephone 1–
866–538–1247 or direct-dial telephone 1–
514–855–2999; fax 514–855–7401; email
PO 00000
Frm 00008
Fmt 4700
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Issued in Des Moines, Washington, on May
21, 2018.
James Cashdollar,
Acting Director, System Oversight Division,
Aircraft Certification Service.
[FR Doc. 2018–11827 Filed 6–6–18; 8:45 am]
BILLING CODE 4910–13–P
DELAWARE RIVER BASIN
COMMISSION
18 CFR Parts 401 and 420
Delaware River Basin
Commission.
ACTION: Final rule.
AGENCY:
Notice is provided of the
Commission’s regulatory program fees
and schedule of water charges for the
fiscal year beginning July 1, 2018.
DATES: This final rule is effective July 1,
2018.
FOR FURTHER INFORMATION CONTACT: Elba
L. Deck, CPA, Director of
Administration and Finance, 609–883–
9500, ext. 201.
SUPPLEMENTARY INFORMATION: The
Delaware River Basin Commission
(‘‘DRBC’’ or ‘‘Commission’’) is a
Federal-interstate compact agency
charged with managing the water
resources of the Delaware River Basin
on a regional basis without regard to
political boundaries. Its members are
the governors of the four basin states—
Delaware, New Jersey, New York and
Pennsylvania—and on behalf of the
federal government, the North Atlantic
Division Commander of the U.S. Army
Corps of Engineers.
In accordance with 18 CFR 401.43(c),
on July 1 of every year beginning July
1, 2017, the Commission’s regulatory
program fees as set forth in Tables 1, 2
and 3 of that section are subject to an
annual adjustment, commensurate with
any increase in the annual April 12month Consumer Price Index (CPI) for
Philadelphia published by the U.S.
Bureau of Labor Statistics during that
SUMMARY:
E:\FR\FM\07JNR1.SGM
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Agencies
[Federal Register Volume 83, Number 110 (Thursday, June 7, 2018)]
[Rules and Regulations]
[Pages 26352-26354]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-11827]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2017-1175; Product Identifier 2017-NM-087-AD; Amendment
39-19300; AD 2018-11-12]
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 all
Bombardier, Inc., Model CL-600-2C10 (Regional Jet Series 700, 701, &
702) airplanes, Model CL-600-2D15 (Regional Jet Series 705) airplanes,
Model CL-600-2D24 (Regional Jet Series 900) airplanes, and Model CL-
600-2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by
a report that Belleville washers installed on the shimmy damper of the
main landing gear (MLG) may fail due to fatigue. This AD requires
revising the maintenance or inspection program, as applicable, to
incorporate a repetitive task specified in the maintenance review board
(MRB) report. We are issuing this AD to address the unsafe condition on
these products.
DATES: This AD is effective July 12, 2018.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 12,
2018.
ADDRESSES: For service information identified in this final rule,
contact Bombardier, Inc., 400 C[ocirc]te-Vertu Road West, Dorval,
Qu[eacute]bec H4S 1Y9, Canada; Widebody Customer Response Center North
America toll-free telephone 1-866-538-1247 or direct-dial telephone 1-
514-855-2999; fax 514-855-7401; email [email protected];
internet https://www.bombardier.com. You may view this referenced
service information at the FAA, Transport Standards Branch, 2200 South
216th St., Des Moines, WA. For information on the availability of this
material at the FAA, call 206-231-3195. It is also available on the
internet at https://www.regulations.gov by searching for and locating
Docket No. FAA-2017-1175.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1175; 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 Office (telephone
800-647-5527) is 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 20590.
FOR FURTHER INFORMATION CONTACT: Cesar Gomez, Aerospace Engineer,
Airframe and Mechanical Systems Section, FAA, New York ACO Branch, 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 all Bombardier, Inc., Model
CL-600-2C10 (Regional Jet Series 700, 701, & 702) airplanes, Model CL-
600-2D15 (Regional Jet Series 705) airplanes, Model CL-600-2D24
(Regional Jet Series 900) airplanes, and Model CL-600-2E25 (Regional
Jet Series 1000) airplanes. The NPRM published in the Federal Register
on January 2, 2018 (83 FR 83) (``the NPRM'').
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2017-14, dated April
21, 2017 (referred to after this as the Mandatory Continuing
Airworthiness Information, or ``the MCAI''), to correct an unsafe
condition for all Bombardier, Inc., Model CL-600-2C10 (Regional Jet
Series 700, 701, & 702) airplanes, Model CL-600-2D15 (Regional Jet
Series 705) airplanes, Model CL-600-2D24 (Regional Jet Series 900)
airplanes, and Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
The MCAI states:
It has been found that Belleville washers installed on the Main
Landing Gear (MLG) Shimmy Damper may fail in fatigue. A failed
washer segment migrating into the piston cavity may interfere with
piston travel. As a result, shimmy damper performance would be
compromised, MLG shimmy could occur and potentially lead to a MLG
failure.
As a result of this investigation, a restoration task has been
added for Belleville washers' replacement at 20,000 flight cycles,
during MLG overhaul. For aeroplanes that have passed the 20,000
flight cycle threshold, a phase-in period is defined.
This [Canadian] AD is issued to mandate the Maintenance Review
Board (MRB)
[[Page 26353]]
revised task for the affected aeroplanes models.
You may examine the MCAI in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2017-
1175.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comment received on the NPRM and
the FAA's response to that comment.
Request to the Contact Manufacturer for Service Information
Bombardier stated that task number 320100-229, Restoration
(Belleville Washer Replacement) of the MLG Shimmy Damper, of the MRB
Report of the Bombardier CRJ700/900/1000 Maintenance Requirements
Manual (MRM)--Part 1, Volume 1, CSP B-053, Revision 17, dated June 25,
2017, is currently specified in paragraph (g) of the proposed AD.
Bombardier commented that it is planning to issue Revision 18 of the
service information by June 25, 2018. Bombardier stated to contact
Bombardier for the latest service information should the AD be
published after June 25, 2018.
We expect to issue this AD prior to the anticipated date of release
of new service information, and we do not agree to delay issuance of
this AD until new service information is released. However, if new
service information is released after this AD is issued, operators may
request approval of an alternative method of compliance (AMOC) under
the provisions of paragraph (j)(1) of this AD. We have not changed this
AD regarding this issue.
Conclusion
We reviewed the relevant data, considered the comment received, 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 for correcting the unsafe condition; and
Do not add any additional burden upon the public than was
already proposed in the NPRM.
Related Service Information Under 1 CFR Part 51
Bombardier has issued MRB report task number 320100-229,
Restoration (Belleville Washer Replacement) of the MLG Shimmy Damper,
of the MRB Report of the Bombardier CRJ700/900/1000 Maintenance
Requirements Manual (MRM)--Part 1, Volume 1, CSP B-053, Revision 17,
dated June 25, 2017. This service information describes the restoration
(Belleville Washer Replacement) of the MLG shimmy damper. This service
information is reasonably available because the interested parties have
access to it through their normal course of business or by the means
identified in the ADDRESSES section.
Costs of Compliance
We estimate that this AD affects 544 airplanes of U.S. registry.
We estimate the following costs to comply with this AD:
We have determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although we
recognize that this number may vary from operator to operator. In the
past, we have estimated that this action takes 1 work-hour per
airplane. Since operators incorporate maintenance or inspection program
changes for their affected fleet(s), we have determined that a per-
operator estimate is more accurate than a per-airplane estimate.
Therefore, we estimate the total cost per operator to be $7,650 (90
work-hours x $85 per work-hour).
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.
This AD is issued in accordance with authority delegated by the
Executive Director, Aircraft Certification Service, as authorized by
FAA Order 8000.51C. In accordance with that order, issuance of ADs is
normally a function of the Compliance and Airworthiness Division, but
during this transition period, the Executive Director has delegated the
authority to issue ADs applicable to transport category airplanes to
the Director of the System Oversight Division.
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:
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.
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):
2018-11-12 Bombardier, Inc., Airplanes: Amendment 39-19300; Docket
No. FAA-2017-1175; Product Identifier 2017-NM-087-AD.
(a) Effective Date
This AD is effective July 12, 2018.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all Bombardier, Inc., Model CL-600-2C10
(Regional Jet Series 700, 701, & 702) airplanes, Model CL-600-2D15
(Regional Jet Series 705) airplanes, Model CL-600-2D24 (Regional Jet
Series 900) airplanes, and Model CL-600-2E25 (Regional Jet Series
1000) airplanes, certificated in any category.
[[Page 26354]]
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
gear.
(e) Reason
This AD was prompted by a report indicating that Belleville
washers installed on the shimmy damper of the main landing gear
(MLG) may fail due to fatigue. We are issuing this AD to prevent a
failed washer segment migrating into the piston cavity and
interfering with piston travel. As a result, the shimmy damper
performance could be compromised, and an MLG shimmy could occur,
potentially leading to an MLG failure and affecting the airplane's
safe flight and landing.
(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
airplane maintenance or inspection program, as applicable, by
incorporating maintenance review board (MRB) report task number
320100-229, Restoration (Belleville Washer Replacement) of the MLG
Shimmy Damper, of the MRB Report of the Bombardier CRJ700/900/1000
Maintenance Requirements Manual (MRM)--Part 1, Volume 1, CSP B-053,
Revision 17, dated June 25, 2017. The initial compliance time for
MRB report task number 320100-229 is specified in paragraphs (g)(1)
and (g)(2) of this AD, as applicable.
(1) For any shimmy damper with 20,000 total accumulated flight
cycles or fewer as of the effective date of this AD, the initial
compliance time is before the accumulation of 26,000 total flight
cycles.
(2) For any shimmy damper with 20,000 total accumulated flight
cycles or more as of the effective date of this AD, the initial
compliance time is specified in paragraph (g)(2)(i) or (g)(2)(ii),
whichever occurs later.
(i) Within 6,000 flight cycles after the effective date of this
AD, but prior to the accumulation of 30,000 total flight cycles.
(ii) Within 30 days after effective date of this AD.
(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 Temporary Revision MRB-0070, dated
October 20, 2015.
(i) No Alternative Actions and/or Intervals
After the airplane maintenance or inspection program has been
revised, as required by paragraph (g) of this AD, no alternative
actions (e.g., inspections) and/or intervals may be used unless the
actions and/or intervals are approved as an alternative method of
compliance (AMOC) in accordance with the procedures specified in
paragraph (j)(1) of this AD.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager, New
York ACO Branch, 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 manager of the certification
office, send it to ATTN: Program Manager, Continuing Operational
Safety, FAA, New York ACO Branch, 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.
(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
Branch, 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.
(k) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian Airworthiness Directive CF-2017-14, dated April 21,
2017, 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-2017-1175.
(2) For more information about this AD, contact Cesar Gomez,
Aerospace Engineer, Airframe and Mechanical Systems Section, FAA,
New York ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY
11590; telephone 516-228-7318; fax 516-794-5531.
(3) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (l)(3) and (l)(4) of this AD.
(l) 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) Maintenance review board (MRB) report task number 320100-
229, Restoration (Belleville Washer Replacement) of the MLG Shimmy
Damper, of the MRB Report of the Bombardier CRJ700/900/1000
Maintenance Requirements Manual (MRM)--Part 1, Volume 1, CSP B-053,
Revision 17, dated June 25, 2017.
(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; Widebody Customer Response Center
North America toll-free telephone 1-866-538-1247 or direct-dial
telephone 1-514-855-2999; fax 514-855-7401; email
[email protected]; internet https://www.bombardier.com.
(4) You may view this service information at the FAA, Transport
Standards Branch, 2200 South 216th St., Des Moines, WA. For
information on the availability of this material at the FAA, call
206-231-3195.
(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 Des Moines, Washington, on May 21, 2018.
James Cashdollar,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2018-11827 Filed 6-6-18; 8:45 am]
BILLING CODE 4910-13-P