Published 2015-10-06 · Federal Register document 2015-25219
Airworthiness Directives; Bombardier, Inc. Airplanes
Publication summary
We are adopting 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 AD was prompted by a determination that no instructions for continued airworthiness exist for the nose landing gear (NLG) alternate extension actuator of the NLG alternate release system. This AD requires revising the maintenance or inspection program, as applicable, to incorporate a new airworthiness limitation task for the NLG alternate extension actuator. We are issuing this AD to prevent failure of the NLG alternate release system and, if the normal NLG extension system also fails, failure of the NLG to extend, and consequent damage to the airplane and injury to occupants.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:23:48.517946+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2015-3bb842c840a7e6e6
- Source row
- results[232]
- Raw source SHA-256
- 3bb842c840a7e6e6e43779ca68008e1e63ad8287ad840c3a981d1f66a934b14b
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2015-20-07
- Effective date printed in this edition
- 2015-11-10
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This AD becomes effective November 10, 2015.
Exact source excerpt. Text positions 10825–10895, end exclusive, in the original decoded publication. SHA-256: 1d72a865674ed0e7b74f443c1522de52f92237134304bc51a6c9f6b07c6def66
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10895–10924, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to the airplanes identified in paragraphs (c)(1)
and (c)(2) of this AD, certificated in any category.
(1) Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700,
701, & 702) airplanes, serial number (S/N) 10002 and subsequent.
(2) Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series
705), and CL-600-2D24 (Regional Jet Series 900) airplanes, S/N 15001
and subsequent.
Exact source excerpt. Text positions 10924–11353, end exclusive, in the original decoded publication. SHA-256: 14b6696f2fc625ba308a51ef9815f1d6f54dfddf6a9df90f4165894617717731
Subject
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
Gear.
Exact source excerpt. Text positions 11353–11438, end exclusive, in the original decoded publication. SHA-256: 1bb4b1d40ca102fb1eac263459df33cf7c23552a0e37fa5eaf137b6491422a4a
Reason
(e) Reason
This AD was prompted by a determination that no instructions for
continued airworthiness exist for the nose landing gear (NLG)
alternate extension actuator of the NLG alternate release system. We
are issuing this AD to prevent failure of the NLG alternate release
system and, if the normal NLG extension system also fails, failure
of the NLG to extend, and consequent damage to the airplane and
injury to occupants.
Exact source excerpt. Text positions 11438–11877, end exclusive, in the original decoded publication. SHA-256: 924350ca6583f6b20b046b851e35d083fcd1e127f907c3cefb1bdefac7366ce2
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11877–11979, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Maintenance or Inspection Program Revision
(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 320100-225, Restoration of the NLG
Manual Release Actuator, of Subject 1-32, Landing Gear, of Section
1, Systems and Powerplant Program, Volume 1 of Part 1, Maintenance
Review Board Report, Revision 14, dated July 10, 2013, of the CRJ
700/900/1000 Maintenance Requirements Manual, CSP-B-053. The initial
compliance time for the task is specified in paragraph (h) of this
AD.
Exact source excerpt. Text positions 11979–12577, end exclusive, in the original decoded publication. SHA-256: 4eb576c278a8d0cf115321d31891bab44d07d439ef0ee8b357694bcacb3c7f2a
Initial Task Compliance Time
(h) Initial Task Compliance Time
Before the accumulation of 20,000 total flight cycles, or within
5,500 flight cycles after the effective date of this AD, whichever
occurs later: Perform the initial restoration specified in Task
320100-225, Restoration of the NLG Manual Release Actuator, of
Subject 1-32, Landing Gear, of Section 1, Systems and Powerplant
Program, Volume 1 of Part 1, Maintenance Review Board Report,
Revision 14, dated July 10, 2013, of the CRJ 700/900/1000
Maintenance Requirements Manual, CSP-B-053.
Exact source excerpt. Text positions 12577–13111, end exclusive, in the original decoded publication. SHA-256: 2d644b6d4137364700d9a0ecaec02a90f9f8ca79eebc7ef84f619675e50db212
No Alternative Actions and Intervals
(i) 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 (j)(1) of this AD.
Exact source excerpt. Text positions 13111–13468, end exclusive, in the original decoded publication. SHA-256: a2897235b7e06d63e3035ebce45fec895f359f3226b9ce550bcfded3e16e63ce
Other FAA AD Provisions
(j) 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.
Exact source excerpt. Text positions 13468–14862, end exclusive, in the original decoded publication. SHA-256: a957f6f5fafa3cbb2772e415ef27d363c659b7a690fd4dc2ac0e35aba1d1bd0f
Related Information
(k) Related Information
Refer to MCAI Canadian Airworthiness Directive CF-2013-24R1,
dated December 24, 2013, for related information. This MCAI may be
found in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-1046-0002.
Exact source excerpt. Text positions 14862–15130, end exclusive, in the original decoded publication. SHA-256: 3268ea1f9e63365e73e460c72f1b715bf876e40da2e9af8c351ee972a06a6af0
Material Incorporated by Reference
(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) Task 320100-225, Restoration of the NLG Manual Release
Actuator, of Subject 1-32, Landing Gear, of Section 1, Systems and
Powerplant Program, Volume 1 of Part 1, Maintenance Review Board
Report, Revision 14, dated July 10, 2013, of the CRJ 700/900/1000
Maintenance Requirements Manual, CSP-B-053.
(ii) Reserved.
(3) For service information identified in this AD, 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
[email protected]; Internet http://www.bombardier.com.
(4) You may view this service information at the FAA, Transport
Airplane Directorate,
[[Page 60284]]
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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 15130–16597, end exclusive, in the original decoded publication. SHA-256: b59ad3440a9047942e8f9ebbb340d526bf88c37c58974c5a6b50e1088b3c9514
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2015-20-07 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
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They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: a8eaaa0c2f32f994e204d6c953ae1662c7300f2e0e0fdf04b4e06a13bca2d5f7. Source manifest: 188730fc6fe8925ea89a3ca68c97b46e3b0016c39e8e5f3dc488d0879768fdb5.
Official source · 2015-10-06
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 80, Number 193 (Tuesday, October 6, 2015)]
[Rules and Regulations]
[Pages 60281-60284]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-25219]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2014-1046; Directorate Identifier 2014-NM-021-AD;
Amendment 39-18286; AD 2015-20-07]
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-600-2C10 (Regional Jet Series 700, 701, &
702), CL-600-2D15 (Regional Jet Series 705), and CL-600-2D24 (Regional
Jet Series 900) airplanes. This AD was prompted by a determination that
no instructions for continued airworthiness exist for the nose landing
gear (NLG) alternate extension actuator of the NLG alternate release
system. This AD requires revising the maintenance or inspection
program, as applicable, to incorporate a new airworthiness limitation
task for the NLG alternate extension actuator. We are issuing this AD
to prevent failure of the NLG alternate release system and, if the
normal NLG extension system also fails, failure of the NLG to extend,
and consequent damage to the airplane and injury to occupants.
DATES: This AD becomes effective November 10, 2015.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 10,
2015.
[[Page 60282]]
ADDRESSES: You may examine the AD docket on the Internet at http://www.regulations.gov/#!docketDetail;D=FAA-2014-1046 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
[email protected]; Internet http://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. It
is also available on the Internet at http://www.regulations.gov by
searching for and locating Docket No. FAA-2014-1046.
FOR FURTHER INFORMATION CONTACT: Luke Walker, Aerospace Engineer,
Airframe and Mechanical Systems Branch, ANE-171, FAA, New York Aircraft
Certification Office (ACO), 1600 Stewart Avenue, Suite 410, Westbury,
NY 11590; telephone 516-228-7363; 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-600-2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15
(Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900)
airplanes. The NPRM published in the Federal Register on January 23,
2015 (80 FR 3502).
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian Airworthiness Directive CF-
2013-24R1, dated December 24, 2013 (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-
2C10 (Regional Jet Series 700, 701, & 702), CL-600-2D15 (Regional Jet
Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes. The
MCAI states:
It was discovered that there are no instructions for continued
airworthiness for the Nose Landing Gear (NLG) alternate extension
actuator. Without an effective maintenance task to maintain the
aeroplane's inherent level of safety, there is a potential that a
dormant failure of the alternate release system of the NLG could
occur. Failure of the NLG alternate release system could prevent the
nose landing gear from extending in the case of a failure of the
normal NLG extension system.
This [Canadian] AD is to mandate the incorporation of a new
maintenance task to prevent failure of the NLG alternate release
system.
Revision 1 of this [Canadian] AD changes the phase-in time to be
based on the NLG manual release actuators instead of aeroplanes.
You may examine the MCAI in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-1046-0002.
Comments
We gave the public the opportunity to participate in developing
this AD. The following presents the comments received on the NPRM (80
FR 3502, January 23, 2015) and the FAA's response to each comment.
Support for the NPRM (80 FR 3502, January 23, 2015)
Airline Pilots Association (ALPA) International agreed with the
intent of the NPRM (80 FR 3502, January 23, 2015).
Request To Revise Compliance Time
Envoy Airlines and Mesa Airlines asked that we revise the
compliance time language in paragraph (h) of the proposed AD (80 FR
3502, January 23, 2015) from ``whichever occurs first'' to ``whichever
occurs later.'' The compliance time, as written, could result in
airplanes being grounded. Envoy Airlines added that the compliance time
referred to in the TCCA AD is ``whichever occurs later.'' Mesa Airlines
noted that changing the compliance time would also allow for scheduling
and parts procurement.
We agree with the commenters' request for the reasons provided, and
due to the fact that this was an inadvertent error. We have revised the
compliance time in paragraph (h) of this AD as requested.
Conclusion
We reviewed the relevant data, considered the comments received,
and determined that air safety and the public interest require adopting
this AD with the change described previously and minor editorial
changes. We have determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM (80 FR 3502, January 23, 2015) for correcting the unsafe
condition; and
<bullet> Do not add any additional burden upon the public than was
already proposed in the NPRM (80 FR 3502, January 23, 2015).
We also determined that these changes will not increase the
economic burden on any operator or increase the scope of this AD.
Related Service Information Under 1 CFR Part 51
Bombardier, Inc. has issued Task 320100-225, Restoration of the NLG
Manual Release Actuator, of Subject 1-32, Landing Gear, of Section 1,
Systems and Powerplant Program, Volume 1 of Part 1, Maintenance Review
Board Report, Revision 14, dated July 10, 2013, of the CRJ 700/900/1000
Maintenance Requirements Manual, CSP-B-053. This service information
describes an airworthiness limitation task for the NLG alternate
extension actuator. 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
of this AD.
Costs of Compliance
We estimate that this AD affects 416 airplanes of U.S. registry.
We also estimate that it takes 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.
In addition, we estimate that any necessary follow-on actions take
about 1 work-hour and require parts costing $0, for a cost of $85 per
product. We have no way of determining the number of aircraft that
might need these actions.
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
[[Page 60283]]
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:
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 http://www.regulations.gov/#!docketDetail;D=FAA-2014-1046; 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):
2015-20-07 Bombardier, Inc.: Amendment 39-18286. Docket No. FAA-
2014-1046; Directorate Identifier 2014-NM-021-AD.
(a) Effective Date
This AD becomes effective November 10, 2015.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the airplanes identified in paragraphs (c)(1)
and (c)(2) of this AD, certificated in any category.
(1) Bombardier, Inc. Model CL-600-2C10 (Regional Jet Series 700,
701, & 702) airplanes, serial number (S/N) 10002 and subsequent.
(2) Bombardier, Inc. Model CL-600-2D15 (Regional Jet Series
705), and CL-600-2D24 (Regional Jet Series 900) airplanes, S/N 15001
and subsequent.
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
Gear.
(e) Reason
This AD was prompted by a determination that no instructions for
continued airworthiness exist for the nose landing gear (NLG)
alternate extension actuator of the NLG alternate release system. We
are issuing this AD to prevent failure of the NLG alternate release
system and, if the normal NLG extension system also fails, failure
of the NLG to extend, and consequent damage to the airplane and
injury to occupants.
(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 320100-225, Restoration of the NLG
Manual Release Actuator, of Subject 1-32, Landing Gear, of Section
1, Systems and Powerplant Program, Volume 1 of Part 1, Maintenance
Review Board Report, Revision 14, dated July 10, 2013, of the CRJ
700/900/1000 Maintenance Requirements Manual, CSP-B-053. The initial
compliance time for the task is specified in paragraph (h) of this
AD.
(h) Initial Task Compliance Time
Before the accumulation of 20,000 total flight cycles, or within
5,500 flight cycles after the effective date of this AD, whichever
occurs later: Perform the initial restoration specified in Task
320100-225, Restoration of the NLG Manual Release Actuator, of
Subject 1-32, Landing Gear, of Section 1, Systems and Powerplant
Program, Volume 1 of Part 1, Maintenance Review Board Report,
Revision 14, dated July 10, 2013, of the CRJ 700/900/1000
Maintenance Requirements Manual, CSP-B-053.
(i) 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 (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 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.
(k) Related Information
Refer to MCAI Canadian Airworthiness Directive CF-2013-24R1,
dated December 24, 2013, for related information. This MCAI may be
found in the AD docket on the Internet at http://www.regulations.gov/#!documentDetail;D=FAA-2014-1046-0002.
(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) Task 320100-225, Restoration of the NLG Manual Release
Actuator, of Subject 1-32, Landing Gear, of Section 1, Systems and
Powerplant Program, Volume 1 of Part 1, Maintenance Review Board
Report, Revision 14, dated July 10, 2013, of the CRJ 700/900/1000
Maintenance Requirements Manual, CSP-B-053.
(ii) Reserved.
(3) For service information identified in this AD, 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
[email protected]; Internet http://www.bombardier.com.
(4) You may view this service information at the FAA, Transport
Airplane Directorate,
[[Page 60284]]
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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Renton, Washington, on September 27, 2015.
Michael Kaszycki,
Acting Manager, Transport Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2015-25219 Filed 10-5-15; 8:45 am]
BILLING CODE 4910-13-P
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