Published 2019-07-03 · Federal Register document 2019-14153
Airworthiness Directives; Bombardier, Inc., Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for all 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 new and more restrictive airworthiness limitations are necessary for operational checks of the landing gear alternate extension system (AES). This AD requires revising the existing maintenance or inspection program, as applicable, to incorporate new and more restrictive airworthiness limitations. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:01.312311+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2019-66422190cf4fa9dc
- Source row
- results[135]
- Raw source SHA-256
- 66422190cf4fa9dc96bac02b1afe14648e349a1393bef6cf5fbf55644fa2ce43
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2019-12-03
- Effective date printed in this edition
- 2019-08-07
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This AD is effective August 7, 2019.
Exact source excerpt. Text positions 10436–10498, end exclusive, in the original decoded publication. SHA-256: ffe0f924244e242b06905d0c057beb360aeb908dc3318d38e89ba4d005145cc7
Affected ADs
(b) Affected ADs
None.
[[Page 31709]]
Exact source excerpt. Text positions 10498–10543, end exclusive, in the original decoded publication. SHA-256: d3d42aaf1e5ed7a5b89a4d84ea6c9e6a3f68ef51283b715066cbe483e8e16534
Applicability wording · Applicability
(c) Applicability
This AD applies to all Bombardier, Inc., Model CL-600-2C10
(Regional Jet Series 700, 701 & 702), CL-600-2D15 (Regional Jet
Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes,
certificated in any category.
Exact source excerpt. Text positions 10543–10789, end exclusive, in the original decoded publication. SHA-256: 0285ee7f6cf13977ba583a4d2eee984ff31c3b17ea2c5a2f5d74bc2ed5d1dd35
Subject
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
gear.
Exact source excerpt. Text positions 10789–10874, end exclusive, in the original decoded publication. SHA-256: 69274928c56ed19d35a0daa54cffa9711e118fc8445a016c40a1122f318391b3
Reason
(e) Reason
This AD was prompted by a determination that new and more
restrictive airworthiness limitations are necessary for operational
checks of the landing gear alternate extension system (AES). The FAA
is issuing this AD to address a deficiency in the existing
maintenance or inspection program, as applicable, that does not meet
the certification criteria for all critical AES failure modes, which
could reduce the ability of the flightcrew to maintain the safe
flight and landing of the airplane.
Exact source excerpt. Text positions 10874–11390, end exclusive, in the original decoded publication. SHA-256: a063a01a913eb33426397abab5947fd5d48a32e90d4fced4f11534e3d4d7c739
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11390–11492, 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
existing maintenance or inspection program, as applicable, to
incorporate the information specified in CRJ Regional Jet
(Bombardier) Temporary Revision ALI-0652, dated July 9, 2018. The
initial compliance time for doing the tasks is at the time specified
in figure 1 to paragraph (g) of this AD.
[GRAPHIC] [TIFF OMITTED] TR03JY19.000
Exact source excerpt. Text positions 11492–11947, end exclusive, in the original decoded publication. SHA-256: 6029f5225903fc096b6bfd473575224708a295ebd9df36f46bce7074ff22de96
No Alternative Actions or Intervals
(h) No Alternative Actions or Intervals
After the existing maintenance or inspection program has been
revised as 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.
Exact source excerpt. Text positions 11947–12344, end exclusive, in the original decoded publication. SHA-256: 9099b302e5358815e96e9653812c291fa64523319809692b61beee4f829f3e1f
Other FAA AD Provisions
(i) 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.
Exact source excerpt. Text positions 12344–13646, end exclusive, in the original decoded publication. SHA-256: 9293c0607d4899afb2c85ba4cee46ae9328b4dfb252ad57a8487dac35b2b86a5
Related Information
(j) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian AD CF-2018-31, dated November 28, 2018, for related
information. This MCAI may be found in the AD docket on the internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2019-0185.
(2) For more information about this AD, contact Darren Gassetto,
Aerospace Engineer, Mechanical Systems and Administrative Services
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; email
[email protected].
Exact source excerpt. Text positions 13646–14257, end exclusive, in the original decoded publication. SHA-256: 3bd506cb503ee1a92651ff01e4d95979c4008a6883759cf0c889aec6afa8baf2
Material Incorporated by Reference
(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) CRJ Regional Jet (Bombardier) Temporary Revision ALI-0652,
dated July 9, 2018.
(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 http://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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 14257–15598, end exclusive, in the original decoded publication. SHA-256: e7f24daa4ef89d285df1247238a26ef3b6062c064e73ce9df9688014a9237f07
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 2019-12-03 · 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.
Why these observations are shown
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: 101daed5af2a64b223be3a6a238270b25708aaabc5ff3f88e02aa0e0c956173f. Source manifest: f2746fcdc849939170fc6a7a49d5859ed26cf20000e01897cf6a8ba200b67f49.
Official source · 2019-07-03
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 84, Number 128 (Wednesday, July 3, 2019)]
[Rules and Regulations]
[Pages 31707-31709]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-14153]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-0185; Product Identifier 2018-NM-178-AD; Amendment
39-19658; AD 2019-12-03]
RIN 2120-AA64
Airworthiness Directives; Bombardier, Inc., Airplanes
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
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
new and more restrictive airworthiness limitations are necessary for
operational checks of the landing gear alternate extension system
(AES). This AD requires revising the existing maintenance or inspection
program, as applicable, to incorporate new and more restrictive
airworthiness limitations. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective August 7, 2019.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of August 7,
2019.
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 http://www.bombardier.com. 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. It is also available on the
internet at http://www.regulations.gov by searching for and locating
Docket No. FAA-2019-0185.
Examining the AD Docket
You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0185; or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this final rule, the regulatory evaluation, any comments received, and
other information. The address for Docket Operations is 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: Darren Gassetto, Aerospace Engineer,
Mechanical Systems and Administrative Services Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7323; fax 516-794-5531; email [email protected].
SUPPLEMENTARY INFORMATION:
Discussion
The FAA 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), CL-600-2D15
(Regional Jet Series 705), and CL-600-2D24 (Regional Jet Series 900)
airplanes. The NPRM published in the Federal Register on March 28, 2019
(84 FR 11656). The NPRM was prompted by a determination that new and
more restrictive airworthiness limitations are
[[Page 31708]]
necessary for operational checks of the landing gear AES. The NPRM
proposed to require revising the existing maintenance or inspection
program, as applicable, to incorporate new and more restrictive
airworthiness limitations.
The FAA is issuing this AD to address a deficiency in the existing
maintenance or inspection program, as applicable, that does not meet
the certification criteria for all critical AES failure modes, which
could reduce the ability of the flightcrew to maintain the safe flight
and landing of the airplane.
Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued Canadian AD CF-2018-31, dated November
28, 2018 (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), CL-600-2D15 (Regional Jet Series 705), and CL-
600-2D24 (Regional Jet Series 900) airplanes. The MCAI states:
During the Bombardier Maintenance Review Board (MRB) inspection
escalation interval project, it was discovered that the current
interval of 8000 hours air time and previous interval of 6000 hours
air time for the MRB Task 320100-203 ``Operational Check of the
Landing Gear Alternate Extension System (AES)'' does not meet the
certification criteria to cover for all critical AES failure modes
[which could reduce the ability of the flightcrew to maintain the
safe flight and landing of the airplane]. For this reason, a new
Certification Maintenance Requirement (CMR) task needs to be
implemented in the maintenance program at a shorter interval of 1600
hours air time.
This [Canadian] AD mandates a new CMR task for an operational
check of the AES with interval of 1600 hours air time.
You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0185.
Comments
The FAA gave the public the opportunity to participate in
developing this final rule. The FAA has considered the comment
received. The Air Line Pilots Association, International (ALPA)
indicated its support for the NPRM.
Conclusion
The FAA reviewed the relevant data, considered the comment
received, and determined that air safety and the public interest
require adopting this final rule as proposed, except for minor
editorial changes. The FAA has determined that these minor changes:
<bullet> Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
<bullet> 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 CRJ Regional Jet (Bombardier) Temporary
Revision ALI-0652, dated July 9, 2018. This service information
describes airworthiness limitations for a CMR task related to
operational checks of the landing gear AES.
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
The FAA estimates that this AD affects 536 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
The FAA has determined that revising the existing maintenance or
inspection program takes an average of 90 work-hours per operator,
although the FAA recognizes that this number may vary from operator to
operator. In the past, the FAA has estimated that this action takes 1
work-hour per airplane. Since operators incorporate maintenance or
inspection program changes for their affected fleet(s), the FAA has
determined that a per-operator estimate is more accurate than a per-
airplane estimate. Therefore, the FAA estimates 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.
The FAA is 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 and
associated appliances to the Director of the System Oversight Division.
Regulatory Findings
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) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
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):
2019-12-03 Bombardier, Inc.: Amendment 39-19658; Docket No. FAA-
2019-0185; Product Identifier 2018-NM-178-AD.
(a) Effective Date
This AD is effective August 7, 2019.
(b) Affected ADs
None.
[[Page 31709]]
(c) Applicability
This AD applies to all Bombardier, Inc., Model CL-600-2C10
(Regional Jet Series 700, 701 & 702), CL-600-2D15 (Regional Jet
Series 705), and CL-600-2D24 (Regional Jet Series 900) airplanes,
certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
gear.
(e) Reason
This AD was prompted by a determination that new and more
restrictive airworthiness limitations are necessary for operational
checks of the landing gear alternate extension system (AES). The FAA
is issuing this AD to address a deficiency in the existing
maintenance or inspection program, as applicable, that does not meet
the certification criteria for all critical AES failure modes, which
could reduce the ability of the flightcrew to maintain the safe
flight and landing of the airplane.
(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
existing maintenance or inspection program, as applicable, to
incorporate the information specified in CRJ Regional Jet
(Bombardier) Temporary Revision ALI-0652, dated July 9, 2018. The
initial compliance time for doing the tasks is at the time specified
in figure 1 to paragraph (g) of this AD.
[GRAPHIC] [TIFF OMITTED] TR03JY19.000
(h) No Alternative Actions or Intervals
After the existing maintenance or inspection program has been
revised as 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 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.
(j) Related Information
(1) Refer to Mandatory Continuing Airworthiness Information
(MCAI) Canadian AD CF-2018-31, dated November 28, 2018, for related
information. This MCAI may be found in the AD docket on the internet
at http://www.regulations.gov by searching for and locating Docket
No. FAA-2019-0185.
(2) For more information about this AD, contact Darren Gassetto,
Aerospace Engineer, Mechanical Systems and Administrative Services
Section, FAA, New York ACO Branch, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 516-228-7323; fax 516-794-5531; email
[email protected].
(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) CRJ Regional Jet (Bombardier) Temporary Revision ALI-0652,
dated July 9, 2018.
(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 http://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: http://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued in Des Moines, Washington, on June 12, 2019.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification
Service.
[FR Doc. 2019-14153 Filed 7-2-19; 8:45 am]
BILLING CODE 4910-13-P
Why this text is shown
The complete text was extracted from the official GovInfo HTML edition for this publication. Acquired 2026-10-09T02:07:25.552713+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- efa094fbfd7a84db47bb6cc99fe7a5d34ce332aa844e9fe70e8410993e621abe
- Text SHA-256
- 101daed5af2a64b223be3a6a238270b25708aaabc5ff3f88e02aa0e0c956173f
Return to the full metadata catalog · Search complete publication text · Explore retained publication text and evidence
Coverage and limits
These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
The collection uses 33 explicit annual source snapshots. Source captures and operative-text qualifications have separate states. Missing information remains unknown.