Published 2022-09-06 · Federal Register document 2022-19117
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate Previously Held by Bombardier, Inc.) Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain MHI RJ Aviation ULC Model CL-600-2D24 (Regional Jet Series 900) airplanes. This AD was prompted by a report of a manufacturing error that can create dents on the lower wing plank, close to the flap arm locations at certain wing stations; as a result, cracks could develop and weaken the structural integrity of the wings before being detected by any existing required inspections. This AD requires an inspection for damage (including dents, cracks, discoloration, gouges, scratches, or other surface damage) of the lower wing plank in the flap arm areas at certain wing stations, and repair if necessary. 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 2026-09-03T22:24:11.345539+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2022-c0cc5a172b1306fa
- Source row
- results[281]
- Raw source SHA-256
- c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2022-18-17
- Effective date printed in this edition
- 2022-10-11
Read 12 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective October 11, 2022.
Exact source excerpt. Text positions 9389–9479, end exclusive, in the original decoded publication. SHA-256: da2788fff684f0f51050580f735014706fb37c02eef3ae838c2ff129ac4b6da5
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 9479–9508, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to MHI RJ Aviation ULC (type certificate
previously held by Bombardier, Inc.) Model CL-600-2D24 (Regional Jet
Series 900) airplanes, certificated in any category, having serial
number 15462 through 15475 inclusive.
Exact source excerpt. Text positions 9508–9766, end exclusive, in the original decoded publication. SHA-256: f93a8e6a50a74b7026933355591c08f5a7b160e6f6718412709c4a4bb98725d3
Subject
(d) Subject
Air Transport Association (ATA) of America Code 57, Wings.
Exact source excerpt. Text positions 9766–9843, end exclusive, in the original decoded publication. SHA-256: 52f35cb894eac2144f3b0de7a455ce53cfbcfebe8c2ccd3b1ccbff2308cfe7df
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a report of a manufacturing error that
can create dents on the lower wing plank, close to the flap arm
locations at certain wing stations; as a result, cracks could
develop and weaken the structural integrity of the wings before
being detected by any existing required inspections. The FAA is
issuing this AD to address dents, cracks, and other damage, that, if
not detected and corrected, could lead to reduced structural
integrity of the wings.
Exact source excerpt. Text positions 9843–10348, end exclusive, in the original decoded publication. SHA-256: 32b45c023f6855e6e24fbbf907ce59714fcafd2521d9233821bf7186076f7b02
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 10348–10450, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Inspection and Corrective Action
(g) Inspection and Corrective Action
Prior to the accumulation of 8,800 total flight hours or within
30 days after the effective date of this AD, whichever occurs later,
perform a detailed visual inspection for damage (including dents,
cracks, discoloration, gouges, scratches, or other surface damage)
of the outer aft lower skin at wing stations (WS) 54.55, WS 128.00,
WS 179.00, WS 220.00, and WS 264.00 in accordance with paragraph B.,
``Procedure,'' of the Accomplishment Instructions of MHI RJ Aviation
Service Bulletin 670BA-57-029, dated February 2, 2021. Do all
applicable corrective actions before further flight. If any damage
is found during the inspection, before further flight, repair using
a method approved by the Manager, New York ACO Branch, FAA; or
Transport Canada Civil Aviation (TCCA); or MHI RJ Aviation ULC's
TCCA Design Approval Organization (DAO). If approved by the DAO, the
approval must include the DAO-authorized signature.
Exact source excerpt. Text positions 10450–11424, end exclusive, in the original decoded publication. SHA-256: 349fa6129672a1dbcb8a7ac762109731f236a79ecbef79544efc4f029b355eae
No Reporting Requirement
(h) No Reporting Requirement
Although MHI RJ Aviation Service Bulletin 670BA-57-029, dated
February 2, 2021, specifies to submit certain information to the
manufacturer, this AD does not include that requirement.
Exact source excerpt. Text positions 11424–11645, end exclusive, in the original decoded publication. SHA-256: 6fd89137a62836da1a32e6b49f7528191d89919770ddedf29889ce7ec01518e1
Special Flight Permit
(i) Special Flight Permit
Special flight permits may be issued in accordance with 14 CFR
21.197 and 21.199 to operate the airplane to a location where the
inspection can be done, provided the flight is a non-revenue flight.
Exact source excerpt. Text positions 11645–11877, end exclusive, in the original decoded publication. SHA-256: 8fd7c62bdedcca1e6b332f4b864b74c412020ce62ba31d7d755d1b36423327a5
Other FAA Provisions
(j) Other FAA 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 responsible Flight Standards 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. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the responsible Flight
Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or TCCA; or MHI RJ Aviation ULC's TCCA DAO. If approved
by the DAO, the approval must include the DAO-authorized signature.
Exact source excerpt. Text positions 11877–13051, end exclusive, in the original decoded publication. SHA-256: 5d2fbcdbd97b2771b350ad66e6924589c69d662faa69f29533c2480312c71ec0
Additional Information
(k) Additional Information
(1) Refer to TCCA AD CF-2021-31, dated September 14, 2021, for
related information. This TCCA AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2022-0592.
(2) For more information about this AD, contact Deep Gaurav,
Aerospace Engineer, Airframe and Propulsion Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone
[[Page 54355]]
516-228-7300; email [email protected].
Exact source excerpt. Text positions 13051–13529, end exclusive, in the original decoded publication. SHA-256: be47c3380391455df089e77768222e9ba1891c1fa80829f981271ec8f678b05f
Material Incorporated by Reference
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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) MHI RJ Aviation Service Bulletin 670BA-57-029, dated
February 2, 2021.
(ii) [Reserved]
(3) For service information identified in this AD, contact MHI
RJ Aviation Group, Customer Response Center, 3655 Ave. des Grandes-
Tourelles, Suite 110, Boisbriand, Qu[eacute]bec J7H 0E2 Canada;
North America toll-free telephone 833-990-7272 or direct-dial
telephone 450-990-7272; fax 514-855-8501; email mhirj.com">thd.crj@mhirj.com;
website mhirj.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety 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, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 13529–14888, end exclusive, in the original decoded publication. SHA-256: 8c716bb1c732dc43776938cafde0b8d58ead253a36797462afe218455daffbb7
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 2022-18-17 · 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: 651305061e7c1037c3fe89539a86fdcf4697ebe0667aaec0ec6634174470e590. Source manifest: e86d8de656b62a361dfab5f5616a46e5af1280475b9fbe7ad4bbb6c944892ff1.
Official source · 2022-09-06
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 87, Number 171 (Tuesday, September 6, 2022)]
[Rules and Regulations]
[Pages 54353-54355]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-19117]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0592; Project Identifier MCAI-2021-01023-T;
Amendment 39-22168; AD 2022-18-17]
RIN 2120-AA64
Airworthiness Directives; MHI RJ Aviation ULC (Type Certificate
Previously Held by 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
certain MHI RJ Aviation ULC Model CL-600-2D24 (Regional Jet Series 900)
airplanes. This AD was prompted by a report of a manufacturing error
that can create dents on the lower wing plank, close to the flap arm
locations at certain wing stations; as a result, cracks could develop
and weaken the structural integrity of the wings before being detected
by any existing required inspections. This AD requires an inspection
for damage (including dents, cracks, discoloration, gouges, scratches,
or other surface damage) of the lower wing plank in the flap arm areas
at certain wing stations, and repair if necessary. The FAA is issuing
this AD to address the unsafe condition on these products.
DATES: This AD is effective October 11, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 11,
2022.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-0592; 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 mandatory continuing airworthiness
information (MCAI), 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.
Material Incorporated by Reference:
<bullet> For service information identified in this final rule,
contact MHI RJ Aviation Group, Customer Response Center, 3655 Ave. des
Grandes-Tourelles, Suite 110, Boisbriand, Qu[eacute]bec J7H 0E2 Canada;
North America toll-free telephone 833-990-7272 or direct-dial telephone
450-990-7272; fax 514-855-8501; email mhirj.com">thd.crj@mhirj.com; website
mhirj.com.
<bullet> You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety 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 at
regulations.gov under Docket No. FAA-2022-0592.
FOR FURTHER INFORMATION CONTACT: Deep Gaurav, Aerospace Engineer,
Airframe and Propulsion Section, FAA, New York ACO Branch, 1600 Stewart
Avenue, Suite 410, Westbury, NY 11590; telephone 516-228-7300; email [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain MHI RJ Aviation
ULC Model CL-600-2D24 (Regional Jet Series 900) airplanes. The NPRM
published in the Federal Register on June 2, 2022 (87 FR 33454). The
NPRM was prompted by AD CF-2021-31, dated September 14, 2021, issued by
Transport Canada Civil Aviation (TCCA), which is the aviation authority
for Canada (referred to after this as the MCAI). The MCAI states that a
manufacturing error may have resulted in dents on the lower wing plank,
close to the five flap arm locations at wing station (WS) 54.55, WS
128.00, WS 179.00, WS 220.00, and WS 264.00. These dents could lead to
cracks that could weaken the structural integrity of the wings before
being detected by any existing required inspection.
In the NPRM, the FAA proposed to require an inspection for damage
(including dents, cracks, discoloration, gouges, scratches, or other
surface damage) of the lower wing plank in the flap arm areas at
certain wing stations, and repair if necessary. The FAA is issuing this
AD to address the unsafe condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-0592.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
referenced above. The FAA reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on this product.
Except for minor editorial changes, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.
Related Service Information Under 1 CFR Part 51
The FAA reviewed MHI RJ Aviation Service Bulletin 670BA-57-029,
dated February 2, 2021. This service information specifies procedures
for, among other actions, doing a detailed visual inspection for damage
(including dents, cracks, discoloration, gouges, scratches, or other
surface damage) of the outer aft lower skin at WS 54.55, WS 128.00, WS
179.00, WS 220.00, and WS 264.00, and repair. 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 14 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
[[Page 54354]]
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
2 work-hours x $85 per hour = $170........................... $0 $170 $2,380
----------------------------------------------------------------------------------------------------------------
The FAA has received no definitive data on which to base the cost
estimates for the on-condition actions specified in this AD.
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.
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.
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:
2022-18-17 MHI RJ Aviation ULC (Type Certificate Previously Held by
Bombardier, Inc.): Amendment 39-22168; Docket No. FAA-2022-0592;
Project Identifier MCAI-2021-01023-T.
(a) Effective Date
This airworthiness directive (AD) is effective October 11, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to MHI RJ Aviation ULC (type certificate
previously held by Bombardier, Inc.) Model CL-600-2D24 (Regional Jet
Series 900) airplanes, certificated in any category, having serial
number 15462 through 15475 inclusive.
(d) Subject
Air Transport Association (ATA) of America Code 57, Wings.
(e) Unsafe Condition
This AD was prompted by a report of a manufacturing error that
can create dents on the lower wing plank, close to the flap arm
locations at certain wing stations; as a result, cracks could
develop and weaken the structural integrity of the wings before
being detected by any existing required inspections. The FAA is
issuing this AD to address dents, cracks, and other damage, that, if
not detected and corrected, could lead to reduced structural
integrity of the wings.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Inspection and Corrective Action
Prior to the accumulation of 8,800 total flight hours or within
30 days after the effective date of this AD, whichever occurs later,
perform a detailed visual inspection for damage (including dents,
cracks, discoloration, gouges, scratches, or other surface damage)
of the outer aft lower skin at wing stations (WS) 54.55, WS 128.00,
WS 179.00, WS 220.00, and WS 264.00 in accordance with paragraph B.,
``Procedure,'' of the Accomplishment Instructions of MHI RJ Aviation
Service Bulletin 670BA-57-029, dated February 2, 2021. Do all
applicable corrective actions before further flight. If any damage
is found during the inspection, before further flight, repair using
a method approved by the Manager, New York ACO Branch, FAA; or
Transport Canada Civil Aviation (TCCA); or MHI RJ Aviation ULC's
TCCA Design Approval Organization (DAO). If approved by the DAO, the
approval must include the DAO-authorized signature.
(h) No Reporting Requirement
Although MHI RJ Aviation Service Bulletin 670BA-57-029, dated
February 2, 2021, specifies to submit certain information to the
manufacturer, this AD does not include that requirement.
(i) Special Flight Permit
Special flight permits may be issued in accordance with 14 CFR
21.197 and 21.199 to operate the airplane to a location where the
inspection can be done, provided the flight is a non-revenue flight.
(j) Other FAA 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 responsible Flight Standards 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. Before using any
approved AMOC, notify your appropriate principal inspector, or
lacking a principal inspector, the manager of the responsible Flight
Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, New York ACO
Branch, FAA; or TCCA; or MHI RJ Aviation ULC's TCCA DAO. If approved
by the DAO, the approval must include the DAO-authorized signature.
(k) Additional Information
(1) Refer to TCCA AD CF-2021-31, dated September 14, 2021, for
related information. This TCCA AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2022-0592.
(2) For more information about this AD, contact Deep Gaurav,
Aerospace Engineer, Airframe and Propulsion Section, FAA, New York
ACO Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone
[[Page 54355]]
516-228-7300; email [email protected].
(l) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference 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) MHI RJ Aviation Service Bulletin 670BA-57-029, dated
February 2, 2021.
(ii) [Reserved]
(3) For service information identified in this AD, contact MHI
RJ Aviation Group, Customer Response Center, 3655 Ave. des Grandes-
Tourelles, Suite 110, Boisbriand, Qu[eacute]bec J7H 0E2 Canada;
North America toll-free telephone 833-990-7272 or direct-dial
telephone 450-990-7272; fax 514-855-8501; email mhirj.com">thd.crj@mhirj.com;
website mhirj.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety 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, email [email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on August 29, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-19117 Filed 9-2-22; 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 2026-10-09T01:40:35.105135+00:00. Text extraction preserves the recorded source wording; it does not determine current requirements.
Open the captured official edition
- Source SHA-256
- 9bfd7259bd2050ac64537c57208d3dabcab84770005aeeb3a4d9ddf21a78a34e
- Text SHA-256
- 651305061e7c1037c3fe89539a86fdcf4697ebe0667aaec0ec6634174470e590
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.