Published 2022-11-16 · Federal Register document 2022-24902
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 all MHI RJ Aviation ULC Model CL-600-2C10 (Regional Jet Series 700, 701 & 702); CL-600-2C11 (Regional Jet Series 550); CL-600-2D15 (Regional Jet Series 705); CL-600-2D24 (Regional Jet Series 900); and CL-600-2E25 (Regional Jet Series 1000) airplanes. This AD was prompted by reports that the landing gear age of certain airplanes was higher than expected for gear overhaul, which could increase the risk of corrosion. This AD requires verifying the calendar age of the nose landing gear (NLG) and main landing gear (MLG) by way of component maintenance documents, and performing corrective actions if necessary. This AD also prohibits installing certain components. 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[351]
- Raw source SHA-256
- c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2022-21-10
- Effective date printed in this edition
- 2022-12-21
Read 13 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective December 21,
2022.
Exact source excerpt. Text positions 10036–10128, end exclusive, in the original decoded publication. SHA-256: a7ca0fbf06983e789e2ad00f377ad2a038f4c9d2e0ee4b33a45e2dd11ad8652d
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 10128–10157, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to all MHI RJ Aviation ULC airplanes identified
in paragraphs (c)(1) through (5) of this AD, certificated in any
category.
(1) Model CL-600-2C10 (Regional Jet Series 700, 701, & 702).
(2) Model CL-600-2C11 (Regional Jet Series 550).
(3) Model CL-600-2D15 (Regional Jet Series 705).
(4) Model CL-600-2D24 (Regional Jet Series 900).
(5) Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
Exact source excerpt. Text positions 10157–10610, end exclusive, in the original decoded publication. SHA-256: 430e2cca70494a38ec48200bdaad5fbe2148cf6683ddf940fc4584d794fb1bac
Subject
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
gear.
Exact source excerpt. Text positions 10610–10695, end exclusive, in the original decoded publication. SHA-256: 69274928c56ed19d35a0daa54cffa9711e118fc8445a016c40a1122f318391b3
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by reports that the landing gear age of
certain airplanes was higher than expected for gear overhaul. The
FAA is issuing this AD to address the possibility of undetected
corrosion due to landing gear age that could lead to main landing
gear (MLG) and/or nose landing gear (NLG) collapse, and consequent
damage to the airplane and injury to the occupants.
Exact source excerpt. Text positions 10695–11103, end exclusive, in the original decoded publication. SHA-256: 75ec13d838cdb5328c89b2ba24dbce532de210fafbfbf203576de1a6efe1b6a6
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 11103–11205, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Determination of Component Calendar Age
(g) Determination of Component Calendar Age
Within 90 days after the effective date of this AD: Verify the
airplane and/or the airplane technical records to determine whether
any MLG and NLG components are affected components based on their
calendar age, in accordance with Section 2, Part A, of the
Accomplishment Instructions of MHI RJ Service Bulletin (SB) 670BA-
32-062, Revision A, dated December 2, 2021.
Exact source excerpt. Text positions 11205–11626, end exclusive, in the original decoded publication. SHA-256: 661b8fc5f7f9fb7b2ca8d9bcef3d12025e4292620d735711dc44e6c55ca344a0
Removal and Replacement of Affected NLG Components
(h) Removal and Replacement of Affected NLG Components
(1) Within the applicable compliance time indicated in figure 1
to paragraph (h) of this AD: Remove the affected NLG components
identified in paragraph (g) of this AD in accordance with Section 2,
Part B, of the Accomplishment Instructions of MHI RJ SB 670BA-32-
062, Revision A, dated December 2, 2021.
(2) Before further flight after removal of the affected
components, replace the removed components with serviceable
components, in accordance with Section 2, Part D, of the
Accomplishment Instructions of MHI RJ SB 670BA-32-062, Revision A,
dated December 2, 2021.
[[Page 68613]]
[GRAPHIC] [TIFF OMITTED] TR16NO22.004
Exact source excerpt. Text positions 11626–12321, end exclusive, in the original decoded publication. SHA-256: 5d59b558c5cc9ffe5d6920b0c786c648967cad2d8b651c8b747d77336777eba5
Removal and Replacement of Affected MLG Components
(i) Removal and Replacement of Affected MLG Components
(1) Within the applicable compliance time indicated in figure 1
to paragraph (h) of this AD: Remove the affected MLG components
identified in paragraph (g) of this AD in accordance with Section 2,
Part E or H, as applicable, of the Accomplishment Instructions of
MHI RJ SB 670BA-32-062, Revision A, dated December 2, 2021.
(2) Before further flight after removing the affected
components, replace the removed components with serviceable
components, in accordance with Section 2, Part G or J, as
applicable, of the Accomplishment Instructions of MHI RJ SB 670BA-
32-062, Revision A, dated December 2, 2021.
Exact source excerpt. Text positions 12321–12999, end exclusive, in the original decoded publication. SHA-256: 54b5fd4f95217b640df3c7e9bed5468e28614a9475badd6416e28927b6fca224
Parts Installation Limitation
(j) Parts Installation Limitation
(1) As of the effective date of this AD, no person may install,
on any airplane, any MLG or NLG component with a calendar age of 12
years or more unless it has been overhauled in accordance with
Section 2, Part C, F, or I, as applicable, of the Accomplishment
Instructions of MHI RJ SB 670BA-32-062, Revision A, dated December
2, 2021.
(2) As of the effective date of this AD, any MLG or NLG
component with a calendar age of less than 12 years may be installed
on any airplane, provided it is overhauled in accordance with
Section 2 Part C, F, or I, as applicable, of the Accomplishment
Instructions of MHI RJ SB 670BA-32-062, Revision A, dated December
2, 2021, prior to reaching 12 years' component calendar age.
Exact source excerpt. Text positions 12999–13768, end exclusive, in the original decoded publication. SHA-256: a56e5b2cff375cd44e3461ef48da20b956a1af3f2db323d42bc12b57ff617b43
Other FAA AD Provisions
(k) 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 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 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 13768–15011, end exclusive, in the original decoded publication. SHA-256: c8eda2707e54fb311dae0e7dc274f290f050282481d437396518ef1d3ccd1bc9
Additional Information
(l) Additional Information
(1) Refer to TCCA AD CF-2021-49, dated December 20, 2021, for
related information. This TCCA AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2022-0885.
(2) For more information about this AD, contact Jiwan
Karunatilake, 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].
Exact source excerpt. Text positions 15011–15478, end exclusive, in the original decoded publication. SHA-256: a05fae1953b1fa7eb819456daa93aa7114ff413ef7b47b2c36222ebdcbe855df
Material Incorporated by Reference
(m) 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 Service Bulletin 670BA-32-062, Revision A, dated
December 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 15478–16840, end exclusive, in the original decoded publication. SHA-256: 1227ed4ca7bb0c1ab58bea3310bf8efc7d24fc6282619200c9fc1d1b1598726e
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 2022-21-10 · 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: 034cee212172551f0d97e1e5b9799897956957e1479f7fe1e4b4431381990ff2. Source manifest: 3149714fa8e2d3b1703b8065fc5dd0c46752cf9a1c40ec0392fdf3ba4b4f8d02.
Official source · 2022-11-16
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 220 (Wednesday, November 16, 2022)]
[Rules and Regulations]
[Pages 68610-68613]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-24902]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0885; Project Identifier MCAI-2021-01429-T;
Amendment 39-22209; AD 2022-21-10]
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 all
MHI RJ Aviation ULC Model CL-600-2C10 (Regional Jet Series 700, 701 &
702); CL-600-2C11 (Regional Jet Series 550); CL-600-2D15 (Regional Jet
Series 705); CL-600-2D24 (Regional Jet Series 900); and CL-600-2E25
(Regional Jet Series 1000) airplanes. This AD was prompted by reports
that the landing gear age of certain airplanes was higher than expected
for gear overhaul, which could increase the risk of corrosion. This AD
requires verifying the calendar age of the nose landing gear (NLG) and
main
[[Page 68611]]
landing gear (MLG) by way of component maintenance documents, and
performing corrective actions if necessary. This AD also prohibits
installing certain components. The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective December 21, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of December 21,
2022.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-0885; 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-2022-0885.
FOR FURTHER INFORMATION CONTACT: Jiwan Karunatilake, 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 all MHI RJ Aviation ULC
Model CL-600-2C10 (Regional Jet Series 700, 701 & 702); CL-600-2C11
(Regional Jet Series 550); CL-600-2D15 (Regional Jet Series 705); CL-
600-2D24 (Regional Jet Series 900); and CL-600-2E25 (Regional Jet
Series 1000) airplanes. The NPRM published in the Federal Register on
July 21, 2022 (87 FR 43450). The NPRM was prompted by AD CF-2021-49,
dated December 20, 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 the landing gear age of certain
airplanes was higher than expected for gear overhaul. The MCAI notes
that undetected corrosion could lead to MLG and/or NLG collapse, and
consequent damage to the airplane and injury to the occupants.
In the NPRM, the FAA proposed to require verifying the calendar age
of the NLG and MLG by way of component maintenance documents, and
performing corrective actions if necessary. The NPRM also proposed to
prohibit installing certain components. 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-2022-0885.
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
MHI RJ has issued Service Bulletin 670BA-32-062, dated December 2,
2021. This service information describes procedures for, among other
actions, verifying the calendar age of the NLG and MLG by way of
component maintenance documents and for removing affected landing gear
components and replacing them with serviceable components. 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 624 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
4 work-hours x $85 per hour = $340........................... $0 $340 $212,160
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary on-
condition actions that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need these on-condition actions:
Estimated Costs of On-Condition Actions
------------------------------------------------------------------------
Labor cost Parts cost Cost per product
------------------------------------------------------------------------
Up to 32 work-hours x $85 per Up to $340,000.... Up to $342,720.
hour = Up to $2,720.
------------------------------------------------------------------------
[[Page 68612]]
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:
2022-21-10 MHI RJ Aviation ULC (Type Certificate Previously Held by
Bombardier, Inc.): Amendment 39-22209; Docket No. FAA-2022-0885;
Project Identifier MCAI-2021-01429-T.
(a) Effective Date
This airworthiness directive (AD) is effective December 21,
2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all MHI RJ Aviation ULC airplanes identified
in paragraphs (c)(1) through (5) of this AD, certificated in any
category.
(1) Model CL-600-2C10 (Regional Jet Series 700, 701, & 702).
(2) Model CL-600-2C11 (Regional Jet Series 550).
(3) Model CL-600-2D15 (Regional Jet Series 705).
(4) Model CL-600-2D24 (Regional Jet Series 900).
(5) Model CL-600-2E25 (Regional Jet Series 1000) airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
gear.
(e) Unsafe Condition
This AD was prompted by reports that the landing gear age of
certain airplanes was higher than expected for gear overhaul. The
FAA is issuing this AD to address the possibility of undetected
corrosion due to landing gear age that could lead to main landing
gear (MLG) and/or nose landing gear (NLG) collapse, and consequent
damage to the airplane and injury to the occupants.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Determination of Component Calendar Age
Within 90 days after the effective date of this AD: Verify the
airplane and/or the airplane technical records to determine whether
any MLG and NLG components are affected components based on their
calendar age, in accordance with Section 2, Part A, of the
Accomplishment Instructions of MHI RJ Service Bulletin (SB) 670BA-
32-062, Revision A, dated December 2, 2021.
(h) Removal and Replacement of Affected NLG Components
(1) Within the applicable compliance time indicated in figure 1
to paragraph (h) of this AD: Remove the affected NLG components
identified in paragraph (g) of this AD in accordance with Section 2,
Part B, of the Accomplishment Instructions of MHI RJ SB 670BA-32-
062, Revision A, dated December 2, 2021.
(2) Before further flight after removal of the affected
components, replace the removed components with serviceable
components, in accordance with Section 2, Part D, of the
Accomplishment Instructions of MHI RJ SB 670BA-32-062, Revision A,
dated December 2, 2021.
[[Page 68613]]
[GRAPHIC] [TIFF OMITTED] TR16NO22.004
(i) Removal and Replacement of Affected MLG Components
(1) Within the applicable compliance time indicated in figure 1
to paragraph (h) of this AD: Remove the affected MLG components
identified in paragraph (g) of this AD in accordance with Section 2,
Part E or H, as applicable, of the Accomplishment Instructions of
MHI RJ SB 670BA-32-062, Revision A, dated December 2, 2021.
(2) Before further flight after removing the affected
components, replace the removed components with serviceable
components, in accordance with Section 2, Part G or J, as
applicable, of the Accomplishment Instructions of MHI RJ SB 670BA-
32-062, Revision A, dated December 2, 2021.
(j) Parts Installation Limitation
(1) As of the effective date of this AD, no person may install,
on any airplane, any MLG or NLG component with a calendar age of 12
years or more unless it has been overhauled in accordance with
Section 2, Part C, F, or I, as applicable, of the Accomplishment
Instructions of MHI RJ SB 670BA-32-062, Revision A, dated December
2, 2021.
(2) As of the effective date of this AD, any MLG or NLG
component with a calendar age of less than 12 years may be installed
on any airplane, provided it is overhauled in accordance with
Section 2 Part C, F, or I, as applicable, of the Accomplishment
Instructions of MHI RJ SB 670BA-32-062, Revision A, dated December
2, 2021, prior to reaching 12 years' component calendar age.
(k) 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 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 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.
(l) Additional Information
(1) Refer to TCCA AD CF-2021-49, dated December 20, 2021, for
related information. This TCCA AD may be found in the AD docket at
regulations.gov under Docket No. FAA-2022-0885.
(2) For more information about this AD, contact Jiwan
Karunatilake, 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].
(m) 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 Service Bulletin 670BA-32-062, Revision A, dated
December 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 October 3, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-24902 Filed 11-15-22; 8:45 am]
BILLING CODE 4910-13-P
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Open the captured official edition
- Source SHA-256
- 3c4e8d9d035ac58053d3c8f935b165669d47bcc5280090f6b011e5cd829f2e44
- Text SHA-256
- 034cee212172551f0d97e1e5b9799897956957e1479f7fe1e4b4431381990ff2
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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.