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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 par
    -agraphs (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 al-
    ready 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 para-
    graph (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,  re-
    place the removed components with serviceable components,  in  accord-
    ance with Section 2, Part D, of the Accomplishment Instructions of MHI
    RJ SB 670BA-32-062, Revision A, dated December 2, 2021.

                 FIGURE 1 TO PARAGRAPH (H) – COMPLIANCE TIME              
    ______________________________________________________________________
    COMPONENT CALENDAR AGE                   COMPLIANCE TIME
    ______________________________________________________________________
    Less than 10 years              Prior to reaching 12 years’ component
                                    calendar age or within 36 months after
                                    the effective date of this AD, which-
                                    ever occurs later

    10 years or more and            Within 36 months after the effective
    less than 12 years              date of this AD or prior to reaching
                                    14 years’ component calendar age,
                                    whichever occurs first

    12 years or more and            Prior to reaching 14 years’ component
    less than 13 years              calendar age

    13 years or more and            Within 12 months after the effective
    less than 14 years              date of this AD

    14 years or more                Within 6 months after the effective
                                    date of this AD
    ______________________________________________________________________

(i) REMOVAL AND REPLACEMENT OF AFFECTED MLG COMPONENTS

(1) Within the applicable compliance time  indicated  in figure 1 to para-
    graph (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 Instruc-
    tions 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 air
    -plane, 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 re-
    quested using the procedures found in 14 CFR 39.19. In accordance with
    14 CFR 39.19, send your request to your principal inspector or respon-
    sible 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  accom-
    plished 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 in-
    formation.  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, Aero-
    space Engineer,  Airframe and Propulsion Section,  FAA,  New York  ACO
    Branch, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;  telephone
    516-228-7300; email 9-avs-nyacocos@faa.gov.

(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, Québec J7H 0E2 Canada;  North America toll-free tele-
    phone 833-990-7272 or direct-dial telephone 450-990-7272; fax 514-855-
    8501; email thd.crj@mhirj.com; website mhirj.com.

(4) You may view this service information at the FAA,  Airworthiness Prod-
    ucts 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 refer-
    ence at the National Archives and Records Administration  (NARA).  For
    information on the availability  of this material  at NARA,  email fr.
    inspection@nara.gov,  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.

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 9-avs
-nyacocos@faa.gov.
PREAMBLE 

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 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:
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.
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 9-avs-nyaco-cos@faa.gov.

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

Labor cost
Parts cost
Cost per product
Cost on U.S. 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 hour = Up to $2,720
Up to $340,000
Up to $342,720

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

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]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive: