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2022-09-02 BOMBARDIER, INC.: Amendment 39-22022; Docket No. FAA-2022-0016; Project Identifier MCAI-2021-00945-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective June 16, 2022.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to Bombardier, Inc.,  Model  BD-100-1A10 airplanes,
    certificated  in  any  category, serial  numbers  20003  through 20892
    inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 32, Landing gear.

(e) UNSAFE CONDITION

    This AD was prompted by a report that the nose wheel steering selector
    valve  (SSV)  can  be   slow  to  deactivate  under   low  temperature
    conditions. The FAA is  issuing this AD to  address a slow nose  wheel
    SSV deactivation, which, in combination with an un-commanded  steering
    input, could  lead to  a delayed  transition to  free castor  mode and
    result in an aircraft runway excursion.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REPLACEMENT OF NOSE WHEEL SSV

    Within 36 months after the effective date of this AD: Replace the nose
    wheel SSV  part number  41130-107 with  the redesigned  nose wheel SSV
    part  number  41130-111;  and   before  further  flight,  perform   an
    operational test of the nose wheel SSV and nose wheel steering control
    system;  in  accordance   with  paragraphs  2.B.   and  2.C.  of   the
    Accomplishment  Instructions  of  the  applicable  service information
    specified in paragraphs (g)(1) and (2) of this AD. If any test  fails,
    do applicable corrective  actions and repeat  the test until  the part
    passes the test.

(1) Bombardier Service Bulletin 100-32-35, dated March 30, 2021.

(2) Bombardier Service Bulletin 350-32-011, dated March 30, 2021.

(h) PARTS INSTALLATION PROHIBITION

    Do not install nose wheel SSV,  part number 41130-107  on any airplane
    as of the applicable compliance time  specified in paragraph (h)(1) or
    (2) of this AD.

(1) For  airplanes  that  have  nose wheel SSV,  part number 41130-107 in-
    stalled as of the effective date of this AD: After replacement of nose
    wheel SSV as required by paragraph (g) of this AD.

(2) For airplanes that,  as of the effective date of this AD,  do not have
    nose wheel SSV,  part number 41130-107 installed:  As of the effective
    date of this AD.

(i) NO REPORTING REQUIREMENT

    Although the service information  specified  in  paragraphs (g)(1) and
    (2) of this AD specifies to submit certain information to the manufac-
    turer, this AD does not include that requirement.

(j) 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 Bombardier,
    Inc.'s TCCA  Design Approval  Organization (DAO).  If approved  by the
    DAO, the approval must include the DAO-authorized signature.

(k) RELATED INFORMATION

(1) Refer to Mandatory Continuing Airworthiness Information  (MCAI) Trans-
    port Canada AD CF-2021-29, dated August 18, 2021, for related informa-
    tion.  This MCAI may be found  in the AD docket  on  the  internet  at
    https://www.regulations.gov  by searching for and locating  Docket No.
    FAA-2022-0016.

(2) For more information about this AD,  contact Chirayu Gupta,  Aerospace
    Engineer, Mechanical Systems and Administrative Services 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.

(l) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference (IBR) of  the service information  listed in this  paragraph
    under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable  to do the actions
    required by this AD, unless this AD specifies otherwise.

(i) Bombardier Service Bulletin 100-32-35, dated March 30, 2021.

(ii) Bombardier Service Bulletin 350-32-011, dated March 30, 2021.

(3) For service information identified in this AD, contact Bombardier Bus-
    iness Aircraft  Customer  Response  Center,  400 Cote-Vertu Road West,
    Dorval, Quebec H4S 1Y9, Canada;  telephone 514-855-2999; email ac.yul@
    aero.bombardier.com; internet http://www.bombardier.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:  https://www.archives.gov/federal-
    register/cfr/ibr-locations.html.

Issued on April 11, 2022. Lance T. Gant, Director, Compliance & Airworthi-
ness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:Chirayu Gupta, Aerospace Engineer, Mechan-
ical Systems and Administrative Services 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.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0016; Project Identifier MCAI-2021-00945-T;
Amendment 39-22022; AD 2022-09-02]
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
certain Bombardier, Inc., Model BD-100-1A10 airplanes. This AD was
prompted by a report that the nose wheel steering selector valve (SSV)
can be slow to deactivate under low temperature conditions. This AD
requires replacing the affected nose wheel SSV with a redesigned nose
wheel SSV, and performing an operational test of the nose wheel SSV and
nose wheel steering control system. This AD also prohibits the
installation of a certain nose wheel SSV. The FAA is issuing this AD to
address the unsafe condition on these products.

DATES: This AD is effective June 16, 2022.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of June 16,
2022.

ADDRESSES: For service information identified in this final rule,
contact Bombardier Business Aircraft Customer Response Center, 400
Cote-Vertu Road West, Dorval, Quebec H4S 1Y9, Canada;
telephone 514-855-2999; email ac.yul@aero.bombardier.com; internet
http://www.bombardier.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 on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2022-
0016.

Examining the AD Docket

You may examine the AD docket on the internet at https://www.regulations.
gov by searching for and locating Docket No. FAA-2022-
0016; 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.

FOR FURTHER INFORMATION CONTACT: Chirayu Gupta, Aerospace Engineer,
Mechanical Systems and Administrative Services 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:

Discussion

Transport Canada Civil Aviation (TCCA), which is the aviation
authority for Canada, has issued TCCA AD CF-2021-29, dated August 18,
2021 (TCCA AD CF-2021-29) (also referred to as the MCAI), to correct an
unsafe condition for certain Bombardier, Inc., Model BD-100-1A10
airplanes. You may examine the MCAI in the AD docket on the internet at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2022-0016.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain Bombardier,
Inc., Model BD-100-1A10 airplanes. The NPRM published in the Federal
Register on January 27, 2022 (87 FR 4170). The NPRM was prompted by a
report that the nose wheel SSV can be slow to deactivate under low
temperature conditions. The NPRM proposed to require replacing the
affected nose wheel SSV with a redesigned nose wheel SSV, and
performing an operational test of the nose wheel SSV and nose wheel
steering control system. The NPRM also proposed to prohibit the
installation of a certain nose wheel SSV. The FAA is issuing this AD to
address a slow nose wheel SSV deactivation, which, in combination with
an un-commanded steering input, could lead to a delayed transition to
free castor mode and result in an aircraft runway excursion. See the
MCAI for additional background information.

Comments

The FAA gave the public the opportunity to participate in
developing this final rule. The FAA received no comments on the NPRM or
on the determination of the cost to the public.

Conclusion

The FAA reviewed the relevant data 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:
Are consistent with the intent that was proposed in the
NPRM for addressing the unsafe condition; and
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 Service Bulletin 100-32-35, dated March 30,
2021; and Service Bulletin 350-32-011, dated March 30, 2021. This
service information describes procedures for replacing the existing
nose wheel SSV (part number 41130-107) with a redesigned nose wheel SSV
(part number 41130-111), and performing an operational test of the nose
wheel SSV and nose wheel steering control system. These documents are
distinct since they apply to different airplane configurations. 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 660 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
$5,793
$6,133
$4,047,780

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: