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2023-04-01 BOMBARDIER, INC.: Amendment 39-22348; Docket No. FAA-2022-1646; Project Identifier MCAI-2022-01135-T.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective April 7, 2023.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Bombardier, Inc., Model BD-700-2A12 airplanes, cer-
    tificated in any category,  serial numbers  70006 through 70061 inclu-
    sive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code: 52, Doors.

(e) UNSAFE CONDITION

    This AD was  prompted by a  report that the  passenger door functional
    test engineering requirements (FTERs)  were not fully accomplished  on
    several  airplanes. The  FAA is  issuing this  AD to  ensure that  the
    passenger  door  is  properly rigged.  The  unsafe  condition, if  not
    addressed, could result  in higher loads  on the passenger  door stops
    that could initiate  cracks before the  intended design service  goal,
    and an in-flight opening of the passenger door.

(f) COMPLIANCE

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

(g) REQUIREMENTS

    Within 72  months after  the effective  date of  this AD,  measure the
    passenger door steps and gap values  on each lateral side of the  door
    at 8 points, and on the lower and upper sides of the door at 4 points,
    in  accordance  with  Part A  of  the  Accomplishment Instructions  of
    Bombardier Service  Bulletin 700-52-7511,  dated  July 22, 2022.  Then
    accomplish the actions  specified by paragraph  (g)(1) or (2)  of this
    AD, as applicable.

(1) If any measurement is not within the specified limits,  before further
    flight,  re-adjust  the  passenger door steps  and  gaps to obtain the
    acceptable (necessary) values  in accordance with Part B of the Accom-
    plishment  Instructions  of  Bombardier  Service Bulletin 700-52-7511,
    dated July 22, 2022.

(2) If all of the measurements  are  within  the  specified limits, before
    further flight,  with  the  door in the closed position,  measure  the
    passenger door stops gaps in accordance with Part C of the Accomplish-
    ment Instructions  of Bombardier  Service Bulletin  700-52-7511, dated
    July 22,  2022. If  any passenger  door stops  gaps measurement is not
    within  the  specified  limits,  before further flight,  re-adjust the
    passenger door stops  to obtain the  acceptable (necessary) values  in
    accordance with Part D  of the Accomplishment Instructions  of Bombar-
    dier Service Bulletin 700-52-7511, dated July 22, 2022.

(h) NO REPORTING REQUIREMENT

    Although Bombardier Service Bulletin 700-52-7511, dated July 22, 2022,
    specifies to submit certain information to the manufacturer,  this  AD
    does not include that requirement.

(i) ADDITIONAL 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;  or  Bombardier  Inc.'s Transport
    Canada Design Organization Approval (DOA). If approved by the DOA, the
    approval must include the DOA-authorized signature.

(j) ADDITIONAL INFORMATION

(1) Refer to Transport Canada AD CF-2022-48,  dated  August 18, 2022,  for
    related  information.  This Transport Canada AD may be found in the AD
    docket at regulations.gov under Docket No. FAA-2022-1646.

(2) For more information about this AD, contact Gabriel Kim, Aerospace En-
    gineer,  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.

(k) 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) Bombardier Service Bulletin 700-52-7511, dated July 22, 2022.

(ii) [Reserved]

(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; website bombardier.com.

(4) You may view this material at the FAA, Airworthiness Products Section,
    Operational Safety Branch,  2200 South 216th Street,  Des Moines,  WA.
    For information on the availability of this material at the FAA,  call
    206-231-3195.

(5) You may view  this material  that is incorporated  by reference 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 February 14, 2023. Christina Underwood, Acting Director, Compli-
ance & Airworthiness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT: Gabriel Kim, Aerospace Engineer, Mechani-
cal 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-2022-1646; Project Identifier MCAI-2022-01135-T;
Amendment 39-22348; AD 2023-04-01]
RIN 2120-AA64

Airworthiness Directives
; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Bombardier, Inc., Model BD-700-2A12 airplanes. This AD was
prompted by report that the passenger door functional test engineering
requirements (FTERs) were not fully accomplished on several airplanes.
This AD requires measuring the passenger door steps, passenger door
gaps, and passenger door stops rigging, and re-adjusting the door if
necessary. The FAA is issuing this AD to address the unsafe condition
on these products.

DATES: This AD is effective April 7, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of April 7,
2023.

ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1646; 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 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; website
bombardier.com.
You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th Street,
Des Moines, WA. For information on the availability of this material at
the FAA, call 206-231-3195. It is also available in the AD docket at
regulations.gov under Docket No. FAA-2022-1646.

FOR FURTHER INFORMATION CONTACT: Gabriel Kim, 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:

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 Bombardier,
Inc., Model BD-700-2A12 airplanes. The NPRM published in the Federal
Register on December 16, 2022 (87 FR 77040). The NPRM was prompted by
AD CF-2022-48, dated August 18, 2022, issued by Transport Canada, which
is the aviation authority for Canada (Transport Canada AD CF-2022-48)
(also referred to as the MCAI). The MCAI states that non-conformities
have been reported involving the passenger door FTERs. It has been
found that the FTER was not fully accomplished on several airplanes
with the assembled airplane in the weight-on-wheel condition, which
could affect the rigging of the passenger door. Door mis-rigging could
result in higher loads on the passenger door stops that could initiate
cracks before the intended design service goal, and an in-flight
opening of the passenger door
In the NPRM, the FAA proposed to require measuring the passenger
door steps, passenger door gaps, and passenger door stops rigging, and
re-adjusting the door 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-2022-1646.

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 Bombardier Service Bulletin 700-52-7511, dated
July 22, 2022. This service information specifies procedures for
measuring the passenger door steps and gaps, rigging of the passenger
door stops, and corrective actions if the measurements are not within
the specified limits. This material 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 29 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
Up to 4 work-hours x $85 per hour = $340
$0
$340
Up to $9,860

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 30 work-hours x $85 per hour = $3,400
$0
Up to $3,400

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this AD may be covered under warranty, thereby reducing the cost impact
on affected operators.

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: