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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2024-1468; Project Identifier MCAI-2023-00975-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    July 8, 2024.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD applies  to Bombardier,  Inc.,  Model  BD-700-2A12 airplanes,
    certificated  in any  category,  serial  numbers 70007,  70008, 70010,
    70012  through  70047  inclusive, 70049,  70051,  70052,  70053, 70055
    through  70077 inclusive,  70079, 70080,  70081,  70083  through 70133
    inclusive, 70135, 70136, 70137, 70138, 70142 through 70148  inclusive,
    70150, 70152, and 70158.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 78, Engine exhaust.

(e) UNSAFE CONDITION

    This AD was prompted by reports that the pivot door pressure seals  on
    the thrust reverser fixed structure were found disbonded or missing on
    several airplanes.  The FAA  is issuing  this AD  to address the pivot
    door pressure seals on the thrust reverser fixed structure. The unsafe
    condition, if not addressed, could result in engine thrust loss due to
    flow path overboard leakage during forward thrust operation and reduce
    airplane performance during one-engine inoperative conditions in climb
    margin and ceiling altitude.

(f) COMPLIANCE

    Comply  with this  AD within  the compliance  times specified,  unless
    already done.

(g) INSPECTION AND FUNCTIONAL TEST

(1) Within 750 flight hours or 18 months,  whichever comes first  from the
    effective date  of this  AD, perform  a general  visual inspection for
    discrepancies (missing, damaged,  or disbonding) of  the 4 pivot  door
    pressure seals on the thrust reverser door of each engine, and perform
    a bonding check as applicable,  and repair or replace each  discrepant
    seal as applicable, in accordance with Part 2.B of the  Accomplishment
    Instructions of Bombardier Service Bulletin 700-78-7501, Revision  01,
    dated July 13, 2023. Applicable corrective actions must be done before
    further flight.

(2) Before further flight  after  accomplishing  the  actions specified in
    paragraph (g)(1) of this AD:  Perform a functional test of  the thrust
    reverser  in   accordance  with   Part  2.C   of  the   Accomplishment
    Instructions of Bombardier Service Bulletin 700-78-7501,  Revision 01,
    dated July 13, 2023.

(h) CREDIT FOR PREVIOUS ACTIONS

    This paragraph provides credit  for actions required by  paragraph (g)
    of this AD, if those actions were performed before the effective  date
    of this AD using Bombardier Service Bulletin 700-78-7501, dated  April
    12, 2023.

(i) NO REPORTING REQUIREMENT

    Although  the  service information  referenced  in Bombardier  Service
    Bulletin 700-78-7501, Revision 01,  dated July 13, 2023,  specifies to
    submit  certain  information to  the  manufacturer, this  AD  does not
    include that requirement.

(j) ADDITIONAL AD PROVISIONS

    The following provisions also apply to this AD:

(1) Alternative Methods of Compliance (AMOCs):  The Manager, International
    Validation 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 International
    Validation Branch, mail it to the address identified in paragraph  (k)
    of this  AD. Information  may be  emailed to: 9-AVS-NYACO-COS@faa.gov.
    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,  International
    Validation Branch,  FAA; or  Transport Canada;  or Bombardier,  Inc.'s
    Transport Canada  Design Approval  Organization (DAO).  If approved by
    the DAO, the approval must include the DAO-authorized signature.

(k) ADDITIONAL INFORMATION

    For more information about this AD, contact Joseph Catanzaro, Aviation
    Safety Engineer,  FAA,  1600 Stewart Avenue,  Suite 410,  Westbury, NY
    11590; telephone 516-228-7366; email joseph.catanzaro@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 700-78-7501,  Revision 01,  dated July 13,
    2023.

(ii) [Reserved]

(3) For Bombardier, Inc. service information,  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.

(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 at the National Archives and Records Admin-
    istration (NARA). For information on the availability of this material
    at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations, or
    email fr.inspection@nara.gov.

Issued on May 14, 2024. James D. Foltz, Deputy Director, Compliance & Air-
worthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this proposed AD by July 8, 2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-1468; Project Identifier MCAI-2023-00975-T]
RIN 2120-AA64

Airworthiness Directives; Bombardier, Inc., Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Bombardier, Inc., Model BD-700-2A12 airplanes. This
proposed AD was prompted by reports that the pivot door pressure seals
on the thrust reverser fixed structure were found disbonded or missing
on several airplanes. This proposed AD would require inspecting the
pivot door pressure seals and accomplishing applicable corrective
actions. This proposed AD would also require a functional test of the
thrust reversers. The FAA is proposing this AD to address the unsafe
condition on these products.

DATES: The FAA must receive comments on this proposed AD by July 8,
2024.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2024-1468; 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 NPRM, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For Bombardier, Inc. service information, 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 service information 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.

FOR FURTHER INFORMATION CONTACT: Joseph Catanzaro, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 516-228-7366; email joseph.catanzaro@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2024-1468; Project Identifier
MCAI-2023-00975-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
the proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.

Confidential Business Information

CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to
Joseph Catanzaro, Aviation Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone 516-228-7366; email
joseph.catanzaro@faa.gov. Any commentary that the FAA receives which is
not specifically designated as CBI will be placed in the public docket
for this rulemaking.

Background

Transport Canada, which is the aviation authority for Canada, has
issued Transport Canada AD CF-2023-61, dated August 16, 2023 (Transport
Canada AD CF-2023-61) (also referred
to after this as the MCAI), to correct an unsafe condition on certain
serial-numbered Bombardier, Inc., Model BD-700-2A12 airplanes. The MCAI
states that the pivot door pressure seals on the thrust reverser fixed
structure were found disbonded or missing on several airplanes. The
investigation revealed that the seal disbond condition was caused by
the variation in the installation process of the seals during bonding
surface preparation and sealant application. The unsafe condition, if
not addressed, could result in engine thrust loss due to flow path
overboard leakage during forward thrust operation and reduce airplane
performance during one-engine inoperative conditions in climb margin
and ceiling altitude.
The FAA is proposing 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-2024-1468.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Bombardier Service Bulletin 700-78-7501, Revision
01, dated July 13, 2023. This service information specifies procedures
for a one-time general visual inspection for discrepant (missing,
damaged, or disbonded) thrust reverser pivoting door pressure seals, a
bonding check of the pivoting door seals, and repair or replacement of
discrepant seals. This service information also specifies procedure for
performing a functional test of the thrust reverser.
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.

FAA's Determination


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 and
service information referenced above. The FAA is issuing this NPRM
after determining that the unsafe condition described previously is
likely to exist or develop on other products of the same type design.

Proposed AD Requirements in This NPRM

This proposed AD would require accomplishing the actions specified
in the service information already described.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 53 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:

Estimated Costs for Required Actions

Labor cost
Parts cost
Cost per product
Cost on U.S. operators
6 work-hours x $85 per hour = $510
$0
$510
$27,030

The FAA estimates the following costs to do any necessary on-
condition action 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 this on-condition action:

Estimated Costs of On-Condition Actions

Labor cost
Parts cost
Cost per product
Up to 24 work-hours x $85 per hour = $2,040
$4,850
Up to $6,890

The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this proposed 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

The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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 Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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: