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PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2024-2543; Project Identifier MCAI-2024-00342-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this  airworthiness directive (AD) by
    January 13, 2025.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to all Bombardier, Inc., Model BD-700-2A12 airplanes.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 34, Navigation.

(e) UNSAFE CONDITION

    This AD was prompted  by the discovery that  a partial loss of  thrust
    after  an  engine  failure during  a  required  navigation performance
    authorization  required  (RNP-AR)   approach  under  certain   weight,
    altitude,  and temperature  (WAT) conditions,  may lead  to a  descent
    below  75  feet  of  the path  guidance,  requiring  a  go-around. The
    resultant vertical deviation may exceed allowable approach containment
    for obstacle clearance and may reduce the safety margins in the missed
    approach.

(f) COMPLIANCE

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

(g) REVISION OF EXISTING AIRPLANE FLIGHT MANUAL (AFM)

    Within  30  days after  the  effective date  of  this AD,  revise  the
    existing  AFM to  include the  information specified  in  (Bombardier)
    Global 7500  Airplane Flight  Manual Temporary  Revision TR-58,  dated
    March 21, 2024.

(h) 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, send it to  the attention of the person  identified
    in paragraph (i) of this  AD and email to: AMOC@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.

(i) ADDITIONAL INFORMATION

    For more information about this AD, contact Joseph Catanzaro, Aviation
    Safety Engineer,  FAA, 1600  Stewart Avenue,  Suite 410,  Westbury, NY
    11590; phone: 516-228-7300; email: 9-avs-nyaco-cos@faa.gov.

(j) MATERIAL INCORPORATED BY REFERENCE

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

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

(i) (Bombardier) Global 7500 Airplane Flight Manual Temporary Revision TR-
    58, dated March 21, 2024.

(ii) Reserved

(3) For material identified  in this AD, contact  Bombardier Business Air-
    craft  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 St., 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 November 21, 2024. Victor Wicklund, Deputy Director,  Compliance
& Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must  receive comments on this  proposed AD by January  13,
2025.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


14 CFR Part 39

[Docket No. FAA-2024-2543; Project Identifier MCAI-2024-00342-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 all Bombardier, Inc., Model BD-700-2A12 airplanes. This proposed AD
was prompted by the discovery that a partial loss of thrust after an
engine failure during a required navigation performance authorization
required (RNP-AR) approach under certain weight, altitude and
temperature (WAT) conditions, may lead to a descent below the specified
path guidance. This proposed AD would require a revision to the
existing airplane flight manual (AFM), to incorporate updated WAT
tables for RNP-AR approach operations. 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 January 13, 2025.

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-2024-2543; 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 material identified in this proposed AD,
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 St., 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;
phone: 516-228-7300; email: 9-avs-nyaco-cos@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 the ADDRESSES section. Include "Docket No. FAA-2024-2543;
Project Identifier MCAI-2024-00342-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; phone: 516-228-7300;
email: 9-avs-nyaco-cos@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-2024-22, dated June 13, 2024 (Transport
Canada AD CF-2024-22) (also referred to after this as the MCAI), to
correct an unsafe condition on all Bombardier, Inc., Model BD-700-2A12
airplanes. The MCAI states that it was discovered that a partial loss
of thrust after an engine failure during an RNP-AR approach under
certain WAT conditions, may lead to a descent below 75 foot of the path
guidance, requiring a go-around. The resultant vertical deviation may
exceed allowable approach containment for obstacle clearance and may
largely reduce the safety margins in the missed approach.

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__.

Material Incorporated by Reference Under 1 CFR Part 51

The FAA reviewed (Bombardier) Global 7500 Airplane Flight Manual
Temporary Revision TR-58, dated March 21, 2024. This material specifies
procedures to update WAT tables for RNP-AR approach operations to
contain possible vertical deviations within the 75 foot requirement.

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.

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
material 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 a revision to the existing AFM to
incorporate updated WAT tables for RNP-AR approach operations that
contain possible vertical deviations within the 75 foot requirement.

Compliance With AFM Revisions

Transport Canada AD CF-2024-22 requires operators to "advise all
flight crews" of revisions to the AFM, and thereafter to "operate the
aeroplane accordingly." However, this proposed AD would not
specifically require those actions as those actions are already
required by FAA regulations.

FAA regulations require operators furnish to pilots any changes to
the AFM (for example, 14 CFR 121.137), and to ensure the pilots are
familiar with the AFM (for example, 14 CFR 91.505). As with any other
flightcrew training requirement, training on the updated AFM content is
tracked by the operators and recorded in each pilot's training record,
which is available for the FAA to review. FAA regulations also require
pilots to follow the procedures in the existing AFM including all
updates. 14 CFR 91.9 requires that any person operating a civil
aircraft must comply with the operating limitations specified in the
AFM. Therefore, including a requirement in this proposed AD to operate
the airplane according to the revised AFM would be redundant and
unnecessary.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 70 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
1 work-hour x $85 per hour = $85.
$0
$85
$5,950

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: