preamble attached >>>
ADs updated daily at www.Tdata.com
PROPOSED AD BOMBARDIER, INC.: Docket No. FAA-2024-1483; Project Identifier MCAI-2023-01094-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    July 29, 2024.

(b) AFFECTED ADS

    This AD replaces AD 2021-10-02,  Amendment 39-21535 (86 FR 33088, June
    24, 2021) (AD 2021-10-02).

(c) APPLICABILITY

    This AD applies to Bombardier, Inc., Model BD-700-1A10, and -1A11 air-
    planes, certificated in any category having serial number 9002 through
    60081 inclusive.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 05,  Time Limits/Main-
    tenance Checks; 55, Flight Controls.

(e) REASON

    This AD was prompted by a determination that new airworthiness limita-
    tions are necessary.  The FAA is issuing  this AD to address sand con-
    tamination and corrosion of  the elevator torque tube  bearings, which
    could lead to binding or seizure of the bearings, and potentially lead
    to a reduction in or loss of airplane pitch control.

(f) COMPLIANCE

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

(g) RETAINED INSPECTION AND CORRECTIVE ACTIONS, WITH CHANGE

    This paragraph restates the requirements of paragraph (g)  of AD 2021-
    10-02, with change to Figure 1 to paragraph (g), which identifies  the
    airplane marketing  designation instead  of the  serial number  range.
    Within 36 months from July 29, 2021 (the effective date of AD  2021-10
    -02) or  within 63  months from  the date  of airplane manufacture, as
    identified  on  the  identification plate  of the  airplane, whichever
    occurs later: Do  a general visual  inspection of the  left- and right
    -hand elevator torque tube bearings for any sand, dust, or  corrosion;
    perform a functional test of  the elevator control system; and  do all
    applicable corrective actions;  in accordance with  the Accomplishment
    Instructions  of paragraphs  2.B., 2.C.,  and 2.D.  of the  applicable
    service information specified in figure 1 to paragraph (g) of this AD.
    Applicable  corrective actions  must  be  done before  further flight.
    Repeat the general visual inspection and functional test thereafter at
    intervals not to exceed 63  months. Accomplishing the revision of  the
    existing maintenance or inspection  program required by paragraph  (i)
    of this AD terminates the requirements of this paragraph.

                 FIGURE 1 TO PARAGRAPH (G) - SERVICE INFORMATION          
    ______________________________________________________________________
                                WITH MARKETING          USE BOMBARDIER
          FOR MODEL-            DESIGNATION-            SERVICE BULLETIN-
    ______________________________________________________________________
    BD-700-1A10 airplanes     Global Express or       700-27-083, Revision
                              Global Express XRS      1, dated December
                                                      7, 2020.

    BD-700-1A10 airplanes     Global 6000             700-27-6012,
                                                      Revision 1, dated
                                                      December 7, 2020.

    BD-700-1A10 airplanes     Global 6500             700-27-6503,
                                                      Revision 1, dated
                                                      December 7, 2020.

    BD-700-1A11 airplanes     Global 5000             700-1A11-27-041,
                                                      Revision 1, dated
                                                      December 7, 2020.

    BD-700-1A11 airplanes     Global 5000             700-27-5012,
                              Featuring Global        Revision 1, dated
                              Vision Flight Deck      December 7, 2020.
                              (GVFD)

    BD-700-1A11 airplanes     Global 5500             700-27-5503,
                                                      Revision 1, dated
                                                      December 7, 2020.
    ______________________________________________________________________

(h) NO REPORTING REQUIREMENT

    Although the service information  identified in Figure 1  to paragraph
    (g)  of  this  AD  specifies  to  submit  certain  information  to the
    manufacturer, this AD does not include that requirement.

(i) NEW REVISION OF THE EXISTING MAINTENANCE OR INSPECTION PROGRAM

    Within  30  days after  the  effective date  of  this AD,  revise  the
    existing  maintenance  or   inspection  program,  as   applicable,  to
    incorporate  the  information specified  in  the applicable  temporary
    revision  identified in  figure 2  to paragraph  (i) of  this AD.  The
    initial compliance time for doing  the tasks is at the  time specified
    in  the  applicable  temporary  revision  identified  in  figure  2 to
    paragraph (i) of this AD, or  within 90 days after the effective  date
    of this AD, whichever occurs later. Accomplishing the revision of  the
    existing maintenance or inspection program required by this  paragraph
    terminates the actions required by paragraph (g) of this AD.

                 FIGURE 2 TO PARAGRAPH (I) - SERVICE INFORMATION          
    ______________________________________________________________________
                                                       USE BOMBARDIER
         FOR MODEL-            USING TLMC MANUAL-      TEMPORARY REVISION-
    ______________________________________________________________________
    BD-700-1A10 airplanes     Bombardier Global        5-2-53, dated March
                              Express BD-700 TLMC      31, 2023.

    BD-700-1A10 airplanes     Bombardier Global        5-2-15, dated March
                              Express XRS, BD-700      31, 2023.
                              TLMC

    BD-700-1A10 airplanes     Bombardier Global        5-2-20, dated March
                              6000, GL 6000 TLMC       31, 2023.

    BD-700-1A10               Global 6500, GL 6500     5-2-3, dated March
                              TLMC                     31, 2023.

    BD-700-1A11 airplanes     Bombardier Global        5-2-21, dated March
                              5000 BD-700 TLMC         31, 2023.

    BD-700-1A11 airplanes     Bombardier Global        5-2-20, dated March
                              5000 GL 5000             31, 2023.
                              Featuring Global
                              Vision Flight Deck
                              (GVFD) TLMC

    BD-700-1A11 airplanes     Global 5500 GL 5500      5-2-3, dated March
                              TLMC                     31, 2023.
    ______________________________________________________________________

(j) NEW NO ALTERNATIVE ACTIONS OR INTERVALS

    After the existing maintenance or inspection program has been  revised
    as required by paragraph (i) of this AD, no alternative actions (e.g.,
    inspections) or intervals may be used unless the actions and intervals
    are  approved  as  an  alternative  method  of  compliance  (AMOC)  in
    accordance with the procedures  specified in paragraph (l)(1)  of this
    AD.

(k) CREDIT FOR PREVIOUS ACTIONS

(1) This paragraph provides credit  for actions required  by paragraph (g)
    of this AD,  if those actions were performed before July 29, 2021 (the
    effective date of AD 2021-10-02) using the applicable service informa-
    tion in paragraphs (k)(1)(i) through (vi) of this AD,  which  are  not
    incorporated by reference in this AD.

(i) Bombardier Service Bulletin 700-1A11-27-041, dated July 23, 2020.

(ii) Bombardier Service Bulletin 700-27-083, dated July 23, 2020.

(iii) Bombardier Service Bulletin 700-27-5012, dated July 23, 2020.

(iv) Bombardier Service Bulletin 700-27-5503, dated July 23, 2020.

(v) Bombardier Service Bulletin 700-27-6012, dated July 23, 2020.

(vi) Bombardier Service Bulletin 700-27-6503, dated July 23, 2020.

(2) This paragraph provides credit  for the initial and repetitive inspec-
    tion actions required by paragraph (i)  of  this  AD  if those actions
    were performed before the effective date of this AD  using the applic-
    able service information  identified  in  figure 1 to paragraph (g) of
    this AD, which were incorporated by reference in AD 2021-10-02, Amend-
    ment 39-21535 (86 FR 33088, June 24, 2021).

(l) 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
    (m)(1)  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.

(m) ADDITIONAL INFORMATION

(1) For more information about this AD contact Gabriel Kim, Aviation Safe-
    ty Engineer, FAA, 1600 Stewart Avenue, Suite 410,  Westbury, NY 11590;
    telephone 516-228-7300; email 9-avs-nyaco-cos@faa.gov.

(2) Service information identified in this AD  that is not incorporated by
    reference is available at the address specified in paragraph (n)(5) of
    this AD.

(n) 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.

(3) The following service information  was  approved  for  IBR on [DATE 35
    DAYS AFTER PUBLICATION OF THE FINAL RULE].

(i) Bombardier  Global  Express,  BD-700 Temporary Revision 5-2-53,  dated
    March 31, 2023 (for Model BD-700-1A10 airplanes).

(ii) Bombardier Global Express XRS, BD-700 Temporary Revision 5-2-15 dated
     March 31, 2023 (for Model BD-700-1A10 airplanes).

(iii) Bombardier  Global  6000,  GL 6000 Temporary Revision 5-2-20,  dated
      March 31, 2023 (for Model BD-700-1A10 airplanes).

(iv) [Bombardier]  Global  6500,  GL 6500 Temporary Revision 5-2-3,  dated
     March 31, 2023 (for Model BD-700-1A10 airplanes).

(v) Bombardier Global 5000,  BD-700 Temporary Revision 5-2-21, dated March
    31, 2023 (for Model BD-700-1A11 airplanes).

(vi) Bombardier  Global  5000  GL 5000 Featuring Global Vision Flight Deck
     Temporary Revision 5-2-20 dated March 31, 2023 (for Model BD-700-1A11
     airplanes).

(vii) [Bombardier] Global 5500 GL 5500  Temporary  Revision,  5-2-3, dated
      March 31, 2023 (for Model BD-700-1A11 airplanes).

(4) The  following  service  information  was approved for IBR on July 29,
    2021 (86 FR 33088, June 24, 2021).

(i) Bombardier Service Bulletin 700-1A11-27-041, Revision 1,  dated Decem-
    ber 7, 2020.

(ii) Bombardier Service Bulletin 700-27-083, Revision 1, dated December 7,
     2020.

(iii) Bombardier Service Bulletin 700-27-5012, Revision 1,  dated December
      7, 2020.

(iv) Bombardier Service Bulletin 700-27-5503, Revision 1 dated December 7,
     2020.

(v) Bombardier Service Bulletin 700-27-6012, Revision 1, dated December 7,
    2020.

(vi) Bombardier Service Bulletin 700-27-6503, Revision 1 dated December 7,
     2020.

(5) For Bombardier service information,  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.

(6) 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.

(7) 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 June 5, 2024.  Suzanne Masterson,  Deputy  Director,  Integrated
Certificate Management Division, Aircraft Certification Service.

DATES: The FAA must receive comments on this NPRM by July 29, 2024.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-1483; Project Identifier MCAI-2023-01094-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 supersede Airworthiness Directive (AD)
2021-10-02, which applies to all Bombardier, Inc., Model BD-700-1A10
and BD-700-1A11 airplanes. AD 2021-10-02 requires repetitive general
visual inspections of the left- and right-hand elevator torque tube
bearings for any sand, dust, or corrosion; repetitive functional tests
of the elevator control system; and replacement of the elevator torque
tube bearings if necessary. Since the FAA issued AD 2021-10-02, the FAA
has determined that a new airworthiness limitation is necessary. This
proposed AD would continue to require certain actions in AD 2021-10-02
and require revising the existing maintenance or inspection program, as
applicable, to incorporate new airworthiness limitations. The FAA is
proposing this AD to address the unsafe condition on these products.

DATES: The FAA must receive comments on this NPRM by July 29, 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-2024-1483; 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, 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: Gabriel Kim, Aviation Safety Engineer,
FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 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 ADDRESSES. Include ``Docket No. FAA-2024-1483; Project Identifier
MCAI-2023-01094-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
Gabriel Kim, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite
410, Westbury, NY 11590; telephone 516-228-7300; email 9-avs-nyaco-cos@faa.gov.
Any commentary that the FAA receives that is not
specifically designated as CBI will be placed in the public docket for
this rulemaking.

Background

The FAA issued AD 2021-10-02, Amendment 39-21535 (86 FR 33088, June
24, 2021) (AD 2021-10-02), for all Bombardier, Inc., Model BD-700-1A10
and BD-700-1A11 airplanes. AD 2021-10-02 was prompted by an MCAI
originated by Transport Canada, which is the aviation authority for
Canada. Transport Canada issued AD CF-2020-29, dated August 21, 2020
(Transport Canada AD CF-2020-29), to correct an unsafe condition.
AD 2021-10-02 requires repetitive general visual inspections of the
left- and right-hand elevator torque tube bearings for any sand, dust,
or corrosion; repetitive functional tests of the elevator control
system; and replacement of the elevator torque tube bearings if
necessary. The FAA issued AD 2021-10-02 to address sand contamination
and corrosion of the elevator torque tube bearings, which could lead to
binding or seizure of the bearings, and potentially lead to a
reduction in or loss of airplane pitch control.

Actions Since AD 2021-10-02 Was Issued

Since the FAA issued AD 2021-10-02, Transport Canada superseded
Transport Canada CF-2020-29, and issued Transport Canada AD CF-2020-
29R1, dated October 20, 2023 (Transport Canada AD CF-2020-29R1)
(referred to after this as the MCAI) to correct an unsafe condition on
certain Bombardier, Inc., Model BD-700-1A10 and BD-700-1A11 airplanes.
The MCAI states that data collected from the reports mandated by
Transport Canada AD CF-2020-29 was used to validate inspection
intervals, which have been integrated into new certification
maintenance requirement (CMR) tasks. The MCAI also states that
Transport Canada AD CF-2020-29R1 mandates the new CMR tasks while
giving credit for initial and repetitive inspections already performed,
revises the applicability to exclude airplanes delivered with the new
CMRs, and removes the reporting requirement.
The FAA is proposing this AD to address sand contamination and
corrosion of the elevator torque tube bearings, which could lead to
binding or seizure of the bearings, and potentially lead to a reduction
in or loss of airplane pitch control.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2024-1483.

Related Service Information Under 1 CFR Part 51

The FAA reviewed the following Bombardier temporary revisions:
Bombardier Global Express, BD-700 Temporary Revision 5-2-
53, dated March 31, 2023 (for Model BD-700-1A10 airplanes);
Bombardier Global Express XRS, BD-700 Temporary Revision
5-2-15, dated March 31, 2023 (for Model BD-700-1A10 airplanes);
Bombardier Global 6000, GL 6000 Temporary Revision 5-2-20,
dated March 31, 2023 (for Model BD-700-1A10 airplanes);
[Bombardier] Global 6500, GL 6500 Temporary Revision 5-2-
3, dated March 31, 2023 (for Model BD-700-1A10 airplanes);
Bombardier Global 5000, BD-700 Temporary Revision 5-2-21,
dated March 31, 2023 (for Model BD-700-1A11 airplanes);
Bombardier Global 5000 GL 5000 Featuring Global Vision
Flight Deck Temporary Revision 5-2-20, dated March 31, 2023 (for Model
BD-700-1A11 airplanes); and
[Bombardier] Global 5500 GL 5500 Temporary Revision, 5-2-
3, dated March 31, 2023 (for Model BD-700-1A11 airplanes).
This service information specifies airworthiness limitations for
certification maintenance requirements. These documents are distinct
since they apply to different airplane models and configurations.
This proposed AD would also require the following service
information which the Director of the Federal Register approved for
incorporation by reference as of July 29, 2021 (86 FR 33088, June 24,
2021).
Bombardier Service Bulletin 700-1A11-27-041, Revision 1,
dated December 7, 2020.
Bombardier Service Bulletin 700-27-083, Revision 1, dated
December 7, 2020.
Bombardier Service Bulletin 700-27-5012, Revision 1, dated
December 7, 2020.
Bombardier Service Bulletin 700-27-5503, Revision 1, dated
December 7, 2020.
Bombardier Service Bulletin 700-27-6012, Revision 1, dated
December 7, 2020.
Bombardier Service Bulletin 700-27-6503, Revision 1, dated
December 7, 2020.
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 Requirements of This NPRM

This proposed AD would retain certain requirements of AD 2021-10-
02. This proposed AD would remove airplanes from the applicability,
remove the reporting requirement, and provide credit for certain
actions. This proposed AD would also require revising the existing
maintenance or inspection program, as applicable, to incorporate a new
airworthiness limitation.
This proposed AD would require revisions to certain operator
maintenance documents to include new actions (e.g., inspections).
Compliance with these actions is required by 14 CFR 91.403(c). For
airplanes that have been previously modified, altered, or repaired in
the areas addressed by this proposed AD, the operator may not be able
to accomplish the actions described in the revisions. In this
situation, to comply with 14 CFR 91.403(c), the operator must request
approval for an alternative method of compliance according to paragraph
(l)(1) of this proposed AD.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 461 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
The FAA has determined that revising the maintenance or inspection
program takes an average of 90 work-hours per operator, although the
agency recognizes that this number may vary from operator to operator.
Since operators incorporate maintenance or inspection program changes
for their affected fleet(s), the FAA has determined that a per-operator
estimate is more accurate than a per-airplane estimate. Therefore, the
agency estimates the average total cost per operator to be $7,650 (90
work-hours x $85 per work-hour).
The FAA estimates the total cost per operator for the new proposed
actions to be $7,650 (90 work-hours x $85 per work-hour).

Estimated Costs for Required Actions

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Retained actions from AD 2021-10-02 22 work-hours x $85 per hour = $1,870 Up to $4 (for four cotter pins) * Up to $1,874 Up to $863,914

* Parts cost include replacement parts where necessary.

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 this on-condition action:

Estimated Costs of On-Condition Actions

Labor cost
Parts cost
Cost per product
5 work-hours x $85 per hour = $425 $271 (for four bearings)
$696

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:

a. Removing Airworthiness Directive 2021-10-02, Amendment 39-21535 (86
FR 33088, June 24, 2021); and

b. Adding the following new airworthiness directive: