Airworthiness Directives; The Boeing Company Airplanes, 57377-57379 [2024-15308]
Download as PDF
Federal Register / Vol. 89, No. 135 / Monday, July 15, 2024 / Proposed Rules
and in accordance with, the Accomplishment
Instructions of Boeing Alert Requirements
Bulletin B787–81205–SB250299–00 RB, Issue
001, dated July 31, 2023.
Note 2 to paragraph (j): Guidance for
accomplishing the actions required by this
AD can be found in Boeing Alert Service
Bulletin B787–81205–SB250299–00, Issue
001, dated July 31, 2023, which is referred to
in Boeing Alert Requirements Bulletin B787–
81205–SB250299–00 RB, Issue 001, dated
July 31, 2023.
(k) New Exception to Service Information
Specifications
Where the Compliance Time columns of
the tables in the ‘‘Compliance’’ paragraph of
Boeing Alert Requirements Bulletin B787–
81205–SB250299–00 RB, Issue 001, dated
July 31, 2023, use the phrase ‘‘the Issue 001
date of Requirements Bulletin B787–81205–
SB250299–00 RB,’’ this AD requires using the
effective date of this AD.
(l) Terminating Action for Clamshell
Coupling Inspection
For the airplanes identified in Boeing Alert
Requirements Bulletin B787–81205–
SB250299–00 RB, Issue 001, dated July 31,
2023: Accomplishment of the actions
required by paragraph (j) of this AD
terminates the requirements of paragraph (g)
of this AD.
ddrumheller on DSK120RN23PROD with PROPOSALS1
(m) Parts Installation Prohibition
As of the effective date of this AD, no
person may install a clamshell coupling, part
number (P/N) 14C02–08C or P/N
AS1655A08, at inspection locations where P/
N 14C02–08C or P/N AS1655A08 was
replaced with P/N 14C34–08C or P/N 14C33–
08 on any airplane in accordance with
Boeing Alert Requirements Bulletin B787–
81205–SB250299–00 RB, Issue 001, dated
July 31, 2023.
(n) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, AIR–520, Continued
Operational Safety 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 the attention of the person
identified in paragraph (o)(1) of this AD.
Information may be emailed to: AMOC@
faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair,
modification, or alteration required by this
AD if it is approved by The Boeing Company
Organization Designation Authorization
(ODA) that has been authorized by the
Manager, AIR–520, Continued Operational
Safety Branch, FAA, to make those findings.
To be approved, the repair method,
modification deviation, or alteration
deviation must meet the certification basis of
VerDate Sep<11>2014
16:24 Jul 12, 2024
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57377
the airplane, and the approval must
specifically refer to this AD.
(4) AMOCs approved for AD 2023–08–04
are approved as AMOCs for the
corresponding provisions of Boeing Alert
Requirements Bulletin B787–81205–
SB380021–00 RB, Issue 001, dated August
12, 2022, that are required by paragraph (g)
of this AD.
DEPARTMENT OF TRANSPORTATION
(o) Related Information
Airworthiness Directives; The Boeing
Company Airplanes
(1) For more information about this AD,
contact Brandon Lucero, Aviation Safety
Engineer, FAA, 2200 South 216th St., Des
Moines, WA 98198; phone: 206–231–3569;
email: Brandon.Lucero@faa.gov.
(2) Material identified in this AD that is not
incorporated by reference is available at the
addresses specified in paragraph (p)(5) of this
AD.
(p) 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 material as
applicable to do the actions required by this
AD, unless this AD specifies otherwise.
(3) The following material was approved
for IBR on [DATE 35 DAYS AFTER
PUBLICATION OF THE FINAL RULE].
(i) Boeing Alert Requirements Bulletin
B787–81205–SB250299–00 RB, Issue 001,
dated July 31, 2023.
(ii) [Reserved]
(4) The following material was approved
for IBR on June 29, 2023 (88 FR 33823, May
25, 2023).
(i) Boeing Alert Requirements Bulletin
B787–81205–SB380021–00 RB, Issue 001,
dated August 12, 2022.
(ii) [Reserved]
(5) For Boeing material identified in this
AD, contact Boeing Commercial Airplanes,
Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC 110–
SK57, Seal Beach, CA 90740–5600; telephone
562–797–1717; website myboeingfleet.com.
(6) 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.
(7) You may view this material at the
National Archives and Records
Administration (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 July 2, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate
Management Division, Aircraft Certification
Service.
[FR Doc. 2024–15235 Filed 7–12–24; 8:45 am]
BILLING CODE 4910–13–P
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Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2024–1689; Project
Identifier AD–2024–00109–T]
RIN 2120–AA64
Federal Aviation
Administration (FAA), DOT.
ACTION: Proposed rule; correction.
AGENCY:
The FAA is correcting a
notice of proposed rulemaking (NPRM)
that was published in the Federal
Register. The NPRM proposed to issue
an airworthiness directive (AD) that
would apply to all The Boeing Company
Model 767–200, –300, and –300F series
airplanes. As published, the docket
number referenced throughout the
NPRM is incorrect. This document
corrects that error. In all other respects,
the original document remains the
same; however, for clarity, the FAA is
publishing the entire proposed rule in
the Federal Register.
DATES: The last date for submitting
comments on the NPRM (89 FR 51856,
June 20, 2024) remains August 5, 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–2024–1689; 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 ‘‘proposed rule;
correction,’’ 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 service information, contact
Boeing Commercial Airplanes,
Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC
SUMMARY:
E:\FR\FM\15JYP1.SGM
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57378
Federal Register / Vol. 89, No. 135 / Monday, July 15, 2024 / Proposed Rules
110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; website
myboeingfleet.com. It is also available at
regulations.gov under Docket No. FAA–
2024–1689.
FOR FURTHER INFORMATION CONTACT:
Stefanie Roesli, Aviation Safety
Engineer, FAA, 2200 South 216th St.,
Des Moines, WA 98198; phone: 206–
231–3964; email: Stefanie.N.Roesli@
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–2024–1689; Project
Identifier AD–2024–00109–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 this
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.
ddrumheller on DSK120RN23PROD with PROPOSALS1
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 Stefanie Roesli,
Aviation Safety Engineer, FAA, 2200
South 216th St., Des Moines, WA 98198;
phone: 206–231–3964; email:
Stefanie.N.Roesli@faa.gov. Any
commentary that the FAA receives that
VerDate Sep<11>2014
16:24 Jul 12, 2024
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is not specifically designated as CBI will
be placed in the public docket for this
rulemaking.
Background
The FAA issued an NPRM (89 FR
51856, June 20, 2024) that would apply
to all The Boeing Company Model 767–
200, –300, and –300F series airplanes.
The NPRM was prompted by a report of
a main landing gear (MLG) collapse
event following maintenance where a
grinder was operating outside of its
input parameters, resulting in possible
heat damage to the outer cylinder of the
MLG. The NPRM proposed to require
replacing any affected outer cylinders.
The FAA is proposing this AD to
address any heat damage to the outer
cylinder of the landing gear. The unsafe
condition, if not addressed, could result
in the inability of a principal structural
element to sustain limit load, gear
collapse resulting in loss of control and
potential for off runway excursion.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Boeing Alert
Requirements Bulletin 767–32A0253
RB, dated February 6, 2024. This service
information specifies procedures for
performing a check of maintenance
records or performing an inspection of
the left and right MLG outer cylinders
for any affected part numbers and serial
numbers and replacing affected
cylinders. 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
ADDRESSES.
Need for the Correction
As published, the docket number
referenced throughout the NPRM is
incorrect. The NPRM incorrectly
references ‘‘Docket No. FAA–2024–
1688.’’ The correct docket number is
‘‘Docket No. FAA–2024–1689.’’
Although no other part of the
preamble or regulatory information has
been corrected, for clarity the FAA is
publishing the entire proposed rule in
the Federal Register.
The comment due date of the NPRM
remains August 5, 2024.
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:
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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.
§ 39.13
[Corrected]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
The Boeing Company: Docket No. FAA–
2024–1689; Project Identifier AD–2024–
00109–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by August 5,
2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all The Boeing
Company Model 767–200, –300, and –300F
series airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of
America Code 32, Landing Gear.
(e) Unsafe Condition
This AD was prompted by a report of a
main landing gear (MLG) collapse event
following maintenance where a grinder was
operating outside of its input parameters,
resulting in possible heat damage to the outer
cylinder of the MLG. The FAA is issuing this
AD to address any heat damage to the outer
cylinder of the landing gear. The unsafe
condition, if not addressed, could result in
the inability of a principal structural element
to sustain limit load, gear collapse resulting
in loss of control and potential for off runway
excursion.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Except as specified by paragraph (h) of this
AD: At the applicable times specified in the
‘‘Compliance’’ paragraph of Boeing Alert
Requirements Bulletin 767–32A0253 RB,
dated February 6, 2024, do all applicable
actions identified in, and in accordance with,
the Accomplishment Instructions of Boeing
Alert Requirements Bulletin 767–32A0253
RB, dated February 6, 2024.
Note 1 to paragraph (g): Guidance for
accomplishing the actions required by this
AD can be found in Boeing Alert Service
Bulletin 767–32A0253, dated February 6,
2024, which is referred to in Boeing Alert
Requirements Bulletin 767–32A0253 RB,
dated February 6, 2024.
(h) Exceptions to Service Information
Specifications
Where the Boeing Recommended
Compliance Time column of the table in the
‘‘Compliance’’ paragraph of Boeing Alert
E:\FR\FM\15JYP1.SGM
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Federal Register / Vol. 89, No. 135 / Monday, July 15, 2024 / Proposed Rules
Requirements Bulletin 767–32A0253 RB,
dated February 6, 2024, uses the phrase ‘‘the
Original Issue date of Requirements Bulletin
767–32A0253 RB,’’ this AD requires using
the effective date of this AD.
(i) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, AIR–520, Continued
Operational Safety 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 the attention of the person
identified in paragraph (j)(1) of this AD.
Information may be emailed to: AMOC@
faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(3) An AMOC that provides an acceptable
level of safety may be used for any repair,
modification, or alteration required by this
AD if it is approved by The Boeing Company
Organization Designation Authorization
(ODA) that has been authorized by the
Manager, AIR–520, Continued Operational
Safety Branch, FAA, to make those findings.
To be approved, the repair method,
modification deviation, or alteration
deviation must meet the certification basis of
the airplane, and the approval must
specifically refer to this AD.
ddrumheller on DSK120RN23PROD with PROPOSALS1
(j) Related Information
(1) For more information about this AD,
contact Stefanie Roesli, Aviation Safety
Engineer, FAA, 2200 South 216th St., Des
Moines, WA 98198; phone: 206–231–3964;
email: Stefanie.N.Roesli@faa.gov.
(2) Service information identified in this
AD that is not incorporated by reference is
available at the addresses specified in
paragraphs (k)(3) and (4) of this AD.
(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 the AD specifies otherwise.
(i) Boeing Alert Requirements Bulletin
767–32A0253 RB, dated February 6, 2024.
(ii) [Reserved]
(3) For service information identified in
this AD, contact Boeing Commercial
Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Blvd.,
MC 110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; website
myboeingfleet.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
VerDate Sep<11>2014
16:24 Jul 12, 2024
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Administration (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 July 8, 2024.
Peter A. White,
Deputy Director, Integrated Certificate
Management Division, Aircraft Certification
Service.
[FR Doc. 2024–15308 Filed 7–12–24; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF HOMELAND
SECURITY
Coast Guard
33 CFR Part 117
[Docket No. USCG–2024–0379]
RIN 1625–AA09
Drawbridge Operation Regulation;
Miami River, North Fork, Miami, FL
Coast Guard, DHS.
Notice of proposed rulemaking.
AGENCY:
ACTION:
The Coast Guard proposes to
remove the operating schedule that
governs the FDOT Railroad Bridge,
across the Miami River, North Fork,
mile 5.3, at Miami, FL. The railroad
bridge is being replaced with a fixed
bridge. We invite your comments on
this proposed rulemaking.
DATES: Comments and related material
must reach the Coast Guard on or before
August 14, 2024.
ADDRESSES: You may submit comments
identified by docket number USCG–
2024–0379 using Federal Decision
Making Portal at https://
www.regulations.gov.
See the ‘‘Public Participation and
Request for Comments’’ portion of the
SUPPLEMENTARY INFORMATION section
below for instructions on submitting
comments. This notice of proposed
rulemaking with its plain-language, 100word-or-less proposed rule summary
will be available in this same docket.
FOR FURTHER INFORMATION CONTACT: If
you have questions on this proposed
rule, call or email Ms. Jennifer Zercher,
Bridge Management Specialist, Seventh
Coast Guard District; telephone 571–
607–5951, email Jennifer.N.Zercher@
uscg.mil.
SUMMARY:
SUPPLEMENTARY INFORMATION:
I. Table of Abbreviations
CFR Code of Federal Regulations
DHS Department of Homeland Security
FR Federal Register
OMB Office of Management and Budget
NPRM Notice of Proposed Rulemaking
(Advance, Supplemental)
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57379
§ Section
U.S.C. United States Code
FL Florida
FDOT Florida Department of
Transportation
II. Background, Purpose and Legal
Basis
The FDOT Railroad Bridge, across the
Miami River, North Fork, mile 5.3, at
Miami, FL, is a single bascule bridge
with a 6-foot vertical clearance at mean
high water in the closed position. The
normal operating schedule is set forth in
33 CFR 117.307.
FDOT applied for and received a
Coast Guard Bridge Permit to replace
the existing moveable railroad bridge
with a fixed railroad bridge. FDOT has
requested the drawbridge operation
regulation be removed and the bridge be
allowed to remain closed to navigation
in anticipation of phase one of the
bridge replacement project, converting
the moveable bridge to a fixed bridge,
beginning August 2024.
The Miami River, under the
jurisdiction of the U.S. Army Corps of
Engineers, is a federal navigation project
channel. On December 21, 2020, the
U.S. Congress approved the
deauthorization of navigational rights
for the portion of the Miami River
between the FDOT Railroad Bridge and
the S–26 SFWMD structure with the
Miami Rivel Canal provision of the
Consolidated Appropriations Act, 2021
(12/21/2020).
III. Discussion of Proposed Rule
Under this proposed rule, the FDOT
Railroad Bridge would be allowed to
remain closed to navigation until the
bridge replacement project is
completed. The waterway from the
railroad bridge to the water control
structure has been deauthorized of
navigational rights, therefore, impacts to
navigation are not expected. Vessels that
can pass beneath the bridge without an
opening would be able to so at any time.
IV. Regulatory Analyses
We developed this proposed rule after
considering numerous statutes and
Executive Orders related to rulemaking.
Below we summarize our analyses
based on these statutes and Executive
Orders.
A. Regulatory Planning and Review
Executive Orders 12866 and 13563
direct agencies to assess the costs and
benefits of available regulatory
alternatives and, if regulation is
necessary, to select regulatory
approaches that maximize net benefits.
This proposed rule has not been
designated a ‘‘significant regulatory
action,’’ under section 3(f) of Executive
E:\FR\FM\15JYP1.SGM
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Agencies
[Federal Register Volume 89, Number 135 (Monday, July 15, 2024)]
[Proposed Rules]
[Pages 57377-57379]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-15308]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-1689; Project Identifier AD-2024-00109-T]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Proposed rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting a notice of proposed rulemaking (NPRM)
that was published in the Federal Register. The NPRM proposed to issue
an airworthiness directive (AD) that would apply to all The Boeing
Company Model 767-200, -300, and -300F series airplanes. As published,
the docket number referenced throughout the NPRM is incorrect. This
document corrects that error. In all other respects, the original
document remains the same; however, for clarity, the FAA is publishing
the entire proposed rule in the Federal Register.
DATES: The last date for submitting comments on the NPRM (89 FR 51856,
June 20, 2024) remains August 5, 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-2024-1689; 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 ``proposed rule; correction,'' 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 service information, contact Boeing Commercial
Airplanes, Attention: Contractual & Data Services (C&DS), 2600
Westminster Blvd., MC
[[Page 57378]]
110-SK57, Seal Beach, CA 90740-5600; telephone 562-797-1717; website
myboeingfleet.com. It is also available at regulations.gov under Docket
No. FAA-2024-1689.
FOR FURTHER INFORMATION CONTACT: Stefanie Roesli, Aviation Safety
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-
231-3964; email: [email protected].
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-2024-1689;
Project Identifier AD-2024-00109-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 this 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
Stefanie Roesli, Aviation Safety Engineer, FAA, 2200 South 216th St.,
Des Moines, WA 98198; phone: 206-231-3964; email:
[email protected]. 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 an NPRM (89 FR 51856, June 20, 2024) that would
apply to all The Boeing Company Model 767-200, -300, and -300F series
airplanes. The NPRM was prompted by a report of a main landing gear
(MLG) collapse event following maintenance where a grinder was
operating outside of its input parameters, resulting in possible heat
damage to the outer cylinder of the MLG. The NPRM proposed to require
replacing any affected outer cylinders. The FAA is proposing this AD to
address any heat damage to the outer cylinder of the landing gear. The
unsafe condition, if not addressed, could result in the inability of a
principal structural element to sustain limit load, gear collapse
resulting in loss of control and potential for off runway excursion.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Boeing Alert Requirements Bulletin 767-32A0253 RB,
dated February 6, 2024. This service information specifies procedures
for performing a check of maintenance records or performing an
inspection of the left and right MLG outer cylinders for any affected
part numbers and serial numbers and replacing affected cylinders. 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 ADDRESSES.
Need for the Correction
As published, the docket number referenced throughout the NPRM is
incorrect. The NPRM incorrectly references ``Docket No. FAA-2024-
1688.'' The correct docket number is ``Docket No. FAA-2024-1689.''
Although no other part of the preamble or regulatory information
has been corrected, for clarity the FAA is publishing the entire
proposed rule in the Federal Register.
The comment due date of the NPRM remains August 5, 2024.
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
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Corrected]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
The Boeing Company: Docket No. FAA-2024-1689; Project Identifier AD-
2024-00109-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by August 5, 2024.
(b) Affected ADs
None.
(c) Applicability
This AD applies to all The Boeing Company Model 767-200, -300,
and -300F series airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 32, Landing
Gear.
(e) Unsafe Condition
This AD was prompted by a report of a main landing gear (MLG)
collapse event following maintenance where a grinder was operating
outside of its input parameters, resulting in possible heat damage
to the outer cylinder of the MLG. The FAA is issuing this AD to
address any heat damage to the outer cylinder of the landing gear.
The unsafe condition, if not addressed, could result in the
inability of a principal structural element to sustain limit load,
gear collapse resulting in loss of control and potential for off
runway excursion.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Except as specified by paragraph (h) of this AD: At the
applicable times specified in the ``Compliance'' paragraph of Boeing
Alert Requirements Bulletin 767-32A0253 RB, dated February 6, 2024,
do all applicable actions identified in, and in accordance with, the
Accomplishment Instructions of Boeing Alert Requirements Bulletin
767-32A0253 RB, dated February 6, 2024.
Note 1 to paragraph (g): Guidance for accomplishing the actions
required by this AD can be found in Boeing Alert Service Bulletin
767-32A0253, dated February 6, 2024, which is referred to in Boeing
Alert Requirements Bulletin 767-32A0253 RB, dated February 6, 2024.
(h) Exceptions to Service Information Specifications
Where the Boeing Recommended Compliance Time column of the table
in the ``Compliance'' paragraph of Boeing Alert
[[Page 57379]]
Requirements Bulletin 767-32A0253 RB, dated February 6, 2024, uses
the phrase ``the Original Issue date of Requirements Bulletin 767-
32A0253 RB,'' this AD requires using the effective date of this AD.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, AIR-520, Continued Operational Safety 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 the attention of the person identified in paragraph
(j)(1) of this AD. Information may be emailed to: [email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by The Boeing Company Organization Designation
Authorization (ODA) that has been authorized by the Manager, AIR-
520, Continued Operational Safety Branch, FAA, to make those
findings. To be approved, the repair method, modification deviation,
or alteration deviation must meet the certification basis of the
airplane, and the approval must specifically refer to this AD.
(j) Related Information
(1) For more information about this AD, contact Stefanie Roesli,
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA
98198; phone: 206-231-3964; email: [email protected].
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (4) of this AD.
(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 the AD specifies otherwise.
(i) Boeing Alert Requirements Bulletin 767-32A0253 RB, dated
February 6, 2024.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-
5600; telephone 562-797-1717; website myboeingfleet.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 Administration (NARA). For information on the availability
of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email [email protected].
Issued on July 8, 2024.
Peter A. White,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-15308 Filed 7-12-24; 8:45 am]
BILLING CODE 4910-13-P