Proposed Rule2024-20160
Airworthiness Directives; The Boeing Company Airplanes
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
September 9, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA proposes to supersede Airworthiness Directive (AD) 2019-14-13, which applies to all The Boeing Company Model 767-200, - 300, -300F, and -400ER series airplanes. AD 2019-14-13 was prompted by reports of uncommanded fore and aft movement of the Captain's and First Officer's seats. AD 2019-14-13 requires identifying the part number, and the serial number if applicable, of the Captain's and First Officer's seats, and applicable on-condition actions for affected seats. AD 2019-14-13 also requires a one-time detailed inspection and repetitive checks of the horizontal movement system (HMS) of the Captain's and First Officer's seats, and applicable on-condition actions. AD 2019-14-13 also provides an optional terminating action for the repetitive actions for certain seats. Since the FAA issued AD 2019- 14-13, the FAA has determined that additional seats are affected by the unsafe condition. This proposed AD would retain the actions required by AD 2019-14-13 and adds an inspection of previously omitted part numbers. The FAA is proposing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 89 Issue 174 (Monday, September 9, 2024)</title>
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[Federal Register Volume 89, Number 174 (Monday, September 9, 2024)]
[Proposed Rules]
[Pages 73003-73009]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2024-20160]
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Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
========================================================================
Federal Register / Vol. 89, No. 174 / Monday, September 9, 2024 /
Proposed Rules
[[Page 73003]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2024-2136; Project Identifier AD-2023-00296-T]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD)
2019-14-13, which applies to all The Boeing Company Model 767-200, -
300, -300F, and -400ER series airplanes. AD 2019-14-13 was prompted by
reports of uncommanded fore and aft movement of the Captain's and First
Officer's seats. AD 2019-14-13 requires identifying the part number,
and the serial number if applicable, of the Captain's and First
Officer's seats, and applicable on-condition actions for affected
seats. AD 2019-14-13 also requires a one-time detailed inspection and
repetitive checks of the horizontal movement system (HMS) of the
Captain's and First Officer's seats, and applicable on-condition
actions. AD 2019-14-13 also provides an optional terminating action for
the repetitive actions for certain seats. Since the FAA issued AD 2019-
14-13, the FAA has determined that additional seats are affected by the
unsafe condition. This proposed AD would retain the actions required by
AD 2019-14-13 and adds an inspection of previously omitted part
numbers. 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 October 24,
2024.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
<bullet> Federal eRulemaking Portal: Go to <a href="http://regulations.gov">regulations.gov</a>. Follow
the instructions for submitting comments.
<bullet> Fax: 202-493-2251.
<bullet> 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.
<bullet> 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 <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2024-2136; 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, any comments received, and other
information. The street address for Docket Operations is listed above.
Material Incorporated by Reference:
<bullet> For Boeing material identified in this proposed AD,
contact Boeing Commercial Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Boulevard, MC 110-SK57, Seal Beach,
CA 90740-5600; phone 562-797-1717; website <a href="http://myboeingfleet.com">myboeingfleet.com</a>.
<bullet> You may view this material at the FAA, Airworthiness
Products Section, Operational Safety Branch, 2200 South 216th Street,
Des Moines, WA. For information on the availability of this material at
the FAA, call 206-231-3195. It is also available at <a href="http://regulations.gov">regulations.gov</a> by
searching for and locating Docket No. FAA-2024-2136.
FOR FURTHER INFORMATION CONTACT: Courtney Tuck, Aviation Safety
Engineer, FAA, 2200 South 216th Street, Des Moines, WA 98198; phone
206-231-3986; email <a href="/cdn-cgi/l/email-protection#6f2c001a1d1b010a164124413b1a0c042f090e0e41080019"><span class="__cf_email__" data-cfemail="abe8c4ded9dfc5ced285e085ffdec8c0ebcdcaca85ccc4dd">[email protected]</span></a>.
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-2024-2136; Project Identifier
AD-2023-00296-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
<a href="http://regulations.gov">regulations.gov</a>, 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
Courtney Tuck, Aviation Safety Engineer, FAA, 2200 South 216th Street,
Des Moines, WA 98198; phone 206-231-3986; email
<a href="/cdn-cgi/l/email-protection#cc8fa3b9beb8a2a9b5e287e298b9afa78caaadade2aba3ba"><span class="__cf_email__" data-cfemail="e5a68a9097918b809ccbaecbb190868ea5838484cb828a93">[email protected]</span></a>. 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 2019-14-13, Amendment 39-19691 (84 FR 38855,
August 8, 2019) (AD 2019-14-13), for all The Boeing Company Model 767-
200, -300, -300F, and -400ER series airplanes. AD 2019-14-13 was
prompted by reports of uncommanded fore and aft movement of the
Captain's and First Officer's seats. AD 2019-14-13 requires an
identification of the part number, and if applicable the serial number,
of the Captain's and First Officer's seats, and applicable on-condition
actions. AD 2019-14-13 also requires a one-time detailed inspection and
repetitive checks of the HMS of the
[[Page 73004]]
Captain's and First Officer's seats, and applicable on-condition
actions. AD 2019-14-13 also provides an optional terminating action for
the repetitive checks of the HMS for certain airplanes. The FAA issued
AD 2019-14-13 to address uncommanded fore and aft movement of the
Captain's and First Officer's seats. An uncommanded fore or aft seat
movement during a critical part of a flight, such as takeoff or
landing, could cause a flight control obstruction or unintended flight
control input, which could result in the loss of the ability to control
the airplane.
Actions Since AD 2019-14-13 Was Issued
Since the FAA issued AD 2019-14-13, Boeing and the seat supplier
(Ipeco) determined that certain seat part numbers were inadvertently
omitted from the service information required by AD 2019-14-13. Ipeco
subsequently updated their service information to include the
additional part numbers, and Boeing updated their service information
as well. Based on this, the FAA has determined that additional seats
are affected by the unsafe condition.
FAA's Determination
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.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed Boeing Special Attention Service Bulletin 767-25-
0539, Revision 2, dated January 27, 2023. This material describes
procedures for identification of the part number, and the serial number
if applicable, of the Captain's and First Officer's seats, and
applicable on-condition actions. On-condition actions include an
inspection of each seat's fore and aft and vertical manual control
levers for looseness, installation of serviceable seats, and a seat
operational test after any cable adjustment. This material also adds
Ipeco seat part numbers 3A258-0007-01-1Z, 3A258-0008-01-1Z, 3A258-0041-
01-1Z, 3A258-0042-01-1Z, and 3A090-0078-04-1. This material also adds
Ipeco seat part numbers 3A090-0078-03-1 and 3A090-0078-05-1, that were
previously removed in Boeing Special Attention Service Bulletin 767-25-
0539, Revision 1, dated January 9, 2014.
The FAA also reviewed Boeing Special Attention Service Bulletin
767-25-0549, Revision 2, dated January 27, 2023. This material
describes procedures for a detailed inspection and repetitive checks of
the HMS (including for any Artus part and amendment numbers of the
horizontal actuator of the HMS) for the Captain's and First Officer's
seats for findings (e.g., evidence of cracks, scores, corrosion, dents,
deformation, or visible wear; and incorrectly assembled microswitch
assemblies, actuators, and limit switches), and applicable on-condition
actions. The on-condition actions include clearing the seat tracks of
foreign object debris (FOD), overhauling the HMS, and replacing the
horizontal actuator. The material also describes procedures for an
optional terminating action for the repetitive checks by installing a
serviceable Captain's or First Officer's seat. The service information
adds Ipeco seat part number 3A090-0078-03-1, 3A090-0078-04-1, and
3A090-0078-05-1.
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 ADDRESSES section.
Proposed AD Requirements in This NPRM
Although this proposed AD does not explicitly restate the
requirements of AD 2019-14-13, this proposed AD would retain all of the
requirements of AD 2019-14-13. Those requirements are referenced in the
service information identified previously, which, in turn, is
referenced in paragraphs (g) and (h) of this proposed AD.
This proposed AD would require accomplishing the actions specified
in the service information already described, except for any
differences identified as exceptions in the regulatory text of this
proposed AD. For information on the procedures and compliance times,
see this service information at <a href="http://regulations.gov">regulations.gov</a> under Docket No. FAA-
2024-2136.
Acceptable Methods of Compliance
The FAA has determined that the actions required by paragraphs (g)
and (h) of this AD are not required, under specific conditions, e.g.,
if it can be shown through maintenance records that the required
actions have already been accomplished by the previous revision of the
service information and specific conditions have been met. Paragraph
(j) of this AD identifies these conditions. Complying with these
conditions adequately addresses the unsafe condition identified in this
proposed AD.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 694 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions per Seat
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost per product operators
----------------------------------------------------------------------------------------------------------------
Identification, seat (retained 1 work-hour x $85 $0 $85................ $117,980.
actions from AD 2019-14-13). per hour = $85.
Detailed inspection, HMS 1 work-hour x $85 $0 $85................ Up to $117,980.
(retained actions from AD 2019- per hour = $85.
14-13).
Checks, HMS (retained from AD 2 work-hours x $85 0 $170, per check Up to $235,960, per
2019-14-13). per hour = $170, cycle. check cycle.
per check cycle.
Identification, seat (new 1 work-hour x $85 0 $85................ Up to $117,980.
proposed actions). per hour = $85.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary on-
condition actions that will be required. The FAA has no way of
determining the number of aircraft that might need these on-condition
actions:
[[Page 73005]]
Estimated Costs of On-Condition Actions *
----------------------------------------------------------------------------------------------------------------
Action Labor cost Parts cost Cost per product
----------------------------------------------------------------------------------------------------------------
Adjustment, control lever cable...... 1 work-hour x $85 per $0..................... $85.
hour = $85.
Overhaul, HMS........................ 11 work-hours x $85 per Up to $5,824........... Up to $6,759.
hour = $935.
Inspection of each seat's fore/aft 1 work-hour x $85 per $0..................... $85 per seat.
and vertical manual control levers. hour = $85 per seat.
Installation of serviceable seats.... 1 work-hour x $85 per $0..................... $85 per seat.
hour = $85 per seat.
Clearing FOD......................... 1 work-hour x $85 per $0..................... $85 per seat.
hour = $85 per seat.
Replacement of the horizontal 1 work-hour x $85 per $7,937 per actuator.... $8,022 per actuator.
actuator. hour = $85 per
actuator.
Operational test, adjusted control 1 work-hour x $85 per $0..................... $85 per seat.
lever cable. hour = $85 per seat.
----------------------------------------------------------------------------------------------------------------
* The estimated cost for tooling to align an affected seat for adjustment of the control lever cable is up to
$46,064.
The FAA has received no definitive data that would enable the FAA
to provide cost estimates for the optional terminating action for the
repetitive checks specified in this proposed AD.
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
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 [Amended]
0
2. The FAA amends Sec. 39.13 by:
0
a. Removing Airworthiness Directive 2019-14-13, Amendment 39-19691 (84
FR 38855, August 8, 2019), and
0
b. Adding the following new Airworthiness Directive:
The Boeing Company: Docket No. FAA-2024-2136; Project Identifier AD-
2023-00296-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by October 24, 2024.
(b) Affected ADs
This AD replaces AD 2019-14-13, Amendment 39-19691 (84 FR 38855,
August 8, 2019) (AD 2019-14-13).
(c) Applicability
(1) This AD applies to all The Boeing Company Model 767-200, -
300, -300F, and -400ER series airplanes, certificated in any
category.
(2) Installation of Supplemental Type Certificate (STC)
ST01920SE does not affect the ability to accomplish the actions
required by this AD. Therefore, for airplanes on which STC ST01920SE
is installed, a ``change in product'' alternative method of
compliance (AMOC) approval request is not necessary to comply with
the requirements of 14 CFR 39.17.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Unsafe Condition
This AD was prompted by reports of uncommanded fore and aft
movement of the Captain's and First Officer's seats. The FAA is
issuing this AD to address uncommanded fore and aft movement of the
Captain's and First Officer's seats. The unsafe condition, if not
addressed, could result in an uncommanded fore or aft seat movement
during a critical part of a flight, such as takeoff or landing, and
could cause a flight control obstruction or unintended flight
control input, which could result in the loss of the ability to
control the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Seat Part Number Identification and On-Condition Actions
Except as specified in paragraphs (i) and (j) of this AD: At the
applicable time specified in the ``Compliance,'' paragraph of Boeing
Special Attention Service Bulletin 767-25-0539, Revision 2, dated
January 27, 2023, do an inspection to determine the part number, and
serial number as applicable, of the Captain's and First Officer's
seats, and all applicable on-condition actions, in accordance with
the Accomplishment Instructions of Boeing Special Attention Service
Bulletin 767-25-0539, Revision 2, dated January 27, 2023. A review
of airplane maintenance records is acceptable in lieu of this
inspection if the part number and serial number of the Captain's and
First Officer's seats can be conclusively determined from that
review.
[[Page 73006]]
(h) Detailed Inspection, and Repetitive Checks of Horizontal Movement
System and On-Condition Actions
Except as specified by paragraphs (i) and (j) of this AD: At the
applicable times specified in the ``Compliance,'' paragraph of
Boeing Special Attention Bulletin 767-25-0549, Revision 2, dated
January 27, 2023, do all applicable actions identified as ``RC''
(required for compliance) in, and in accordance with, the
Accomplishment Instructions of Boeing Special Attention Bulletin
767-25-0549, Revision 2, dated January 27, 2023. Actions identified
as terminating action in Boeing Special Attention Bulletin 767-25-
0549, Revision 2, dated January 27, 2023, terminate the applicable
required actions of this AD, provided the terminating action is done
in accordance with the Accomplishment Instructions of Boeing Special
Attention Service Bulletin 767-25-0549, Revision 2, dated January
27, 2023.
(i) Exceptions to Service Information Specifications
(1) Where the ``Compliance'' paragraph of Boeing Special
Attention Bulletin 767-25-0549, Revision 2, dated January 27, 2023,
refers to the original issue date of the service bulletin, this AD
requires using September 12, 2019 (the effective date of AD 2019-14-
13).
(2) Where the ``Compliance'' paragraph of Boeing Special
Attention Bulletin 767-25-0549, Revision 2, dated January 27, 2023,
refers to the Revision 2 date of the service bulletin, this AD
requires using the effective date of this AD.
(3) Where the ``Compliance'' paragraph of Boeing Special
Attention Service Bulletin 767-25-0539, Revision 2, dated January
27, 2023, refers to within 72 months after the original issue date
of the service bulletin, this AD requires using within 36 months
after September 12, 2019 (the effective date of AD 2019-14-13).
(4) Where the ``Compliance'' paragraph of Boeing Special
Attention Bulletin 767-25-0539, Revision 2, dated January 27, 2023,
refers to the Revision 2 date of the service bulletin, this AD
requires using the effective date of this AD.
(j) Acceptable Conditions for Compliance
If the airplane records show that an Ipeco Captain's or First
Officer's seat meets all criteria specified in any row in figure 1
to paragraph (j) of this AD, the actions specified in paragraphs (g)
and (h) of this AD are not required for that seat.
Figure 1 to Paragraph (j)--Alternative Acceptable Seats
[[Page 73007]]
[GRAPHIC] [TIFF OMITTED] TP09SE24.004
[[Page 73008]]
[GRAPHIC] [TIFF OMITTED] TP09SE24.005
(k) 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 (l)
of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#d99894969a99bfb8b8f7beb6af"><span class="__cf_email__" data-cfemail="6524282a26250304044b020a13">[email protected]</span></a>.
(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.
(4) AMOCs approved for AD 2019-14-13 are approved as AMOCs for
the corresponding provisions of Boeing Special Attention Service
Bulletin 767-25-0539, Revision 2, dated January 27, 2023, and Boeing
Special Attention Service Bulletin 767-25-0549, Revision 2, dated
January 27, 2023, that are required by paragraphs (g) and (h) of
this AD.
(5) For service information that contains steps that are labeled
as Required for Compliance (RC), the provisions of paragraphs
(k)(5)(i) and (ii) of this AD apply.
(i) The steps labeled as RC, including substeps under an RC step
and any figures identified in an RC step, must be done to comply
with the AD. If a step or substep is labeled ``RC Exempt,'' then the
RC requirement is removed from that step or substep. An AMOC is
required for any deviations to RC steps, including substeps and
identified figures.
(ii) Steps not labeled as RC may be deviated from using accepted
methods in accordance with the operator's maintenance or inspection
program without obtaining approval of an AMOC, provided the RC
steps, including substeps and identified figures, can still be done
as specified, and the airplane can be put back in an airworthy
condition.
(l) Related Information
For more information about this AD, contact Courtney Tuck,
Aviation Safety Engineer, FAA, 2200 South 216th Street, Des
[[Page 73009]]
Moines, WA 98198; phone 206-231-3986; email <a href="/cdn-cgi/l/email-protection#33705c4641475d564a1d781d67465058735552521d545c45"><span class="__cf_email__" data-cfemail="397a564c4b4d575c401772176d4c5a52795f5858175e564f">[email protected]</span></a>.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register approved the
incorporation by reference (IBR) 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 the AD specifies otherwise.
(i) Boeing Special Attention Service Bulletin 767-25-0539,
Revision 2, dated January 27, 2023.
(ii) Boeing Special Attention Service Bulletin 767-25-0549,
Revision 2, dated January 27, 2023.
(3) For Boeing material identified in this AD, contact Boeing
Commercial Airplanes, Attention: Contractual & Data Services (C&DS),
2600 Westminster Boulevard, MC 110-SK57, Seal Beach, CA 90740-5600;
phone 562-797-1717; website <a href="http://myboeingfleet.com">myboeingfleet.com</a>.
(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 Administration (NARA). For information on the availability
of this material at NARA, visit <a href="http://www.archives.gov/federal-register/cfr/ibr-locations">www.archives.gov/federal-register/cfr/ibr-locations</a> or email <a href="/cdn-cgi/l/email-protection#9bfde9b5f2f5e8ebfef8eff2f4f5dbf5fae9fab5fcf4ed"><span class="__cf_email__" data-cfemail="7e180c5017100d0e1b1d0a1711103e101f0c1f50191108">[email protected]</span></a>.
Issued on August 26, 2024.
Suzanne Masterson,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2024-20160 Filed 9-6-24; 8:45 am]
BILLING CODE 4910-13-P
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