Rule2025-19390
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
October 2, 2025
Effective
November 6, 2025
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 787-8, 787-9, and 787-10 airplanes. This AD was prompted by reports of corrosion on one or more of the eight lower fitting assemblies and adjacent lavatory components on certain lavatories. This AD requires a detailed inspection of the lower fitting assemblies and the centerline partition threshold of the lavatories for corrosion, recording on the modification record placard, and applicable on-condition actions. This AD also requires revising the existing maintenance program to incorporate a detailed inspection of the lavatory vertical side forward fittings for corrosion or damage. The FAA is issuing this AD to address the unsafe condition on these products.
Full Text
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<title>Federal Register, Volume 90 Issue 189 (Thursday, October 2, 2025)</title>
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[Federal Register Volume 90, Number 189 (Thursday, October 2, 2025)]
[Rules and Regulations]
[Pages 47532-47535]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2025-19390]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-0347; Project Identifier AD-2024-00441-T;
Amendment 39-23156; AD 2025-20-03]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain The Boeing Company Model 787-8, 787-9, and 787-10 airplanes.
This AD was prompted by reports of corrosion on one or more of the
eight lower fitting assemblies and adjacent lavatory components on
certain lavatories. This AD requires a detailed inspection of the lower
fitting assemblies and the centerline partition threshold of the
lavatories for corrosion, recording on the modification record placard,
and applicable on-condition actions. This AD also requires revising the
existing maintenance program to incorporate a detailed inspection of
the lavatory vertical side forward fittings for corrosion or damage.
The FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective November 6, 2025.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of November 6,
2025.
ADDRESSES:
AD Docket: You may examine the AD docket at <a href="http://regulations.gov">regulations.gov</a> under
Docket No. FAA-2025-0347; 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 final rule, any comments received, and other
information. The address for Docket Operations is U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
<bullet> For the 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 <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 St., 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> under
Docket No. FAA-2025-0347.
FOR FURTHER INFORMATION CONTACT: Nicole S. Tsang, Aviation Safety
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 206-
231-3959; email: <a href="/cdn-cgi/l/email-protection#733d1a101c1f165d205d2700121d14331512125d141c05"><span class="__cf_email__" data-cfemail="88c6e1ebe7e4eda6dba6dcfbe9e6efc8eee9e9a6efe7fe">[email protected]</span></a>.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain The Boeing
Company Model 787-8, 787-9, and 787-10 airplanes. The NPRM was
published in the Federal Register on April 7, 2025 (90 FR 14927). The
NPRM was prompted by reports of corrosion on one or more of the eight
lower fitting assemblies and adjacent lavatory components on certain
lavatories. In the NPRM, the FAA proposed to require a detailed
inspection of the lower fitting assemblies and the centerline partition
threshold of the lavatories for corrosion, recording on the
modification record placard, and applicable on-condition actions. The
FAA also proposed to require revising the existing maintenance program
to incorporate a detailed inspection of the lavatory vertical side
forward fittings for corrosion or damage. The FAA is issuing this AD to
address the unsafe condition on these products.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from ProTech Aero Services Limited who
supported the NPRM without change.
The FAA received additional comments from five commenters,
including All Nippon Airways (All Nippon), American Airlines
(American), Boeing, and an anonymous commenter. The following presents
the comments received on the NPRM and the FAA's response to each
comment.
Request To Exclude Certain Airplanes From the Applicability
American requested that the FAA revise the applicability of the
proposed AD to exclude Model 787-8, 787-9, and 787-10 airplanes that
have never been equipped with Jamco family 95/96 lavatories. American
noted Boeing Special Attention Requirements Bulletin B787-81205-
SB250302-00 RB, Issue 001, dated August 21, 2024, identifies airplanes
that were delivered with and without the Jamco family 95/96 lavatories
and airplanes known to have been modified to be equipped with the
affected lavatories. American also noted the requirements bulletin
includes conditions to account for airplanes that may have been
modified to either remove or install the affected lavatories. Based on
this, American concluded the proposed AD is only applicable to
airplanes that have, or have had, Jamco family 95/96 lavatories
installed, and airplanes that have never had the affected lavatories
installed are exempted from the inspections specified in the proposed
AD.
The FAA agrees to exclude airplanes that were neither delivered
with the affected lavatories, nor equipped with the affected lavatories
after delivery. These airplanes are identified as Group 3,
Configuration 1, and Group 4, Configuration 3 airplanes in table 1 of
the requirements bulletin, and no actions are required for those
airplanes. The FAA has revised paragraph (c) of this AD accordingly.
Request To Extend the Inspection Compliance Time
United requested that the FAA extend the compliance time for the
inspection by 3 months. United stated that the proposed compliance time
does not allow it to schedule the inspection for all of its affected
airplanes during base maintenance visits, which would force some of its
airplanes out of service.
The FAA disagrees with commenter's request. The FAA assessed the
risk and determined that the inspection
[[Page 47533]]
compliance times specified in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin B787-81205-SB250302-00 RB,
Issue 001, dated August 21, 2024, are appropriate to mitigate the risk.
The FAA considered the safety implications and normal maintenance
schedules when establishing compliance times that adequately address
the unsafe condition of this AD. However, under the provisions of
paragraph (k) of this AD, the FAA will consider requests for approval
of an extension of the compliance time if sufficient data are submitted
to substantiate that the new compliance time would provide an
acceptable level of safety. The FAA has not changed the AD in this
regard.
Request To Coordinate Inspection Intervals With Operators
A commenter requested that the FAA closely coordinate with
operators to carefully define the inspection intervals to ensure
operators can achieve compliance with minimal possible operational
disruption.
The FAA acknowledges the commenter's request but has not revised
the AD in this regard for the same reasons noted in the FAA's response
to the previous comment.
Request To Revise Compliance Time for Placard Recording and Maintenance
Plan Revision
Boeing requested the FAA add a note to paragraph (g) of the
proposed AD to allow accomplishing the placard recording (condition 1,
action 1 and condition 2, action 2) and maintenance plan revision
(condition 1, action 2 and condition 2, action 3) within 38 months
after completing the initial inspection. Boeing noted that Boeing
Special Attention Requirements Bulletin B787-81205-SB250302-00 RB,
Issue 001, dated August 21, 2024, specifies those actions should be
completed before further flight after the inspection. Boeing, however,
asserted those actions are not critical to flight safety and should not
be required to be done before further flight for an airplane to return
to service. Boeing stated it has no plans to revise the requirements
bulletin to account for this.
The FAA partially agrees with the commenter's request. The FAA
agrees that the placard recording and maintenance plan revision are
administrative changes that are not critical to flight safety. However,
the FAA disagrees with extending the compliance time to 38 months after
accomplishing the inspection. The FAA has determined that extending the
compliance time to 90 days after accomplishing the inspection or repair
instructions, as applicable, is an appropriate time for accomplishing
the administrative actions. Accordingly, the FAA has added a new
exception to paragraph (h)(2) of this AD.
Request To Reference Interim Actions
All Nippon requested that the FAA revise the proposed AD to
reference any interim action, such as a service bulletin or other
relevant measure, if one is issued before the proposed AD is finalized.
The FAA acknowledges the commenter's request, but no change is
necessary to the AD in this regard. The FAA has determined no later
service information or any other measure that would affect AD
compliance has been issued in the interim. The FAA has not changed the
AD in this regard.
Request for an Alternative Method of Compliance (AMOC)
Boeing requested that the FAA revise the proposed AD to allow
accomplishment of the inspection in accordance with maintenance review
board report (MRBR) Item Number 25-185-00 for lavatories with no
previous repairs as an AMOC to accomplishing the inspection in
accordance with paragraph 3.A., step (3) of the Accomplishment
Instructions of Jamco Service Bulletin B80-25-4112, Revision 2, dated
April 24, 2024. Boeing stated that the inspections in the Jamco service
bulletin and MRBR item are identical, and that some operators
accomplished the inspections in accordance with the MRBR item prior to
the service bulletin release, and those operators would like to receive
credit.
The FAA partially agrees. The FAA disagrees with adding an AMOC to
this AD but agrees that an inspection accomplished before the effective
date of this AD using MRBR Item Number 25-185-00 for lavatories with no
previous repairs is acceptable for compliance with the inspection
required by paragraph (g) of this AD. Accordingly, the FAA has added a
new paragraph (j) to this AD allowing credit. The FAA notes that
operators may apply for an AMOC in accordance with the provisions in
paragraph (k) of this AD to use MRBR Item Number 25-185-00 as a method
of compliance after the effective date of this AD.
Request To Revise an Exception to the Requirements Bulletin
Boeing requested that the FAA revise paragraph (h)(2) of the
proposed AD to state, where Boeing Special Attention Requirements
Bulletin B787-81205-SB250302-00 RB, Issue 001, dated August 21, 2024,
specifies contacting Boeing for repair instructions, and if those
instructions include a modification to the maintenance actions or
intervals specified in section (g) of the proposed AD, then the
proposed AD requires doing the repair using a method approved in
accordance with the procedures specified in paragraph (j) of the
proposed AD. Boeing stated repairs that do not change the inspection
method or interval specified in the requirements bulletin comply with
the proposed AD.
The FAA disagrees with Boeing's request. The exception in paragraph
(h)(3) of this AD (corresponding to paragraph (h)(2) of the proposed
AD) is intended to require an AMOC anytime a manufacturer needs to be
contacted for repair instructions. Adopting the requested wording would
allow operators to circumvent the procedures in 14 CFR 39.19, as
specified in paragraph (k) of this AD. Since the requirements bulletin
does not provide repair instructions or point to another source for
repair instructions, such as an aircraft maintenance manual (AMM), an
operator will need to contact Boeing if corrosion is found, and that
should be done according to the procedures in paragraph (k) of this AD
to ensure the FAA has awareness of all repair instructions. If certain
corrosion findings can be corrected using existing procedures like an
AMM task, then this can be addressed with a revision to the service
information. If alternative repair instructions that go beyond what is
specified in the current service information are needed to address the
unsafe condition, and those repairs involve changing the inspection
method or interval, then the service information can be revised to
specify contacting Boeing for repair instructions for that situation.
The FAA has not revised the AD in this regard.
Request To Clarify Inspection Procedures for Previously Repaired
Fittings
Boeing requested the FAA add a new exception to paragraph (h) of
the proposed AD to clarify that the detailed inspection in paragraph
3.A, step (4) of Jamco Service Bulletin B80-25-4112, Revision 2, dated
April 24, 2024, is required for Jamco lavatories with basic part number
(P/N) B80095( ) or B80096( ) on which a previous repair has been
completed on a lavatory fitting. Boeing stated that Boeing Service
bulletin B787-81205-SB250302-00 only points to paragraph 3.A, step (3)
of the Jamco service bulletin as a method of compliance for the
detailed inspection, but that step is only
[[Page 47534]]
applicable to lavatories with no previous repairs of lavatory fittings.
Boeing also stated it has no plans to revise the corresponding service
bulletin to account for this.
The FAA partially agrees. The FAA agrees that paragraph 3.A., step
(4) of the Jamco service bulletin is applicable to lavatories with a
previous repair of a lavatory fitting with a doubler that covers the
bottom of the fitting and extends below the access hole. These lavatory
fittings have an additional step (4) for accessing the bottom of the
fitting to do the detailed inspection because the doubler may hide
corrosion. However, the FAA disagrees that paragraph 3.A., step (3) of
the Jamco service bulletin is only applicable to lavatories with no
previous repairs of lavatory fittings. Step (3) of the Jamco service
bulletin is applicable to all lavatories with P/N B80095( ) or B80096(
) because step (3) provides details on how to inspect the visible
surfaces for corrosion. The FAA has added a new exception in paragraph
(h)(4) of this AD to clarify that the detailed inspection must be
accomplished using step (3) and step (4), as applicable.
Conclusion
The FAA reviewed the relevant data, considered any comments
received, and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these products. Except for minor editorial changes, and
any other changes described previously, this AD is adopted as proposed
in the NPRM. None of the changes will increase the economic burden on
any operator.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed Boeing Special Attention Requirements Bulletin
B787-81205-SB250302-00 RB, Issue 001, dated August 21, 2024. This
material specifies procedures for a detailed inspection of the eight
lower fitting assemblies and the centerline partition threshold of the
Jamco family 95/96 lavatories for corrosion, recording on the
modification record placard, and applicable on-condition actions. On
condition actions include repairing any corrosion found. This material
also specifies revising the existing maintenance program to incorporate
MRBR item number 25-185-00 (detailed inspection of the lavatory
vertical side forward fittings for corrosion or damage).
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.
Costs of Compliance
The FAA estimates that this AD affects 159 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost per product operators
----------------------------------------------------------------------------------------------------------------
Inspection and placard recording 15 work-hours x $3,700 per $4,975 per Up to $4,746,150
$85 per hour = lavatory. lavatory. (up to 6
$1,275 per lavatories per
lavatory. airplane).
----------------------------------------------------------------------------------------------------------------
The FAA has determined that revising the existing maintenance
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 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 FAA
estimates the average total cost per operator to be $7,650 (90 work-
hours x $85 per work-hour).
The FAA has received no definitive data on which to base the cost
estimates for the on-condition repairs specified in this AD.
The FAA has included all known costs in its cost estimate.
According to the parts manufacturer, however, some or all of the costs
of this 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
This AD will not have federalism implications under Executive Order
13132. This AD will 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 that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will 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 Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 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 adding the following new airworthiness
directive:
[[Page 47535]]
2025-20-03 The Boeing Company: Amendment 39-23156; Docket No. FAA-
2025-0347; Project Identifier AD-2024-00441-T.
(a) Effective Date
This airworthiness directive (AD) is effective November 6, 2025.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company Model 787-8, 787-9, and
787-10 airplanes, certificated in any category, as identified in
Boeing Special Attention Requirements Bulletin B787-81205-SB250302-
00 RB, Issue 001, dated August 21, 2024, except for airplanes
identified as Group 3, Configuration 1; and Group 4, Configuration 3
airplanes.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Unsafe Condition
This AD was prompted by reports of corrosion on one or more of
the eight lower fitting assemblies and adjacent lavatory components
on the Jamco family 95/96 lavatories. The FAA is issuing this AD to
address corrosion that could cause the lavatories to break free from
the lower mounts during an event with high g-forces. The unsafe
condition, if not addressed, could result in potential serious
injury to passengers and crew or a displaced lavatory blockage that
prevents egress through the aisle and exits.
(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
Special Attention Requirements Bulletin B787-81205-SB250302-00 RB,
Issue 001, dated August 21, 2024, do all applicable actions
identified in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Requirements Bulletin B787-
81205-SB250302-00 RB, Issue 001, dated August 21, 2024.
Note 1 to paragraph (g): Guidance for accomplishing the actions
required by this AD can be found in Boeing Special Attention Service
Bulletin B787-81205-SB250302-00, Issue 001, dated August 21, 2024,
which is referred to in Boeing Special Attention Requirements
Bulletin B787-81205-SB250302-00 RB, Issue 001, dated August 21,
2024.
(h) Exceptions to Requirements Bulletin Specifications
(1) Where the ``Effectivity'' paragraph and the Boeing
Recommended Compliance Time columns of the tables in the
``Compliance'' paragraph of Boeing Special Attention Requirements
Bulletin B787-81205-SB250302-00 RB, Issue 001, dated August 21,
2024, refer to the Issue 001 date of Requirements Bulletin B787-
81205-SB250302-00 RB, this AD requires using the effective date of
this AD.
(2) Where the Boeing Recommended Compliance Time columns of the
tables in the ``Compliance'' paragraph of Boeing Special Attention
Requirements Bulletin B787-81205-SB250302-00 RB, Issue 001, dated
August 21, 2024, for Condition 1, Action 1 and Action 2; and
Condition 2, Action 2 and Action 3, specify modifying the record
placard and incorporating Maintenance Review Board Report (MRBR)
Item Number 25-185-00 ``Before further flight'', this AD requires
replacing that text with ``Within 90 days''.
(3) Where Boeing Special Attention Requirements Bulletin B787-
81205-SB250302-00 RB, Issue 001, dated August 21, 2024, specifies
contacting Boeing for repair instructions, this AD requires doing
the repair using a method approved in accordance with the procedures
specified in paragraph (k) of this AD.
(4) Where the Method of Compliance columns in the
``Accomplishment Instructions'' paragraph of Boeing Special
Attention Requirements Bulletin B787-81205-SB250302-00 RB, Issue
001, dated August 21, 2024, specifies doing a detailed inspection
using ``Paragraph 3.A. step (3)'', this AD requires replacing that
text with ``Paragraph 3.A. step (3) and step (4), as applicable''.
(i) No Alternative Actions and Intervals
After the existing maintenance program has been revised as
required by paragraph (g) of this AD, no alternative actions (e.g.,
inspections) or intervals may be used unless the actions or
intervals are approved as an alternative method of compliance (AMOC)
in accordance with the procedures specified in paragraph (k) of this
AD.
(j) Credit for Previous Inspections
For airplane lavatories with no previous repairs on which MRBR
Item Number 25-185-00 was accomplished before the effective date of
this AD, the inspection required by paragraph (g) of this AD is not
required.
(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)(1) of this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#b6f7fbf9f5f6d0d7d798d1d9c0"><span class="__cf_email__" data-cfemail="f8b9b5b7bbb89e9999d69f978e">[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.
(l) Related Information
(1) For more information about this AD, contact Nicole S. Tsang,
Aviation Safety Engineer, FAA, 2200 South 216th St., Des Moines, WA
98198; phone: 206-231-3959; email: <a href="/cdn-cgi/l/email-protection#17597e74787b7239443943647679705771767639707861"><span class="__cf_email__" data-cfemail="9ed0f7fdf1f2fbb0cdb0caedfff0f9def8ffffb0f9f1e8">[email protected]</span></a>.
(2) Material identified in this AD that is not incorporated by
reference is available at the address specified in paragraph (m)(3)
this AD.
(m) 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 the AD specifies otherwise.
(i) Boeing Special Attention Requirements Bulletin B787-81205-
SB250302-00 RB, Issue 001, dated August 21, 2024.
(ii) [Reserved]
(3) For the 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 <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 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 <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#d7b1a5f9beb9a4a7b2b4a3beb8b997b9b6a5b6f9b0b8a1"><span class="__cf_email__" data-cfemail="0f697d2166617c7f6a6c7b6660614f616e7d6e21686079">[email protected]</span></a>.
Issued on September 23, 2025.
Peter A. White,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2025-19390 Filed 10-1-25; 8:45 am]
BILLING CODE 4910-13-P
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