Published 2025-12-12 · Federal Register document 2025-22629
Airworthiness Directives; The Boeing Company Airplanes
Publication summary
The FAA is superseding Airworthiness Directive (AD) 2023-09- 04, which applied to certain The Boeing Company Model 737-600, -700, - 700C, -800, -900, and -900ER series airplanes, and certain Model 737-8 and -9 airplanes. AD 2023-09-04 required inspecting all escape slide assemblies to identify affected parts and replacing affected escape slide assemblies with different assemblies. This AD was prompted by the determination that additional airplanes might be affected by the unsafe condition. This AD retains the requirements of AD 2023-09-04 and requires those actions for additional airplanes, including Model 737- 8200 airplanes. The FAA is issuing this AD to address the unsafe condition on these products.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:20.413248+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2025-67d39c2af9a91434
- Source row
- results[310]
- Raw source SHA-256
- 67d39c2af9a914349adee3ee1cee836da6415ed54d2b01123da75b563b687ab0
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2025-25-04
- Effective date printed in this edition
- 2026-01-16
Read 13 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective January 16, 2026.
Exact source excerpt. Text positions 12272–12362, end exclusive, in the original decoded publication. SHA-256: 976e7411032057302f3cd319a0c8d5ae1c8aa8eb70db92646d07251d0f07b771
Affected ADs
(b) Affected ADs
This AD replaces AD 2023-09-04, Amendment 39-22427 (88 FR 33817,
May 25, 2023) (AD 2023-09-04).
Exact source excerpt. Text positions 12362–12482, end exclusive, in the original decoded publication. SHA-256: 150a780f257bec1e6a2646a587c63202c30a8fb2330fb1f1d60a1694fee8074f
Applicability wording · Applicability
(c) Applicability
This AD applies to The Boeing Company Model 737-600, -700, -
700C, -800, -900, and -900ER series airplanes, and Model 737-8, 737-
9, and 737-8200 airplanes, certificated in any category.
Exact source excerpt. Text positions 12482–12693, end exclusive, in the original decoded publication. SHA-256: d5b324abb5af7794a68c16f67b750b69d25f151b3dab7f7d6e93789ebcc8d7a4
Subject
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
Exact source excerpt. Text positions 12693–12787, end exclusive, in the original decoded publication. SHA-256: cd842d64513c20d1d1bce522de9bad2824ec75abe7ad967bbaaaf7decc400437
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by reports of uncommanded escape slide
deployments in the passenger compartment, caused by too much tension
in the inflation cable and the movement of the escape slide assembly
in the escape slide compartment. The FAA is issuing this AD to
address inflation of the
[[Page 57687]]
escape slide while it is in the escape slide compartment, which
could result in injury to passengers and crew during normal
operation, or impede an emergency evacuation by rendering the exit
unusable.
Exact source excerpt. Text positions 12787–13325, end exclusive, in the original decoded publication. SHA-256: 5454dd9e9bd385aceb39c200d3db4f76f77c3721cae673e9011c18822efbc31f
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 13325–13427, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Retained Inspection, With No Changes
(g) Retained Inspection, With No Changes
This paragraph restates the requirements of paragraph (g) of AD
2023-09-04, with no changes. For airplanes identified in Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, Revision 1,
dated April 13, 2022; and Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 1, dated April 11, 2022: Except as
specified in paragraph (i) of this AD, at the applicable times
specified in the ``Compliance'' paragraph of Boeing Special
Attention Requirements Bulletin 737-25-1855 RB, Revision 1, dated
April 13, 2022; and Boeing Special Attention Requirements Bulletin
737-25-1866 RB, Revision 1, dated April 11, 2022, do all applicable
actions identified in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Requirements Bulletin 737-
25-1855 RB, Revision 1, dated April 13, 2022 (for Model 737-600, -
700, -700C, -800, -900, and -900ER series airplanes); and Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 1,
dated April 11, 2022 (for Model 737-8 and -9 airplanes); as
applicable.
Note 1 to paragraph (g): Guidance for accomplishing the actions
required by paragraph (g) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1855, Revision 1, dated April 13,
2022, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1855 RB, Revision 1, dated April 13, 2022.
Note 2 to paragraph (g): Guidance for accomplishing the actions
required by paragraph (g) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1866, Revision 1, dated April 11,
2022, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 1, dated April 11, 2022.
Exact source excerpt. Text positions 13427–15217, end exclusive, in the original decoded publication. SHA-256: 86e8db523f99616f963f1f9dd07520e5fa81baa00906e194a4eb141ea8624cc9
New Required Actions
(h) New Required Actions
For airplanes not identified in Boeing Special Attention
Requirements Bulletin 737-25-1855 RB, Revision 1, dated April 13,
2022; or Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 1, dated April 11, 2022: Except as specified in
paragraph (i) of this AD, at the applicable times specified in the
``Compliance'' paragraph of Boeing Special Attention Requirements
Bulletin 737-25-1855 RB, Revision 1, dated April 13, 2022; and
Boeing Special Attention Requirements Bulletin 737-25-1866 RB,
Revision 2, dated July 19, 2024, do all applicable actions
identified in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Requirements Bulletin 737-
25-1855 RB, Revision 1, dated April 13, 2022 (for Model 737-600, -
700, -700C, -800, -900, and -900ER series airplanes), and Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 2,
dated July 19, 2024 (for Model 737-8, 737-9, and 737-8200
airplanes); as applicable.
Note 3 to paragraph (h): Guidance for accomplishing the actions
required by paragraph (h) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1855, Revision 1, dated April 13,
2022, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1855 RB, Revision 1, dated April 13, 2022.
Note 4 to paragraph (h): Guidance for accomplishing the actions
required by paragraph (h) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1866, Revision 2, dated July 19,
2024, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 2, dated July 19, 2024.
Exact source excerpt. Text positions 15217–16910, end exclusive, in the original decoded publication. SHA-256: d489ab85b54fa386725c97ef65feea7eb392f8ebbe8a86f55ae561bb8f632638
Exceptions to Requirements Bulletin Specifications
(i) Exceptions to Requirements Bulletin Specifications
(1) For paragraph (g) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, Revision 1,
dated April 13, 2022, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1855 RB,'' this AD requires using June
29, 2023 (the effective date of AD 2023-09-04).
(2) For paragraph (g) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 1,
dated April 11, 2022, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1866 RB,'' this AD requires using June
29, 2023 (the effective date of AD 2023-09-04).
(3) For paragraph (h) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, Revision 1,
dated April 13, 2022, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1855 RB,'' this AD requires using the
effective date of this AD.
(4) For paragraph (h) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 2,
dated July 19, 2024, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1866 RB,'' this AD requires using the
effective date of this AD.
(5) Where Boeing Special Attention Requirements Bulletin 737-25-
1855 RB, Revision 1, dated April 13, 2022; Boeing Special Attention
Requirements Bulletin 737-25-1866 RB, Revision 1, dated April 11,
2022; and Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 2, dated July 19, 2024, specify doing an inspection of
the escape slide assembly to determine whether P/N 5A3307-7 is
installed, for this AD a review of airplane maintenance records is
acceptable in lieu of this inspection, provided the part number of
the escape slide assembly can be conclusively determined from that
review.
Exact source excerpt. Text positions 16910–19074, end exclusive, in the original decoded publication. SHA-256: 87921257df4831f0ae59af0933100868f4eae99a7702fa81970a271a9ebeaabb
Credit for Previous Actions
(j) Credit for Previous Actions
(1) This paragraph provides credit for the actions specified in
paragraph (g) of this AD, if those actions were performed before
June 29, 2023 (the effective date of AD 2023-09-04) using Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, dated August
31, 2021; or Boeing Special Attention Requirements Bulletin 737-25-
1866 RB, dated September 27, 2021; as applicable.
(2) This paragraph provides credit for the actions specified in
paragraph (h) of this AD, if those actions were performed before the
effective date of this AD using Boeing Special Attention
Requirements Bulletin 737-25-1855 RB, dated August 31, 2021; Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, dated
September 27, 2021; or Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 1, dated April 11, 2022; as
applicable.
Exact source excerpt. Text positions 19074–19963, end exclusive, in the original decoded publication. SHA-256: 905a6813916447a1f6133dd3d0f20f4488a07430cd1f6848837d75a787893f81
Alternative Methods of Compliance (AMOCs)
(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: [email protected].
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
responsible Flight Standards Office.
(2) 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.
(3) AMOCs approved for AD 2023-09-04 are approved as AMOCs for
the corresponding provisions of paragraph (g) of this AD.
Exact source excerpt. Text positions 19963–21365, end exclusive, in the original decoded publication. SHA-256: 9348f7cb2f963ead736f7de4341eaac914f59500de58b701dc01da3671f21881
Additional Information
(l) Additional Information
(1) For more information about this AD, contact Katherine
Venegas, Aviation Safety Engineer, FAA, 2200 South 216th St., Des
Moines, WA 98198; phone: 562-627-5353; email:
[email protected].
(2) Material identified in this AD that is not incorporated by
reference is available at the address specified in paragraph (m)(5)
this AD.
Exact source excerpt. Text positions 21365–21736, end exclusive, in the original decoded publication. SHA-256: 218ed1406f7cf17886295ae3d15ac5390cd54a9ed15b8d426bc60830939061e7
Material Incorporated by Reference
(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.
(3) The following material was approved for IBR on January 16,
2026.
[[Page 57688]]
(i) Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 2, dated July 19, 2024.
(ii) [Reserved]
(4) The following material was approved for IBR on June 29, 2023
(88 FR 33817, May 25, 2023).
(i) Boeing Special Attention Requirements Bulletin 737-25-1855
RB, Revision 1, dated April 13, 2022.
(ii) Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 1, dated April 11, 2022.
(5) For the 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 [email protected].
Exact source excerpt. Text positions 21736–23330, end exclusive, in the original decoded publication. SHA-256: dd23f348ff2e0188683382de087d67894a0175f234545fb7e5cddc2a5ab84770
Explicit historical replacement wording
Find all recorded historical references to AD 2025-25-04 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 735cc9fd72f578198be2380cc33c4aa2bd1513aad4407763606709177a29517d. Source manifest: 62ab8c1034efe998573264f2677ffcec0e680fb6b3b0ac67cf295e12541473af.
Official source · 2025-12-12
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[Federal Register Volume 90, Number 237 (Friday, December 12, 2025)]
[Rules and Regulations]
[Pages 57685-57688]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2025-22629]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2025-0481; Project Identifier AD-2024-00614-T;
Amendment 39-23212; AD 2025-25-04]
RIN 2120-AA64
Airworthiness Directives; The Boeing Company Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is superseding Airworthiness Directive (AD) 2023-09-
04, which applied to certain The Boeing Company Model 737-600, -700, -
700C, -800, -900, and -900ER series airplanes, and certain Model 737-8
and -9 airplanes. AD 2023-09-04 required inspecting all escape slide
assemblies to identify affected parts and replacing affected escape
slide assemblies with different assemblies. This AD was prompted by the
determination that additional airplanes might be affected by the unsafe
condition. This AD retains the requirements of AD 2023-09-04 and
requires those actions for additional airplanes, including Model 737-
8200 airplanes. The FAA is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective January 16, 2026.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 16,
2026.
The Director of the Federal Register approved the incorporation by
reference of certain other publications listed in this AD as of June
29, 2023 (88 FR 33817, May 25, 2023).
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2025-0481; 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 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.
<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 regulations.gov under
Docket No. FAA-2025-0481.
FOR FURTHER INFORMATION CONTACT: Katherine Venegas, Aviation Safety
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 562-
627-5353; email: [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2023-09-04, Amendment 39-22427 (88 FR
33817, May 25, 2023) (AD 2023-09-04). AD 2023-09-04 applied to certain
The Boeing Company Model 737-600, -700, -700C, -800, -900, and -900ER
series airplanes, and certain Model 737-8 and -9 airplanes. The NPRM
was published in the Federal Register on April 10, 2025 (90 FR 15321).
The NPRM was prompted by the determination that additional airplanes
might be affected by the unsafe condition. In the NPRM, the FAA
proposed to continue to require the actions in AD 2023-09-04 and
requires those actions for additional airplanes, including Model 737-
8200 airplanes. The FAA is issuing this AD to address inflation of the
escape slide while it is in the escape slide compartment, which could
result in injury to passengers and crew during normal operation, or
impede an emergency evacuation by rendering the exit unusable.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from the Air Line Pilots Association,
International (ALPA), Aviation Partners Boeing (APB), Boeing, ProTech
Aero Services Limited (ProTech), and United Airlines who supported the
NPRM without change.
The FAA received an additional comment from the Turkish Airlines.
The following presents the comment received on the NPRM and the FAA's
response to the comment.
Request To Revise the Credit for Previous Actions Paragraph
Turkish Airlines requested that the FAA revise paragraph (j)(1) of
the proposed AD to provide credit for the actions specified in
paragraph (g) of the proposed AD if those actions were performed before
the effective date of the proposed AD, using Boeing Special Attention
Requirements Bulletin 737-25-1855 RB, dated August 31, 2021; or Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, dated September
27, 2021; as applicable. In the NPRM, the FAA proposed to provide
credit only if those actions were performed before June 29, 2023 (the
effective date of AD 2023-09-04). The commenter stated that paragraph
(j)(1) of the proposed AD does not cover actions performed between June
29, 2023, and the effective date of the proposed AD.
The FAA disagrees with the request. Paragraphs (g) and (j)(1) of
this AD retain the requirements of paragraphs (g) and (i),
respectively, of AD 2023-09-04 with no changes. Accordingly, paragraph
(j)(1) of this AD provides credit for the requirements of paragraph (g)
of this AD using the original issue of the applicable requirements
bulletin, only if performed before June 29, 2023. After June 29, 2023,
the requirements of paragraph (g) must be accomplished using Revision 1
of the applicable requirements bulletin. If operators would like to use
the original issue of the applicable requirements bulletin after June
29, 2023, operators must request approval to use that service
information as an alternative method of compliance (AMOC) under the
provisions of paragraph (k) of this AD. The FAA has not changed the AD
in this regard.
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, this
AD is adopted as proposed in the NPRM. None of the changes will
[[Page 57686]]
increase the economic burden on any operator.
Material Incorporated by Reference Under 1 CFR Part 51
The FAA reviewed Boeing Special Attention Requirements Bulletin
737-25-1866 RB, Revision 2, dated July 19, 2024. This material
specifies procedures for inspecting all escape slide assemblies to
identify any escape slide assembly having part number (P/N) 5A3307-7
and replacing it with an assembly having P/N 5A3307-9 or P/N 5A3307-
701. Escape slide assembly P/N 5A3307-701 is one on which a firing
cable retention has been modified and the assembly has been
reidentified with a new part number.
This AD also requires Boeing Special Attention Requirements
Bulletin 737-25-1855 RB, Revision 1, dated April 13, 2022; and Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 1,
dated April 11, 2022, which the Director of the Federal Register
approved for incorporation by reference as of June 29, 2023 (88 FR
33817, May 25, 2023).
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 2,666 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Inspection or maintenance records 2 work-hours x $85 per $0 $170 $425,340 (2,502
review (retained action from AD hour = $170. airplanes)
2023-09-04).
Inspection or maintenance records 2 work-hours x $85 per 0 170 $27,880 (164 airplanes)
review (new action). hour = $170.
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any replacements that
would be required based on the results of the inspection. The agency
has no way of determining the number of aircraft that might need these
replacements:
On-Condition Costs
----------------------------------------------------------------------------------------------------------------
Action Labor cost Parts cost Cost per product
----------------------------------------------------------------------------------------------------------------
Replacement.................... Up to 1 work hour x Up to $19,000.................. Up to $19,085 per
$85 per hour = up to escape slide
$85. assembly.
----------------------------------------------------------------------------------------------------------------
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:
0
a. Removing Airworthiness Directive (AD) 2023-09-04, Amendment 39-22427
(88 FR 33817, May 25, 2023); and
0
b. Adding the following new AD:
2025-25-04 The Boeing Company: Amendment 39-23212; Docket No. FAA-
2025-0481; Project Identifier AD-2024-00614-T.
(a) Effective Date
This airworthiness directive (AD) is effective January 16, 2026.
(b) Affected ADs
This AD replaces AD 2023-09-04, Amendment 39-22427 (88 FR 33817,
May 25, 2023) (AD 2023-09-04).
(c) Applicability
This AD applies to The Boeing Company Model 737-600, -700, -
700C, -800, -900, and -900ER series airplanes, and Model 737-8, 737-
9, and 737-8200 airplanes, certificated in any category.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Unsafe Condition
This AD was prompted by reports of uncommanded escape slide
deployments in the passenger compartment, caused by too much tension
in the inflation cable and the movement of the escape slide assembly
in the escape slide compartment. The FAA is issuing this AD to
address inflation of the
[[Page 57687]]
escape slide while it is in the escape slide compartment, which
could result in injury to passengers and crew during normal
operation, or impede an emergency evacuation by rendering the exit
unusable.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Retained Inspection, With No Changes
This paragraph restates the requirements of paragraph (g) of AD
2023-09-04, with no changes. For airplanes identified in Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, Revision 1,
dated April 13, 2022; and Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 1, dated April 11, 2022: Except as
specified in paragraph (i) of this AD, at the applicable times
specified in the ``Compliance'' paragraph of Boeing Special
Attention Requirements Bulletin 737-25-1855 RB, Revision 1, dated
April 13, 2022; and Boeing Special Attention Requirements Bulletin
737-25-1866 RB, Revision 1, dated April 11, 2022, do all applicable
actions identified in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Requirements Bulletin 737-
25-1855 RB, Revision 1, dated April 13, 2022 (for Model 737-600, -
700, -700C, -800, -900, and -900ER series airplanes); and Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 1,
dated April 11, 2022 (for Model 737-8 and -9 airplanes); as
applicable.
Note 1 to paragraph (g): Guidance for accomplishing the actions
required by paragraph (g) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1855, Revision 1, dated April 13,
2022, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1855 RB, Revision 1, dated April 13, 2022.
Note 2 to paragraph (g): Guidance for accomplishing the actions
required by paragraph (g) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1866, Revision 1, dated April 11,
2022, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 1, dated April 11, 2022.
(h) New Required Actions
For airplanes not identified in Boeing Special Attention
Requirements Bulletin 737-25-1855 RB, Revision 1, dated April 13,
2022; or Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 1, dated April 11, 2022: Except as specified in
paragraph (i) of this AD, at the applicable times specified in the
``Compliance'' paragraph of Boeing Special Attention Requirements
Bulletin 737-25-1855 RB, Revision 1, dated April 13, 2022; and
Boeing Special Attention Requirements Bulletin 737-25-1866 RB,
Revision 2, dated July 19, 2024, do all applicable actions
identified in, and in accordance with, the Accomplishment
Instructions of Boeing Special Attention Requirements Bulletin 737-
25-1855 RB, Revision 1, dated April 13, 2022 (for Model 737-600, -
700, -700C, -800, -900, and -900ER series airplanes), and Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 2,
dated July 19, 2024 (for Model 737-8, 737-9, and 737-8200
airplanes); as applicable.
Note 3 to paragraph (h): Guidance for accomplishing the actions
required by paragraph (h) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1855, Revision 1, dated April 13,
2022, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1855 RB, Revision 1, dated April 13, 2022.
Note 4 to paragraph (h): Guidance for accomplishing the actions
required by paragraph (h) of this AD can be found in Boeing Special
Attention Service Bulletin 737-25-1866, Revision 2, dated July 19,
2024, which is referred to in Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 2, dated July 19, 2024.
(i) Exceptions to Requirements Bulletin Specifications
(1) For paragraph (g) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, Revision 1,
dated April 13, 2022, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1855 RB,'' this AD requires using June
29, 2023 (the effective date of AD 2023-09-04).
(2) For paragraph (g) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 1,
dated April 11, 2022, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1866 RB,'' this AD requires using June
29, 2023 (the effective date of AD 2023-09-04).
(3) For paragraph (h) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, Revision 1,
dated April 13, 2022, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1855 RB,'' this AD requires using the
effective date of this AD.
(4) For paragraph (h) of this AD: Where the Compliance Time
columns of the tables in the ``Compliance'' paragraph of Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, Revision 2,
dated July 19, 2024, use the phrase ``the Original Issue date of
Requirements Bulletin 737-25-1866 RB,'' this AD requires using the
effective date of this AD.
(5) Where Boeing Special Attention Requirements Bulletin 737-25-
1855 RB, Revision 1, dated April 13, 2022; Boeing Special Attention
Requirements Bulletin 737-25-1866 RB, Revision 1, dated April 11,
2022; and Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 2, dated July 19, 2024, specify doing an inspection of
the escape slide assembly to determine whether P/N 5A3307-7 is
installed, for this AD a review of airplane maintenance records is
acceptable in lieu of this inspection, provided the part number of
the escape slide assembly can be conclusively determined from that
review.
(j) Credit for Previous Actions
(1) This paragraph provides credit for the actions specified in
paragraph (g) of this AD, if those actions were performed before
June 29, 2023 (the effective date of AD 2023-09-04) using Boeing
Special Attention Requirements Bulletin 737-25-1855 RB, dated August
31, 2021; or Boeing Special Attention Requirements Bulletin 737-25-
1866 RB, dated September 27, 2021; as applicable.
(2) This paragraph provides credit for the actions specified in
paragraph (h) of this AD, if those actions were performed before the
effective date of this AD using Boeing Special Attention
Requirements Bulletin 737-25-1855 RB, dated August 31, 2021; Boeing
Special Attention Requirements Bulletin 737-25-1866 RB, dated
September 27, 2021; or Boeing Special Attention Requirements
Bulletin 737-25-1866 RB, Revision 1, dated April 11, 2022; as
applicable.
(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: [email protected].
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
responsible Flight Standards Office.
(2) 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.
(3) AMOCs approved for AD 2023-09-04 are approved as AMOCs for
the corresponding provisions of paragraph (g) of this AD.
(l) Additional Information
(1) For more information about this AD, contact Katherine
Venegas, Aviation Safety Engineer, FAA, 2200 South 216th St., Des
Moines, WA 98198; phone: 562-627-5353; email:
[email protected].
(2) Material identified in this AD that is not incorporated by
reference is available at the address specified in paragraph (m)(5)
this AD.
(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.
(3) The following material was approved for IBR on January 16,
2026.
[[Page 57688]]
(i) Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 2, dated July 19, 2024.
(ii) [Reserved]
(4) The following material was approved for IBR on June 29, 2023
(88 FR 33817, May 25, 2023).
(i) Boeing Special Attention Requirements Bulletin 737-25-1855
RB, Revision 1, dated April 13, 2022.
(ii) Boeing Special Attention Requirements Bulletin 737-25-1866
RB, Revision 1, dated April 11, 2022.
(5) For the 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 [email protected].
Issued on December 3, 2025.
Peter A. White,
Deputy Director, Integrated Certificate Management Division, Aircraft
Certification Service.
[FR Doc. 2025-22629 Filed 12-11-25; 8:45 am]
BILLING CODE 4910-13-P
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