Rule2025-22629

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
December 12, 2025
Effective
January 16, 2026

Issuing agencies

Transportation DepartmentFederal Aviation Administration

Abstract

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.

Full Text

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<title>Federal Register, Volume 90 Issue 237 (Friday, December 12, 2025)</title>
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[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2025-22629]


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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.

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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 <a href="http://regulations.gov">regulations.gov</a> 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 <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-2025-0481.

FOR FURTHER INFORMATION CONTACT: Katherine Venegas, Aviation Safety 
Engineer, FAA, 2200 South 216th St., Des Moines, WA 98198; phone: 562-
627-5353; email: <a href="/cdn-cgi/l/email-protection#503b3124383522393e357e26353e35373123103631317e373f26"><span class="__cf_email__" data-cfemail="9cf7fde8f4f9eef5f2f9b2eaf9f2f9fbfdefdcfafdfdb2fbf3ea">[email&#160;protected]</span></a>.

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.
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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: <a href="/cdn-cgi/l/email-protection#6d2c20222e2d0b0c0c430a021b"><span class="__cf_email__" data-cfemail="67262a28242701060649000811">[email&#160;protected]</span></a>. 
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: 
<a href="/cdn-cgi/l/email-protection#167d77627e73647f787338607378737177655670777738717960"><span class="__cf_email__" data-cfemail="325953465a57405b5c571c44575c57555341725453531c555d44">[email&#160;protected]</span></a>.
    (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 <a href="http://myboeingfleet.com">myboeingfleet.com</a>.
    (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 <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#6402164a0d0a17140107100d0b0a240a0516054a030b12"><span class="__cf_email__" data-cfemail="dabca8f4b3b4a9aabfb9aeb3b5b49ab4bba8bbf4bdb5ac">[email&#160;protected]</span></a>.

    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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