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PROPOSED AD THE BOEING COMPANY: Docket No. FAA-2022-1410; Project Identifier AD-2022-00198-T.
(a) COMMENTS DUE DATE

    The FAA must receive comments on this airworthiness directive (AD)  by
    January 17, 2023.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This  AD  applies  to The Boeing Company airplanes identified in para-
    graphs (c)(1) and (2) of this AD.

(1) Model 737-600, -700, -700C, -800, -900 and -900ER series airplanes, as
    identified  in  Boeing Special Attention Requirements Bulletin 737-25-
    1855 RB, Revision 1, dated April 13, 2022.

(2) Model 737-8 and -9 airplanes as identified in Boeing Special Attention
    Requirements Bulletin 737-25-1866 RB, Revision 1 dated April 11, 2022.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 25, Equipment/furnish-
    ings.

(e) UNSAFE CONDITION

    This  AD  was prompted  by reports of uncommanded escape slide deploy-
    ments 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 infla-
    tion of the escape slide  while it is in the escape slide compartment,
    which could result in injury to passengers and crew  during normal op-
    eration, or impede an emergency evacuation by rendering the exit unus-
    able.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready 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 Atten-
    tion 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 ident-
    ified 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 this AD can be found in Boeing Special Attention 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 this AD can be found in Boeing Special Attention 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) EXCEPTIONS TO SERVICE INFORMATION SPECIFICATIONS

(1) 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."

(2) 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 "the effective date of this AD."

(i) CREDIT FOR PREVIOUS ACTIONS

    This paragraph provides credit for the actions specified in  paragraph
    (g) 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,  or  Boeing Special Attention
    Requirements Bulletin  737-25-1866 RB,  dated  September 27, 2021,  as
    applicable.

(j) ALTERNATIVE METHODS OF COMPLIANCE (AMOCS)

(1) The  Manager,  Seattle ACO 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 (k) of this AD. Information may be emailed to:
    9-ANM-Seattle-ACO-AMOC-Requests@faa.gov.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking a principal inspector,  the manager of the respon-
    sible 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,  Seattle ACO 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.

(k) RELATED INFORMATION

    For more information about this AD,  contact Brandon Lucero, Aerospace
    Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle
    ACO Branch, 2200 South 216th St, Des Moines, WA 98198; phone: 206-231-
    3569; email: brandon.lucero@faa.gov.

(l) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference  (IBR)  of the service information  listed in this paragraph
    under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this service information as applicable  to do the actions
    required by this AD, unless the AD specifies otherwise.

(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, Revi-
     sion 1, dated April 11, 2022.

(3) For service information identified in this AD,  contact Boeing Commer-
    cial Airplanes,  Attention:  Contractual & Data Services (C&DS),  2600
    Westminster Blvd.,  MC 110-SK57, Seal Beach, CA 90740-5600;  telephone
    562-797-1717; website myboeingfleet.com.

(4) You may view this service information at the FAA,  Airworthiness Prod-
    ucts 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 service information  that is incorporated by refer-
    ence at the National Archives and Records Administration  (NARA).  For
    information on the availability of this material at NARA fr.inspection
    @nara.gov or go to www.archives.gov/federal-register/cfr/ibr-locations
    .html.

Issued on November 1, 2022.  Christina Underwood, Acting Director, Compli-
ance & Airworthiness Division, Aircraft Certification Service.

DATES: The FAA must receive comments  on this proposed AD  by  January 17,
2023.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-1410; Project Identifier AD-2022-00198-T]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain The Boeing Company Model 737-600, -700, -700C, -800, -900,
and -900ER series airplanes, and certain Model 737-8 and -9 airplanes.
This proposed 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. This proposed AD would require inspecting
all escape slide assemblies to identify affected parts, and applicable
on-condition actions. The FAA is proposing this AD to address the
unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by January 17,
2023.

ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to regulations.gov. Follow
the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1410; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this NPRM, any comments received, and other information. The
street address for Docket Operations is listed above.
Material Incorporated by Reference:
For service information identified in this NPRM, 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.
You may view this service information 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-2022-1410.

FOR FURTHER INFORMATION CONTACT: Brandon Lucero, Aerospace Engineer,
Cabin Safety and Environmental Systems Section, FAA, Seattle ACO
Branch, 2200 South 216th St., Des Moines, WA 98198; phone: 206-231-
3569; email: brandon.lucero@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2022-1410; Project Identifier
AD-2022-00198-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
this proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this NPRM.

Confidential Business Information

CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to
Brandon Lucero, Aerospace Engineer, Cabin Safety and Environmental
Systems Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des
Moines, WA 98198; phone: 206-231-3569; email: brandon.lucero@faa.gov.
Any commentary that the FAA receives that is not specifically
designated as CBI will be placed in the public docket for this
rulemaking.

Background

The FAA has received reports from Boeing of uncommanded escape
slide deployments in the passenger compartment while the airplane was
on the ground, caused by too much tension in the inflation cable
(introduced during packing of the slide) and the movement of the escape
slide assembly in the escape slide compartment during normal airplane
operations. The escape slide is used in the door-mounted escape system
of the forward and aft entry doors, and the forward and aft galley
service doors on the affected airplanes. This excessive tension and
movement could result in inflation of the escape slide while it is in
the escape slide compartment or uncommanded deployment of the escape
slide inside the cabin. This unsafe condition, if not addressed, could
result in injury to passengers and crew during normal airplane
operation or impede an emergency evacuation by rendering the exit
unusable.

FAA's Determination

The FAA is issuing this NPRM after determining that the unsafe
condition described previously is likely to exist or develop on other
products of the same type design.

Related Service Information Under 1 CFR Part 51

The FAA reviewed 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. This service information specifies procedures for inspecting
all escape slide assemblies to identify affected parts, and applicable
on-condition actions. The on-condition actions include replacing any
escape slide assembly having part number (P/N) 5A3307-7 with a new
assembly having P/N 5A3307-9 or P/N 5A3307-701 (an escape slide
assembly having P/N 5A3307-701 is one on which a firing cable retention
modification has been done and the assembly has been reidentified).
These documents are distinct since they apply to different airplane
models.
This service information is reasonably available because the
interested parties have access to it through their normal course of
business or by the means identified in ADDRESSES.

Proposed AD Requirements in This NPRM

This proposed AD would require accomplishing the actions specified
in the service information already described, except for any
differences identified as exceptions in the regulatory text of this
proposed AD. For information on the procedures and compliance times,
see this service information at regulations.gov by searching for and
locating Docket No. FAA-2022-1410.

Costs of Compliance

The FAA estimates that this AD, if adopted as proposed, would
affect 2,502 airplanes of U.S. registry. The FAA estimates the
following costs to comply with this proposed AD:

Estimated Costs

Action
Labor cost
Parts cost
Cost per product
Cost on U.S. operators
Inspection 1 work-hours x $85 per hour = $85
$0
$170
$212,670

The FAA estimates the following costs to do any necessary
replacements that would be required based on the results of the
proposed 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 hours x $85 per hour = up to $85 Up to $19,000 Up to $19,085 per escape slide 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

The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national Government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.

The Proposed Amendment

Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

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]

2. The FAA amends Sec. 39.13 by adding the following new
airworthiness directive: