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2022-08-05 THE BOEING COMPANY:
Amendment 39-22008; Docket No. FAA-2021-1169; Project Identifier AD-2021-01011-T.

(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective May 27, 2022.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to The Boeing Company  Model 737-800 series airplanes,
    certificated in any category,  as identified  in Boeing Alert Require-
    ments Bulletin 737-53A1401 RB, dated April 27, 2021.

(d) SUBJECT

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) UNSAFE CONDITION

    This AD  was prompted  by the determination  that insufficient sealing
    may allow water to enter the lower lobe electronic equipment (EE)  bay
    through the  main deck  floor structure  at the  rigid cargo  barrier,
    which could cause damage  to EE bay line  replacement units in the  E5
    rack. The FAA is issuing this AD to address water ingress in the lower
    lobe  EE bay,  which could  result in  water damage  to  the  air data
    inertial  reference  units  and  flight  management  computers  during
    flight, leading to a complete loss of data to primary flight  displays
    and  electronic navigation  functions, which  could prevent  continued
    safe flight and landing.

(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 Alert Require-
    ments Bulletin 737-53A1401 RB, dated April 27, 2021, do all applicable
    actions identified in, and in accordance with,  the Accomplishment In-
    structions of Boeing Alert Requirements Bulletin 737-53A1401 RB, dated
    April 27, 2021.

Note 1 to paragraph (g):  Guidance for accomplishing  the actions required
by this AD  can  be  found  in  Boeing Alert Service Bulletin 737-53A1401,
dated  April 27, 2021,  which is referred  to in Boeing Alert Requirements
Bulletin 737-53A1401 RB, dated April 27, 2021.

(h) EXCEPTIONS TO SERVICE INFORMATION SPECIFICATIONS

(1) Where the Compliance Time column  of the tables  in  the  "Compliance"
    paragraph of Boeing Alert Requirements Bulletin 737-53A1401 RB,  dated
    April 27, 2021,  uses the phrase  "the original issue date of Require-
    ments Bulletin 737-53A1401 RB,"  this AD requires using "the effective
    date of this AD."

(2) Where Boeing Alert Requirements Bulletin 737-53A1401 RB,  dated  April
    27, 2021, specifies contacting Boeing for repair instructions: This AD
    requires doing the repair using  a method approved in accordance  with
    the procedures specified in paragraph (i) of this AD.

(i) 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 (j) of this AD. Information may be emailed to:
    9-ANM-Seattle-ACO-AMOCRequests@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,  modifica-
    tion deviation,  or  alteration deviation  must meet the certification
    basis of  the airplane,  and the  approval must  specifically refer to
    this AD.

(j) RELATED INFORMATION

    For more information about this AD,  contact Courtney Tuck,  Aerospace
    Engineer, Cabin Safety and Environmental Systems Section, FAA, Seattle
    ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax:
    206-231-3986; email: courtney.k.tuck@faa.gov.

(k) 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 Alert Requirements Bulletin  737-53A1401  RB,  dated  April 27,
    2021.

(ii) [Reserved]

(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; Internet https://www.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: https://www.archives.gov/federal-register/cfr/ibr
    -locations.html.

Issued on April 4, 2022.  Lance T. Gant, Director, Compliance & Airworthi-
ness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:  Courtney Tuck, Aerospace Engineer, Cabin
Safety and Environmental Systems Section,  FAA,  Seattle ACO Branch,  2200
South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3986; email:
courtney.k.tuck@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-1169; Project Identifier AD-2021-01011-T;
Amendment 39-22008; AD 2022-08-05]
RIN 2120-AA64

Airworthiness Directives; The Boeing Company Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain The Boeing Company Model 737-800 series airplanes. This AD was
prompted by the determination that insufficient sealing may allow water
to enter the lower lobe electronic equipment (EE) bay through the main
deck floor structure at the rigid cargo barrier (RCB), which could
cause damage to EE bay line replacement units (LRUs) in the E5 rack.
This AD requires detailed inspections for the presence and condition of
sealant at certain locations and applicable on-condition actions. This
AD also requires replacing the moisture barrier tape at a certain
location, replacing the weather seal at a certain location, and
installing seat track fillers. The FAA is issuing this AD to address
the unsafe condition on these products.

DATES: This AD is effective May 27, 2022
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of May 27,
2022.

ADDRESSES: For service information identified in this final rule,
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; internet https://www.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
https://www.regulations.gov by searching for and locating Docket No.
FAA-2021-1169.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-1169; 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.

FOR FURTHER INFORMATION CONTACT: Courtney Tuck, Aerospace Engineer,
Cabin Safety and Environmental Systems Section, FAA, Seattle ACO
Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-
231-3986; email: courtney.k.tuck@faa.gov.

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 737-800 series airplanes. The
NPRM published in the Federal Register on January 26, 2022 (87 FR
3946). The NPRM was prompted by the determination that insufficient
sealing may allow water to enter the lower lobe EE bay through the main
deck floor structure at the RCB, which could cause damage to EE bay
LRUs in the E5 rack. In the NPRM, the FAA proposed to require detailed
inspections for the presence and condition of sealant at certain
locations and applicable on-condition actions. The NPRM also proposed
to require replacing the moisture barrier tape at a certain location,
replacing the weather seal at a certain location, and installing seat
track fillers. The FAA is issuing this AD to address water ingress in
the lower lobe EE bay, which could result in water damage to the air
data inertial reference units and flight management computers during
flight, leading to a complete loss of data to primary flight displays
and electronic navigation functions, which could prevent continued safe
flight and landing.

Discussion of Final Airworthiness Directive

Comments

The FAA received comments from Air Line Pilots Association,
International (ALPA), Boeing, and an individual, who supported the NPRM
without change.
The FAA received an additional comment from Aviation Partners
Boeing (APB). The following presents the comment received on the NPRM
and the FAA's response to the comment.

Effect of Winglets on Accomplishment of the Proposed Actions

APB stated that the installation of winglets per Supplemental Type
Certificate (STC) ST00830SE does not affect compliance with the
mandated actions in the proposed rule.
The FAA agrees with the commenter. Therefore, the installation of
STC ST00830SE does not affect the ability to accomplish the actions
required by this AD. The FAA has not changed this 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. Except for minor editorial changes, this AD is adopted as
proposed in the NPRM. None of the changes will increase the economic
burden on any operator.

Related Service Information Under 1 CFR Part 51

The FAA reviewed Boeing Alert Requirements Bulletin 737-53A1401 RB,
dated April 27, 2021. This service information specifies procedures for
detailed inspections of the forward main deck cargo compartment floor
to RCB, floor panel joints, drain troughs, seat track splices, and, for
some airplanes, the lower lobe E5 rack drain pan shroud for sealant
condition and application, and applicable on-condition actions. This
service information also specifies procedures for replacing the main
deck cargo door weather seal, replacing the moisture barrier tape on
the forward main deck cargo compartment floor, and installing seat
track fillers in the EE bay. On-condition actions include repair,
removing existing sealant, and applying new sealant. 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.

Costs of Compliance

The FAA estimates that this AD affects 7 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs

Action Labor cost Parts cost Cost per product Cost on U.S. operators
Inspect sealant Up to 12 work-hours x $85 per hour = Up to $1,020 $0 Up to $1,020 Up to $7,140
Remove/reinstall drain trough Up to 15 hours x $85 per hour = Up to $1,275 Negligible Up to $1,275 Up to $8,925
Replace weather seal Up to 7 work-hours x $85 per hour = Up to $595 $9,680 Up to $10,275 Up to $71,925
Replace barrier tape Up to 20 work-hours x $85 per hour = Up to $1,700 Negligible Up to $1,700 Up to $11,900
Install seat track filler Up to 2 work-hours x $85 per hour = Up to $170 Negligible Up to $170 Up to $1,190

The FAA estimates the following costs to do any necessary
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
Install or replace sealant 26 work-hours x $85 per hour = $2,210
Negligible
$2,210

The FAA has received no definitive data on which to base the cost
estimates for the on-condition actions specified in this AD.
The FAA has included all known costs in its cost estimate.
According to the 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

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: