Published 2022-04-22 · Federal Register document 2022-08543
Airworthiness Directives; The Boeing Company Airplanes
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:11.345539+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2022-c0cc5a172b1306fa
- Source row
- results[146]
- Raw source SHA-256
- c0cc5a172b1306fa2cd8dc66863122ada13332e685d87687bd0becf2dab37a5e
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2022-08-05
- Effective date printed in this edition
- 2022-05-27
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective May 27, 2022.
Exact source excerpt. Text positions 11965–12051, end exclusive, in the original decoded publication. SHA-256: 2bd35e72323951c5e0e4ae57032107838ea6b715eb55a62ce45971f1c4ff7402
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 12051–12080, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to The Boeing Company Model 737-800 series
airplanes, certificated in any category, as identified in Boeing
Alert Requirements Bulletin 737-53A1401 RB, dated April 27, 2021.
Exact source excerpt. Text positions 12080–12296, end exclusive, in the original decoded publication. SHA-256: 2358cac3cd7ab0ff443c4d6ce01a3c7fcb88eed71cf9e26dfbffb3dcb14aad28
Subject
(d) Subject
Air Transport Association (ATA) of America Code 53, Fuselage.
Exact source excerpt. Text positions 12296–12376, end exclusive, in the original decoded publication. SHA-256: 297e69b8a6e159f28612e8bd82a91daa2fd8fd1d9d38af67161f67738908fa6c
Unsafe Condition
(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.
Exact source excerpt. Text positions 12376–13045, end exclusive, in the original decoded publication. SHA-256: 80481017f747f87334f104ed6d28541e5aedea72bcf16901998637b3f7c56e52
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 13045–13147, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Required Actions
(g) Required Actions
Except as specified by paragraph (h) of this AD: At the
applicable times specified in the ``Compliance'' paragraph of Boeing
Alert Requirements Bulletin 737-53A1401 RB, dated April 27, 2021, do
all applicable actions identified in, and in accordance with, the
Accomplishment Instructions 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.
Exact source excerpt. Text positions 13147–13812, end exclusive, in the original decoded publication. SHA-256: 5d10e2ead2254762a14b0cc66cb6a141f019eaca73baa58cf2c6e22993affb82
Exceptions to Service Information Specifications
(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 Requirements 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.
Exact source excerpt. Text positions 13812–14452, end exclusive, in the original decoded publication. SHA-256: 53108716ef8c3bc0f75b9ca840fcdb279c13ae7d9c2ea7b6951ec3f9857cf0de
Alternative Methods of Compliance (AMOCs)
(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: [email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by The Boeing Company Organization Designation
Authorization (ODA) that has been authorized by the Manager, 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.
Exact source excerpt. Text positions 14452–15680, end exclusive, in the original decoded publication. SHA-256: f19291f3f42ac7c9f6795b7c518c1275dc0d73e4ccaff259645118512b5f206b
Related Information
(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: [email protected].
Exact source excerpt. Text positions 15680–15964, end exclusive, in the original decoded publication. SHA-256: 2583f75a04bb6458c01a5fe07d3fc1b2235c9942bd2caa65cc38e0df7b543749
Material Incorporated by Reference
(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 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.
(4) 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 15964–17240, end exclusive, in the original decoded publication. SHA-256: a366b845af9afc0fe7f64054fb22b573d1a6b2e7a73027e71e4f54b15546b978
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2022-08-05 · 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: 7cdfff1a260d57a015f6398c229a22a1ccc2592eeecb5f752ef7e236a462da97. Source manifest: 39c8ee0520ac90ffb53ab8178ab2bbf110da3a32b1936b77de3ef871e3cdcb0a.
Official source · 2022-04-22
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 87, Number 78 (Friday, April 22, 2022)]
[Rules and Regulations]
[Pages 24034-24036]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-08543]
-----------------------------------------------------------------------
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: [email protected].
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
[[Page 24035]]
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 $0......................... Up to $1,020............... Up to $7,140.
per hour = Up to $1,020.
Remove/reinstall drain trough....... Up to 15 hours x $85 per Negligible................. Up to $1,275............... Up to $8,925.
hour = Up to $1,275.
Replace weather seal................ Up to 7 work-hours x $85 $9,680..................... Up to $10,275.............. Up to $71,925.
per hour = Up to $595.
Replace barrier tape................ Up to 20 work-hours x $85 Negligible................. Up to $1,700............... Up to $11,900.
per hour = Up to $1,700.
Install seat track filler........... Up to 2 work-hours x $85 Negligible................. Up to $170................. Up to $1,190.
per hour = Up to $170.
--------------------------------------------------------------------------------------------------------------------------------------------------------
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
----------------------------------------------------------------------------------------------------------------
Cost per
Action Labor cost Parts cost product
----------------------------------------------------------------------------------------------------------------
Install or replace sealant.......... 26 work-hours x $85 per hour Negligible.................. $2,210
= $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.
[[Page 24036]]
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive:
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 Requirements 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 already done.
(g) Required Actions
Except as specified by paragraph (h) of this AD: At the
applicable times specified in the ``Compliance'' paragraph of Boeing
Alert Requirements Bulletin 737-53A1401 RB, dated April 27, 2021, do
all applicable actions identified in, and in accordance with, the
Accomplishment Instructions 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 Requirements 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: [email protected].
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
(3) An AMOC that provides an acceptable level of safety may be
used for any repair, modification, or alteration required by this AD
if it is approved by The Boeing Company Organization Designation
Authorization (ODA) that has been authorized by the Manager, 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.
(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: [email protected].
(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 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.
(4) 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on April 4, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-08543 Filed 4-21-22; 8:45 am]
BILLING CODE 4910-13-P
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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