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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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680238d3b913b51bfcc16650b95c133c5ff313ca3bee372d504708db526ddf8e
Text SHA-256
7cdfff1a260d57a015f6398c229a22a1ccc2592eeecb5f752ef7e236a462da97

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