Published 2021-06-24 · Federal Register document 2021-13125
Airworthiness Directives; The Boeing Company Airplanes
Publication summary
The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737-8 and 737-9 airplanes. This AD was prompted by a report that during refueling of the right main tank, if there is a failure of the automatic shutoff system, the refueling panel does not provide the required indication that the automatic shutoff has failed. This AD requires installing a new fuel quantity processor unit (FQPU) and doing an FQPU software check. 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 2026-09-03T22:24:08.106391+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2021-9c919420683447c6
- Source row
- results[218]
- Raw source SHA-256
- 9c919420683447c683ad0c877cb886e341c11862be32b47c536a001b1d76dcb5
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2021-12-13
- Effective date printed in this edition
- 2021-07-29
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective July 29, 2021.
Exact source excerpt. Text positions 8219–8306, end exclusive, in the original decoded publication. SHA-256: c0ddcba3e52c2b17f7241130aaccfe94293ddb1866575e2ab97ea2868b3c809d
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 8306–8335, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(c) Applicability
This AD applies to The Boeing Company Model 737-8 and 737-9
airplanes, certificated in any category, as identified in Boeing
Special Attention Requirements Bulletin 737-28-1363 RB, dated June
2, 2020.
Exact source excerpt. Text positions 8335–8563, end exclusive, in the original decoded publication. SHA-256: 54204c86aa46a892e59194301aa0e494600422ae6ed31f9474d4f5ea3fa33312
Subject
(d) Subject
Air Transport Association (ATA) of America Code 28, Fuel.
[[Page 33112]]
Exact source excerpt. Text positions 8563–8655, end exclusive, in the original decoded publication. SHA-256: 1e004d1ff11486a5d6f03675fce5a8535f5ce3a0e835395e28d16a4b43319535
Unsafe Condition
(e) Unsafe Condition
This AD was prompted by a report that during refueling of the
right main tank, if there is a failure of the automatic shutoff
system, the refueling panel does not provide the required flashing
indication that the automatic shutoff has failed to shut off the
fuel. The FAA is issuing this AD to address this indication failure
to warn the person fueling the airplane, which could cause overfill
of the right main tank, spilled fuel, and pooling on the ground that
could come in contact with an ignition source, resulting in a ground
fire.
Exact source excerpt. Text positions 8655–9228, end exclusive, in the original decoded publication. SHA-256: 6eed7116295a6b6413832dd7c5ce9dd875041a07514ab8a00c4bb6577e2c76eb
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 9228–9330, 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
Special Attention Requirements Bulletin 737-28-1363 RB, dated June
2, 2020, do all applicable actions identified in, and in accordance
with, the Accomplishment Instructions of Boeing Special Attention
Requirements Bulletin 737-28-1363 RB, dated June 2, 2020.
Note 1 to paragraph (g): Guidance for accomplishing the actions
required by this AD can be found in Boeing Special Attention Service
Bulletin 737-28-1363, dated June 2, 2020, which is referred to in
Boeing Special Attention Requirements Bulletin 737-28-1363 RB, dated
June 2, 2020.
Exact source excerpt. Text positions 9330–10036, end exclusive, in the original decoded publication. SHA-256: bdec9b1d0f387bb15ca20a282d54e59475d04f923ec156f3ab9031a61bca6896
Exception to Service Information Specifications
(h) Exception to Service Information Specifications
Where Boeing Special Attention Requirements Bulletin 737-28-1363
RB, dated June 2, 2020, uses the phrase ``the Original Issue date of
Requirements Bulletin 737-28-1363 RB,'' this AD requires using ``the
effective date of this AD.''
Exact source excerpt. Text positions 10036–10329, end exclusive, in the original decoded publication. SHA-256: 6c67eecfad941fca93a0034e805eea883bbe1b583479e2c909bd7d37100b9da5
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)(1) 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 10329–11560, end exclusive, in the original decoded publication. SHA-256: f451ab31f1b31cc9d8aede5ef2d6ba1b589303a255b9ab81531131abb1140b03
Related Information
(j) Related Information
(1) For more information about this AD, contact Chris Baker,
Aerospace Engineer, Propulsion Section, FAA, Seattle ACO Branch,
2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-
3552; email: [email protected].
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (4) of this AD.
Exact source excerpt. Text positions 11560–11989, end exclusive, in the original decoded publication. SHA-256: 843b5338dfa26a7b240ffc2f750fb50fc838bbc1a4aa7ea573a1ce2654610e52
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 Special Attention Requirements Bulletin 737-28-1363
RB, dated June 2, 2020.
(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 [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Exact source excerpt. Text positions 11989–13281, end exclusive, in the original decoded publication. SHA-256: 7ed724bcc341cdc63865f6affb62cb97589d515065bafdf6e06cc949c5e6cc04
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 2021-12-13 · 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.
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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: 15c48f68376d3d93712dfb10c5bf1abf0759000e761a596a53af932b6ea5c741. Source manifest: a24eb62b22113ae2f79828e44ab1a252ae063f60ce5e65696f0e7ab0900f996f.
Official source · 2021-06-24
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 86, Number 119 (Thursday, June 24, 2021)]
[Rules and Regulations]
[Pages 33110-33112]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-13125]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0017; Project Identifier AD-2020-01186-T;
Amendment 39-21600; AD 2021-12-13]
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 737-8 and 737-9 airplanes. This AD was
prompted by a report that during refueling of the right main tank, if
there is a failure of the automatic shutoff system, the refueling panel
does not provide the required indication that the automatic shutoff has
failed. This AD requires installing a new fuel quantity processor unit
(FQPU) and doing an FQPU software check. The FAA is issuing this AD to
address the unsafe condition on these products.
DATES: This AD is effective July 29, 2021.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of July 29,
2021.
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-2021-0017.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0017; 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
[[Page 33111]]
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590.
FOR FURTHER INFORMATION CONTACT: Chris Baker, Aerospace Engineer,
Propulsion Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des
Moines, WA 98198; phone and fax: 206-231-3552; 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 737-8 and 737-9 airplanes. The NPRM published in the
Federal Register on April 2, 2021 (86 FR 17324). The NPRM was prompted
by a report that during refueling of the right main tank, if there is a
failure of the automatic shutoff system, the refueling panel does not
provide the required indication that the automatic shutoff has failed.
In the NPRM, the FAA proposed to require installing a new FQPU and
doing an FQPU software check. The FAA is issuing this AD to address
this indication failure to warn the person fueling the airplane, which
could cause overfill of the right main tank, spilled fuel, and pooling
on the ground that could come in contact with an ignition source,
resulting in a ground fire.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from Boeing and United Airlines who
supported the NPRM without change.
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 Special Attention Requirements Bulletin
737-28-1363 RB, dated June 2, 2020. The service information specifies
procedures for replacing the FQPU having an incorrect indication
threshold with an FQPU with part number 30128-06 or 30128-58, as
applicable, or an FQPU with a later-approved part number, and doing an
FQPU software check. 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 66 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Installation and software check....... 3 work-hour x $85 per $0 $255 $16,830
hour = $255.
----------------------------------------------------------------------------------------------------------------
The FAA has included all known costs in this 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
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:
2021-12-13 The Boeing Company: Amendment 39-21600; Docket No. FAA-
2021-0017; Project Identifier AD-2020-01186-T.
(a) Effective Date
This airworthiness directive (AD) is effective July 29, 2021.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company Model 737-8 and 737-9
airplanes, certificated in any category, as identified in Boeing
Special Attention Requirements Bulletin 737-28-1363 RB, dated June
2, 2020.
(d) Subject
Air Transport Association (ATA) of America Code 28, Fuel.
[[Page 33112]]
(e) Unsafe Condition
This AD was prompted by a report that during refueling of the
right main tank, if there is a failure of the automatic shutoff
system, the refueling panel does not provide the required flashing
indication that the automatic shutoff has failed to shut off the
fuel. The FAA is issuing this AD to address this indication failure
to warn the person fueling the airplane, which could cause overfill
of the right main tank, spilled fuel, and pooling on the ground that
could come in contact with an ignition source, resulting in a ground
fire.
(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
Special Attention Requirements Bulletin 737-28-1363 RB, dated June
2, 2020, do all applicable actions identified in, and in accordance
with, the Accomplishment Instructions of Boeing Special Attention
Requirements Bulletin 737-28-1363 RB, dated June 2, 2020.
Note 1 to paragraph (g): Guidance for accomplishing the actions
required by this AD can be found in Boeing Special Attention Service
Bulletin 737-28-1363, dated June 2, 2020, which is referred to in
Boeing Special Attention Requirements Bulletin 737-28-1363 RB, dated
June 2, 2020.
(h) Exception to Service Information Specifications
Where Boeing Special Attention Requirements Bulletin 737-28-1363
RB, dated June 2, 2020, uses the phrase ``the Original Issue date of
Requirements Bulletin 737-28-1363 RB,'' this AD requires using ``the
effective date 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)(1) 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
(1) For more information about this AD, contact Chris Baker,
Aerospace Engineer, Propulsion Section, FAA, Seattle ACO Branch,
2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-
3552; email: [email protected].
(2) Service information identified in this AD that is not
incorporated by reference is available at the addresses specified in
paragraphs (k)(3) and (4) of this AD.
(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 Special Attention Requirements Bulletin 737-28-1363
RB, dated June 2, 2020.
(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 [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on June 3, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2021-13125 Filed 6-23-21; 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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