Airworthiness Directives; The Boeing Company Airplanes, 33110-33112 [2021-13125]
Download as PDF
33110
Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations
(a) Effective Date
This airworthiness directive (AD) is
effective July 29, 2021.
(b) Affected Airworthiness Directives
None.
(c) Applicability
This AD applies to Airbus Helicopters
Deutschland GmbH (AHD) Model MBB–BK
117 D–2 helicopters, certificated in any
category, having an affected part as defined
in European Union Aviation Safety Agency
(EASA) AD 2019–0198, dated August 15,
2019 (EASA AD 2019–0198).
(d) Subject
Joint Aircraft System Component (JASC)
Code 2700, Flight Control System.
(k) Related Information
(e) Reason
This AD was prompted by a short circuit
in a yaw trim actuator connector that
occurred during production electrical tests.
Subsequent investigations determined that a
sharp edge in the wire harness trim
connector backshell damaged the wiring
insulation. The FAA is issuing this AD to
address an unsafe condition that could result
in yaw or pitch trim runaway and subsequent
loss of control of the helicopter.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Requirements
Except as specified in paragraph (h) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with EASA AD 2019–0198.
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(h) Exceptions to EASA AD 2019–0198
(1) Where EASA AD 2019–0198 refers to its
effective date, this AD requires using the
effective date of this AD.
(2) Where paragraph (1) of EASA AD 2019–
0198 specifies to replace each affected part
with a serviceable part within 9 months, this
AD requires replacing each affected part with
a serviceable part within 30 hours time-inservice after the effective date of this AD.
(3) Although the service information
referenced in EASA AD 2019–0198 specifies
to discard certain parts, this AD requires
removing those parts from service.
(4) Where the service information
referenced in EASA AD 2019–0198 specifies
to use tooling, equivalent tooling may be
used.
(5) Paragraph (2) of EASA AD 2019–0198
does not apply to this AD; this AD requires
compliance with paragraph (i) of this AD.
(6) The ‘‘Remarks’’ section of EASA AD
2019–0198 does not apply to this AD.
(i) Parts Installation Prohibition
As of the effective date of this AD, do not
install a wire harness trim connector
backshell identified in paragraph (c) of this
AD on any helicopter.
(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, International Validation
Branch, FAA, has the authority to approve
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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 local
Flight Standards District Office, as
appropriate. If sending information directly
to the manager of the International Validation
Branch, send it to the attention of the person
identified in paragraph (k) of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
For more information about this AD,
contact Katherine Venegas, Aviation Safety
Engineer, Los Angeles ACO Branch,
Compliance & Airworthiness Division, FAA,
3960 Paramount Blvd., Lakewood, CA 90712;
telephone (562) 627–5353; email
katherine.venegas@faa.gov.
(l) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless this AD specifies otherwise.
(i) European Union Aviation Safety Agency
(EASA) AD 2019–0198, dated August 15,
2019.
(ii) [Reserved]
(3) For EASA AD 2019–0198, contact the
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet
www.easa.europa.eu. You may find this
EASA AD on the EASA website at https://
ad.easa.europa.eu.
(4) You may view this service information
at the FAA, Office of the Regional Counsel,
Southwest Region, 10101 Hillwood Pkwy.,
Room 6N–321, Fort Worth, TX 76177. For
information on the availability of this
material at the FAA, call (817) 222–5110.
This material may be found in the AD docket
on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2021–0256.
(5) You may view this material that is
incorporated by reference at the National
Archives and Records Administration
(NARA). For information on the availability
of this material at NARA, email fedreg.legal@
nara.gov, or go to https://www.archives.gov/
federal-register/cfr/ibr-locations.html.
Issued on May 28, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2021–13127 Filed 6–23–21; 8:45 am]
BILLING CODE 4910–13–P
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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
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
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.
SUMMARY:
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
E:\FR\FM\24JNR1.SGM
24JNR1
33111
Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations
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: christopher.r.baker@
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 737–8 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
Action
Labor cost
Installation and software check ......................
3 work-hour × $85 per 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.
khammond on DSKJM1Z7X2PROD with RULES
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.
VerDate Sep<11>2014
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Jkt 253001
Cost per
product
Parts cost
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.
$0
Cost on U.S.
operators
$255
$16,830
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.
§ 39.13
[Amended]
2. The FAA amends § 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.
List of Subjects in 14 CFR Part 39
(c) Applicability
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
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.
The Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
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(d) Subject
Air Transport Association (ATA) of
America Code 28, Fuel.
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24JNR1
33112
Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations
(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.
deviation must meet the certification basis of
the airplane, and the approval must
specifically refer to this AD.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(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 fedreg.legal@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
(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.
khammond on DSKJM1Z7X2PROD with RULES
(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:
9-ANM-Seattle-ACO-AMOC-Requests@
faa.gov.
(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
VerDate Sep<11>2014
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Jkt 253001
(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: christopher.r.baker@faa.gov.
(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.
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
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–0680; Project
Identifier 2020–NM–079–AD; Amendment
39–21598; AD 2021–12–11]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
AGENCY:
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ACTION:
Final rule.
The FAA is superseding
Airworthiness Directive (AD) 2016–25–
29, which applied to certain The Boeing
Company Model 767–200 and –300
series airplanes. AD 2016–25–29
required replacing the cargo
compartment insulation blankets on the
left and right sides with new insulation
blankets that incorporate fire stops. This
AD was prompted by a report of a fire
in the bilge area of the cargo
compartment that burned through the
insulation blankets that were intended
to prevent smoke from migrating behind
the cargo compartment sidewall liners
and upward into the main cabin. This
AD continues to require the actions in
AD 2016–25–29 for certain airplanes.
This AD also adds airplanes to the
applicability and requires a general
visual inspection of the replacement
insulation blankets to determine if the
blankets are in serviceable condition
and correctly installed, and applicable
on-condition actions. For certain
airplanes, this AD also requires an
inspection to determine the insulation
blanket part number installed;
replacement of additional insulation
blankets; and applicable on-condition
actions. The FAA is issuing this AD to
address the unsafe condition on these
products.
SUMMARY:
This AD is effective July 29,
2021.
The Director of the Federal Register
approved the incorporation by reference
of a certain publications 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–2020–
0680.
DATES:
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2020–0680; 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
E:\FR\FM\24JNR1.SGM
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Agencies
[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]
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