Airworthiness Directives; The Boeing Company Airplanes, 33112-33116 [2021-13097]
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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.
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(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
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(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
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Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations
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: Julie
Linn, Aerospace Engineer, Cabin Safety
and Environmental Systems Section,
FAA, Seattle ACO Branch, 2200 South
216th St., Des Moines, WA 98198;
phone and fax: 206–231–3584; email:
Julie.Linn@faa.gov.
SUPPLEMENTARY INFORMATION:
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Background
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 2016–25–29,
Amendment 39–18755 (81 FR 94956,
December 27, 2016) (AD 2016–25–29).
AD 2016–25–29 applied to certain The
Boeing Company Model 767–200 and
–300 series airplanes, and required
replacing the cargo compartment
insulation blankets on the left and right
sides with new insulation blankets that
incorporate fire stops. The NPRM
published in the Federal Register on
August 10, 2020 (85 FR 48122). The
NPRM 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. In the
NPRM, the FAA proposed to continue to
require the actions in AD 2016–25–29
for certain airplanes. The NPRM also
proposed to add airplanes to the
applicability and proposed to require 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, the NPRM
also proposed to require 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 a fire
in the bilge area of the cargo
compartment, which if not contained
could lead to a possible smoke and fire
event in the passenger compartment.
Discussion of Final Airworthiness
Directive
Comments
The FAA received comments from
three commenters, including Aviation
Partners Boeing, Delta Air Lines (DAL),
and United Airlines (UAL). The
following presents the comments
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received on the NPRM and the FAA’s
response to each comment.
Effect of Winglets on Accomplishment
of the Proposed Actions
Aviation Partners Boeing stated that
the installation of winglets per
Supplemental Type Certificate (STC)
ST01920SE does not affect the
accomplishment of the manufacturer’s
service instructions.
The FAA agrees with the commenter
that STC ST01920SE does not affect the
accomplishment of the manufacturer’s
service instructions. Therefore, the
installation of STC ST01920SE does not
affect the ability to accomplish the
actions required by this AD. The FAA
has not changed this AD in this regard.
Request To Delay Rule Pending Revised
Referenced Service Information
UAL concurs with the NPRM and
requested that the FAA delay issuance
of the final rule until the referenced
Illustrated Parts Catalog (IPC) and
airplane maintenance manual (AMM)
specified in Boeing Service Bulletin
767–25–0550, Revision 1, dated
December 4, 2019, are revised to ensure
continued airworthiness and safety.
UAL stated that the referenced service
information will provide proper
documentation support to maintain the
insulation blanket changes specified in
Boeing Service Bulletin 767–25–0550,
Revision 1, dated December 4, 2019,
prior to the release of the final rule.
UAL also commented that the revised
referenced service information can
mitigate incorrect repairs and blanket
installation, and minimize future
alternative methods of compliance
(AMOC) requests.
The FAA disagrees with delaying the
final rule. Since the publication of the
NPRM, the operator’s existing IPC and
AMM have been revised and provide
accurate part numbers and corrective
action procedures for missing insulation
blankets. In addition, an operator unable
to accomplish the actions in this AD for
any reason may request approval of an
AMOC under the provisions of
paragraph (i)(1) of this AD, if sufficient
data are submitted to substantiate that
the change would provide an acceptable
level of safety. The FAA has not
changed this AD in this regard.
Request To Identify Proper Insulation
Blankets
UAL expressed concern about the
post-compliance maintenance
configuration using Boeing Service
Bulletin 767–25–0550, Revision 1, dated
December 4, 2019, in the absence of a
revised Boeing 767 IPC (i.e., Boeing 767
IPC sections 25–21–05; 25–52–03; 25–
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33113
52–52; 25–52–62; 25–55–01) to identify
the proper insulation blankets with
integrated fire stops. UAL described
disagreements in the service
information for the identity of the
insulation blanket installations and
corresponding part numbers in the aft
and forward cargo compartment of postmodification airplanes and missing
insulation blankets from certain
appendixes and figures. UAL stated that
it is essential to identify post-service
bulletin configurations in certain Boeing
767 IPCs to ensure that AD compliance
is maintained and to avoid inadvertent
demodification by maintenance
technicians. UAL commented that the
configuration control for the airplane is
the IPC, which maintenance technicians
use for proper part replacement, and
would alert maintenance personnel of
insulation blankets having the
integrated fire stops to ensure continued
airworthiness.
As the FAA stated previously, since
the NPRM was issued, relevant sections
of the IPC have been revised. The
operator’s existing IPC contains the
accurate part numbers and corrects
missing insulation blankets. For
clarification, the part numbers for the
insulation blankets specified in Boeing
Special Attention Service Bulletin 767–
25–0550, dated January 15, 2015, and
Boeing Special Attention Service
Bulletin 767–25–0550, Revision 1, dated
December 4, 2019, are acceptable for
installation; the new part numbers
requires less work to install. The FAA
has revised paragraph (h)(4) of this AD
accordingly.
In addition, Boeing found that the
insulation blankets at certain locations
were not affected by the integrated fire
stop issue that are addressed in Boeing
Special Attention Service Bulletin 767–
25–0550, Revision 1, dated December 4,
2019. Therefore, these insulation
blankets were removed from Boeing
Special Attention Service Bulletin 767–
25–0550, Revision 1, dated December 4,
2019. Boeing Special Attention Service
Bulletin 767–25–0550, Revision 1, dated
December 4, 2019, includes work to reinspect the installation of the insulation
blankets that were installed in Boeing
Special Attention Service Bulletin 767–
25–0550, dated January 15, 2015. Since
those insulation blankets that are not
affected by the fire stop issue were
removed from Boeing Special Attention
Service Bulletin 767–25–0550, Revision
1, dated December 4, 2019, there is no
need for instructions in Revision 1 to
inspect the work that was performed in
Boeing Special Attention Service
Bulletin 767–25–0550, dated January 15,
2015. The FAA has not changed this AD
in this regard.
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Request To Correct the Date of the
Service Information
UAL commented that, in the toolbox
on https://www.myboeingfleet.com,
there are two versions of Boeing Special
Attention Service Bulletin 767–25–
0550, Revision 1: One version is dated
December 4, 2019, and one version is
dated December 5, 2019. UAL also
commented that the header of the
toolbox states that Boeing Special
Attention Service Bulletin 767–25–
0550, Revision 1, dated December 4,
2019, is not the current version. UAL
stated that the proper service
information date needs to be addressed
in the NPRM.
The FAA has confirmed that the
correct date of the service information is
December 4, 2019, and that there is
currently only one version of the service
information cited on https://
www.myboeingfleet.com. The FAA has
not changed this AD in this regard.
Request for Correct Figure Reference
DAL commented that figure 42–A of
Boeing Special Attention Service
Bulletin 767–25–0550, Revision 1, dated
December 4, 2019, refers to item 4
between stations 434 through 456, but it
should be item 3. DAL stated this
citation has been confirmed by Boeing
in Service Request 3–4634446605.
The FAA agrees that the correct
reference for figure 42–A between
stations 434 through 456 of Boeing
Special Attention Service Bulletin 767–
25–0550, Revision 1, dated December 4,
2019, is item 3. In addition, figure 42 is
a RC step. The FAA has added
paragraph (h)(2) of this AD to identify
the correct item number.
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Request To Correct Insulation Blanket
Location
DAL commented that in figure 51 of
Boeing Special Attention Service
Bulletin 767–25–0550, Revision 1, dated
December 4, 2019, there should be an
insulation blanket depicted between
station (STA) 1395 and STA 1417. DAL
also commented that appendixes D, E,
F, G, H, and I of Boeing Special
Attention Service Bulletin 767–25–
0550, Revision 1, dated December 4,
2019, show the insulation blanket part
numbers between STA 1395 and STA
1417. DAL reported that Boeing
confirmed that the insulation blanket
was missing from that figure.
The FAA agrees with the commenter’s
statement. The FAA has added
paragraph (h)(3) of this AD to specify
that Boeing Special Attention Service
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Bulletin 767–25–0550, Revision 1, dated
December 4, 2019, figures 49, 50, and
51, between STA 1395 and STA 1417,
should indicate that an insulation
blanket is installed.
Request To Allow Stoppage Options Due
to the Pandemic
For airplanes that have been in mass
parking due to the worldwide
pandemic, DAL requested clock
stoppage options such as those offered
to operators by the manufacturer for
scheduled maintenance program tasks.
DAL stated that this request is for
airplanes that meet the following
conditions:
• Airplanes that are currently
undergoing storage, or airplanes that
will enter storage during the compliance
time of the proposed AD.
• Airplanes that were preserved with
instructions in close reference to the
AMM procedures.
DAL also commented that an airplane
in a preserved state does not experience
the following risk factors that are taken
into consideration for the proposed AD:
• Passenger Safety: The newly
installed insulation blankets are meant
to prevent smoke from migrating behind
the cargo compartment sidewall liners
and upward into the main cabin, where
it could affect passengers. If the airplane
does not have passengers during the
time in which it is preserved, there is no
increased risk to the public.
• Potential fire in the cargo
compartments: Since the airplane is not
in operation, there is no cargo being
stored in the cargo compartments,
meaning it is highly unlikely that there
will be a fire initiated to cause smoke.
In addition, DAL asserted that the
safety risk associated with the inferior
insulation blankets installed on the
airplane is either a small consideration
or not a consideration at all in the
calculation of overall fleet risk because
the concern is not with degradation of
insulation blanket material, or any other
factor in which an increase in
compliance time would increase the
risk.
The FAA disagrees with having
stoppage options due to the unsafe
condition. In developing an appropriate
compliance time, the FAA considered
the safety implications, parts
availability, and normal maintenance
schedules for timely accomplishment of
the actions in this AD. Further, the FAA
arrived at the proposed compliance time
with Boeing’s concurrence. It is difficult
to plan for every possible storage
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scenario, and currently, the FAA does
not have procedures that would address
every possible scenario to ensure that all
airplanes will be addressed in a timely
manner once the airplanes are back in
service. If an operator is unable to
accomplish the actions in this AD for
whatever reason or has the airplane in
storage, it may request approval of an
AMOC under the provisions of
paragraph (i)(1) of this AD, if sufficient
data are submitted to substantiate that
the change would provide an acceptable
level of safety. 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, and any
other changes described previously, 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 Service Bulletin 767–25–
0550, Revision 1, dated December 4,
2019. The service information describes
procedures for replacement of cargo
compartment insulation blankets
between stringers 29 and 33, on the left
and right sides, with new insulation
blankets that incorporate fire stops; an
inspection to determine the insulation
blanket part number installed between
stringers 29 and 33, on the left and right
sides; a general visual inspection of the
replacement insulation blankets
between stringers 29 and 33, on the left
and right sides to determine if the
insulation blankets are in serviceable
condition and correctly installed; and
applicable on-condition actions. Oncondition actions include repair,
replacement, and correction of
insulation blanket installations. 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 329 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
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33115
ESTIMATED COSTS FOR REQUIRED ACTIONS
Action
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
Replacement (retained actions from
AD 2016-25-29).
Inspections and replacements (new
proposed action).
Up to 54 work-hours × $85 per hour
= Up to $4,590.
Up to 62 work-hour × $85 per hour =
Up to $5,270.
(*)
Up to $4,590 ........
Up to $1,510,110.
Up to $35,900
Up to $41,170 ......
Up to $13,944,530.
* The FAA has received no definitive data that would enable providing parts cost estimates for the retained actions specified in this AD.
The FAA has received no definitive
data that would enable us to provide
cost estimates for the on-condition
actions specified in this AD.
According to the manufacturer, some
of the costs of this AD may be covered
under warranty, thereby reducing the
cost impact on affected operators. The
FAA does not control warranty coverage
for affected operators. As a result, the
FAA has included all available costs in
our cost estimate.
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.
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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
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under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
cabin. The FAA is issuing this AD to address
a fire in the bilge area of the cargo
compartment, which if not contained could
lead to a possible smoke and fire event in the
passenger compartment.
(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
paragraph 1.E., ‘‘Compliance,’’ of Boeing
Special Attention Service Bulletin 767–25–
0550, Revision 1, dated December 4, 2019, do
all applicable actions identified as ‘‘RC’’
(required for compliance) in, and in
accordance with, the Accomplishment
Instructions of Boeing Special Attention
Service Bulletin 767–25–0550, Revision 1,
dated December 4, 2019.
(d) Subject
Air Transport Association (ATA) of
America Code 25, Equipment/furnishings.
(h) Exceptions and Clarifications to Service
Information Specifications
(1) Where Boeing Special Attention Service
Bulletin 767–25–0550, Revision 1, dated
December 4, 2019, uses the phrase ‘‘the
Revision 1 date of this service bulletin,’’ this
AD requires using ‘‘the effective date of this
AD.’’
(2) Where Figure 42–A of Boeing Special
Attention Service Bulletin 767–25–0550,
Revision 1, dated December 4, 2019,
identifies item 4 between stations 434
through 456, the correct item between
stations 434 through 456 is item 3.
(3) Figures 49, 50, and 51 of Boeing Special
Attention Service Bulletin 767–25–0550,
Revision 1, dated December 4, 2019, are
missing the depiction of an insulation
blanket, and an installation blanket must be
installed between station (STA) 1395 and
1417.
(4) The part numbers for the insulation
blankets specified in Boeing Special
Attention Service Bulletin 767–25–0550,
dated January 15, 2015, and Boeing Special
Attention Service Bulletin 767–25–0550,
Revision 1, dated December 4, 2019, are
acceptable for installation; the new part
numbers specified in Boeing Special
Attention Service Bulletin 767–25–0550,
Revision 1, dated December 4, 2019, require
less work to install.
(e) Unsafe Condition
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
(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
2. The FAA amends § 39.13 by:
a. Removing Airworthiness Directive
(AD) 2016–25–29, Amendment 39–
18755 (81 FR 94956, December 27,
2016); and
■ b. Adding the following new AD:
■
■
2021–12–11 The Boeing Company:
Amendment 39–21598; Docket No.
FAA–2020–0680; Project Identifier
2020–NM–079–AD.
(a) Effective Date
This airworthiness directive (AD) is
effective July 29, 2021.
(b) Affected ADs
This AD replaces AD 2016–25–29,
Amendment 39–18755 (81 FR 94956,
December 27, 2016) (AD 2016–25–29).
(c) Applicability
This AD applies to The Boeing Company
Model 767–200, –300, –300F, and –400ER
series airplanes, certificated in any category,
as identified in Boeing Special Attention
Service Bulletin 767–25–0550, Revision 1,
dated December 4, 2019.
PO 00000
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Federal Register / Vol. 86, No. 119 / Thursday, June 24, 2021 / Rules and Regulations
principal inspector or local Flight Standards
District Office, as appropriate. If sending
information directly to the manager of the
certification office, send it to the attention of
the person identified in paragraph (j) of this
AD. Information may be emailed to: 9-ANMSeattle-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 local flight standards district office/
certificate holding district 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.
(4) AMOCs approved previously for AD
2016–25–29 are approved as AMOCs for the
corresponding provisions of Boeing Special
Attention Service Bulletin 767–25–0550,
Revision 1, dated December 4, 2019, that are
required by paragraph (g) of this AD.
(5) For service information that contains
steps that are labeled as Required for
Compliance (RC), the provisions of
paragraphs (i)(5)(i) and (ii) of this AD apply.
(i) The steps labeled as RC, including
substeps under an RC step and any figures
identified in an RC step, must be done to
comply with the AD. If a step or substep is
labeled ‘‘RC Exempt,’’ then the RC
requirement is removed from that step or
substep. An AMOC is required for any
deviations to RC steps, including substeps
and identified figures.
(ii) Steps not labeled as RC may be
deviated from using accepted methods in
accordance with the operator’s maintenance
or inspection program without obtaining
approval of an AMOC, provided the RC steps,
including substeps and identified figures, can
still be done as specified, and the airplane
can be put back in an airworthy condition.
khammond on DSKJM1Z7X2PROD with RULES
(j) Related Information
For more information about this AD,
contact Julie Linn, Aerospace Engineer,
Cabin Safety and Environmental Systems
Section, FAA, Seattle ACO Branch, 2200
South 216th St., Des Moines, WA 98198;
phone and fax: 206–231–3584; email:
Julie.Linn@faa.gov.
(k) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) of the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
(2) You must use this service information
as applicable to do the actions required by
this AD, unless the AD specifies otherwise.
(i) Boeing Special Attention Service
Bulletin 767–25–0550, Revision 1, dated
December 4, 2019.
(ii) [Reserved]
(3) For service information identified in
this AD, contact Boeing Commercial
VerDate Sep<11>2014
16:01 Jun 23, 2021
Jkt 253001
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.
Issued on June 3, 2021.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2021–13097 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–2020–1028; Project
Identifier AD–2020–00978–T; Amendment
39–21599; AD 2021–12–12]
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 all The
Boeing Company Model 717–200
airplanes. This AD was prompted by a
report of discrepant spoiler assemblies,
which have the wrong splice bar
installed and lack reinforcing doublers,
and by reports that some splice bars
were shipped for installation on Model
717–200 airplanes, although they were
not eligible for installation on Model
717–200 airplanes and were identified
incorrectly with the Model 717–200
splice bar part number. This AD
requires a one-time inspection of the
left- and right-wing inboard and
outboard spoiler assemblies, for the
correct configuration of the splice bar
and doublers, and repair or replacement
if necessary. 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
SUMMARY:
PO 00000
Frm 00036
Fmt 4700
Sfmt 4700
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–2020–
1028.
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2020–1028; 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:
Mohit Garg, Aerospace Engineer,
Airframe Section, FAA, Los Angeles
ACO Branch, 3960 Paramount
Boulevard, Lakewood, CA 90712–4137;
phone: 562–627–5264; fax: 562–627–
5210; email: mohit.garg@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 all The Boeing Company Model
717–200 airplanes. The NPRM
published in the Federal Register on
December 29, 2020 (85 FR 85559). The
NPRM was prompted by a report of
discrepant spoiler assemblies, which
have the wrong splice bar installed and
lack reinforcing doublers, and by reports
that some splice bars were shipped for
installation on Model 717–200
airplanes, although they were not
eligible for installation on Model 717–
200 airplanes and were identified
incorrectly with the Model 717–200
splice bar part number. In the NPRM,
the FAA proposed to require a one-time
inspection of the left- and right-wing
inboard and outboard spoiler assemblies
for the correct splice bar and doublers
E:\FR\FM\24JNR1.SGM
24JNR1
Agencies
[Federal Register Volume 86, Number 119 (Thursday, June 24, 2021)]
[Rules and Regulations]
[Pages 33112-33116]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2021-13097]
-----------------------------------------------------------------------
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
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: 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.
DATES: 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.
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
[[Page 33113]]
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: Julie Linn, Aerospace Engineer, Cabin
Safety and Environmental Systems Section, FAA, Seattle ACO Branch, 2200
South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3584;
email: [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 to supersede AD 2016-25-29, Amendment 39-18755 (81 FR
94956, December 27, 2016) (AD 2016-25-29). AD 2016-25-29 applied to
certain The Boeing Company Model 767-200 and -300 series airplanes, and
required replacing the cargo compartment insulation blankets on the
left and right sides with new insulation blankets that incorporate fire
stops. The NPRM published in the Federal Register on August 10, 2020
(85 FR 48122). The NPRM 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. In
the NPRM, the FAA proposed to continue to require the actions in AD
2016-25-29 for certain airplanes. The NPRM also proposed to add
airplanes to the applicability and proposed to require 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, the NPRM also
proposed to require 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 a fire in the bilge area of the cargo compartment, which if not
contained could lead to a possible smoke and fire event in the
passenger compartment.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from three commenters, including Aviation
Partners Boeing, Delta Air Lines (DAL), and United Airlines (UAL). The
following presents the comments received on the NPRM and the FAA's
response to each comment.
Effect of Winglets on Accomplishment of the Proposed Actions
Aviation Partners Boeing stated that the installation of winglets
per Supplemental Type Certificate (STC) ST01920SE does not affect the
accomplishment of the manufacturer's service instructions.
The FAA agrees with the commenter that STC ST01920SE does not
affect the accomplishment of the manufacturer's service instructions.
Therefore, the installation of STC ST01920SE does not affect the
ability to accomplish the actions required by this AD. The FAA has not
changed this AD in this regard.
Request To Delay Rule Pending Revised Referenced Service Information
UAL concurs with the NPRM and requested that the FAA delay issuance
of the final rule until the referenced Illustrated Parts Catalog (IPC)
and airplane maintenance manual (AMM) specified in Boeing Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019, are revised
to ensure continued airworthiness and safety. UAL stated that the
referenced service information will provide proper documentation
support to maintain the insulation blanket changes specified in Boeing
Service Bulletin 767-25-0550, Revision 1, dated December 4, 2019, prior
to the release of the final rule. UAL also commented that the revised
referenced service information can mitigate incorrect repairs and
blanket installation, and minimize future alternative methods of
compliance (AMOC) requests.
The FAA disagrees with delaying the final rule. Since the
publication of the NPRM, the operator's existing IPC and AMM have been
revised and provide accurate part numbers and corrective action
procedures for missing insulation blankets. In addition, an operator
unable to accomplish the actions in this AD for any reason may request
approval of an AMOC under the provisions of paragraph (i)(1) of this
AD, if sufficient data are submitted to substantiate that the change
would provide an acceptable level of safety. The FAA has not changed
this AD in this regard.
Request To Identify Proper Insulation Blankets
UAL expressed concern about the post-compliance maintenance
configuration using Boeing Service Bulletin 767-25-0550, Revision 1,
dated December 4, 2019, in the absence of a revised Boeing 767 IPC
(i.e., Boeing 767 IPC sections 25-21-05; 25-52-03; 25-52-52; 25-52-62;
25-55-01) to identify the proper insulation blankets with integrated
fire stops. UAL described disagreements in the service information for
the identity of the insulation blanket installations and corresponding
part numbers in the aft and forward cargo compartment of post-
modification airplanes and missing insulation blankets from certain
appendixes and figures. UAL stated that it is essential to identify
post-service bulletin configurations in certain Boeing 767 IPCs to
ensure that AD compliance is maintained and to avoid inadvertent
demodification by maintenance technicians. UAL commented that the
configuration control for the airplane is the IPC, which maintenance
technicians use for proper part replacement, and would alert
maintenance personnel of insulation blankets having the integrated fire
stops to ensure continued airworthiness.
As the FAA stated previously, since the NPRM was issued, relevant
sections of the IPC have been revised. The operator's existing IPC
contains the accurate part numbers and corrects missing insulation
blankets. For clarification, the part numbers for the insulation
blankets specified in Boeing Special Attention Service Bulletin 767-25-
0550, dated January 15, 2015, and Boeing Special Attention Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019, are
acceptable for installation; the new part numbers requires less work to
install. The FAA has revised paragraph (h)(4) of this AD accordingly.
In addition, Boeing found that the insulation blankets at certain
locations were not affected by the integrated fire stop issue that are
addressed in Boeing Special Attention Service Bulletin 767-25-0550,
Revision 1, dated December 4, 2019. Therefore, these insulation
blankets were removed from Boeing Special Attention Service Bulletin
767-25-0550, Revision 1, dated December 4, 2019. Boeing Special
Attention Service Bulletin 767-25-0550, Revision 1, dated December 4,
2019, includes work to re-inspect the installation of the insulation
blankets that were installed in Boeing Special Attention Service
Bulletin 767-25-0550, dated January 15, 2015. Since those insulation
blankets that are not affected by the fire stop issue were removed from
Boeing Special Attention Service Bulletin 767-25-0550, Revision 1,
dated December 4, 2019, there is no need for instructions in Revision 1
to inspect the work that was performed in Boeing Special Attention
Service Bulletin 767-25-0550, dated January 15, 2015. The FAA has not
changed this AD in this regard.
[[Page 33114]]
Request To Correct the Date of the Service Information
UAL commented that, in the toolbox on https://www.myboeingfleet.com, there are two versions of Boeing Special
Attention Service Bulletin 767-25-0550, Revision 1: One version is
dated December 4, 2019, and one version is dated December 5, 2019. UAL
also commented that the header of the toolbox states that Boeing
Special Attention Service Bulletin 767-25-0550, Revision 1, dated
December 4, 2019, is not the current version. UAL stated that the
proper service information date needs to be addressed in the NPRM.
The FAA has confirmed that the correct date of the service
information is December 4, 2019, and that there is currently only one
version of the service information cited on https://www.myboeingfleet.com. The FAA has not changed this AD in this regard.
Request for Correct Figure Reference
DAL commented that figure 42-A of Boeing Special Attention Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019, refers to
item 4 between stations 434 through 456, but it should be item 3. DAL
stated this citation has been confirmed by Boeing in Service Request 3-
4634446605.
The FAA agrees that the correct reference for figure 42-A between
stations 434 through 456 of Boeing Special Attention Service Bulletin
767-25-0550, Revision 1, dated December 4, 2019, is item 3. In
addition, figure 42 is a RC step. The FAA has added paragraph (h)(2) of
this AD to identify the correct item number.
Request To Correct Insulation Blanket Location
DAL commented that in figure 51 of Boeing Special Attention Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019, there should
be an insulation blanket depicted between station (STA) 1395 and STA
1417. DAL also commented that appendixes D, E, F, G, H, and I of Boeing
Special Attention Service Bulletin 767-25-0550, Revision 1, dated
December 4, 2019, show the insulation blanket part numbers between STA
1395 and STA 1417. DAL reported that Boeing confirmed that the
insulation blanket was missing from that figure.
The FAA agrees with the commenter's statement. The FAA has added
paragraph (h)(3) of this AD to specify that Boeing Special Attention
Service Bulletin 767-25-0550, Revision 1, dated December 4, 2019,
figures 49, 50, and 51, between STA 1395 and STA 1417, should indicate
that an insulation blanket is installed.
Request To Allow Stoppage Options Due to the Pandemic
For airplanes that have been in mass parking due to the worldwide
pandemic, DAL requested clock stoppage options such as those offered to
operators by the manufacturer for scheduled maintenance program tasks.
DAL stated that this request is for airplanes that meet the following
conditions:
Airplanes that are currently undergoing storage, or
airplanes that will enter storage during the compliance time of the
proposed AD.
Airplanes that were preserved with instructions in close
reference to the AMM procedures.
DAL also commented that an airplane in a preserved state does not
experience the following risk factors that are taken into consideration
for the proposed AD:
Passenger Safety: The newly installed insulation blankets
are meant to prevent smoke from migrating behind the cargo compartment
sidewall liners and upward into the main cabin, where it could affect
passengers. If the airplane does not have passengers during the time in
which it is preserved, there is no increased risk to the public.
Potential fire in the cargo compartments: Since the
airplane is not in operation, there is no cargo being stored in the
cargo compartments, meaning it is highly unlikely that there will be a
fire initiated to cause smoke.
In addition, DAL asserted that the safety risk associated with the
inferior insulation blankets installed on the airplane is either a
small consideration or not a consideration at all in the calculation of
overall fleet risk because the concern is not with degradation of
insulation blanket material, or any other factor in which an increase
in compliance time would increase the risk.
The FAA disagrees with having stoppage options due to the unsafe
condition. In developing an appropriate compliance time, the FAA
considered the safety implications, parts availability, and normal
maintenance schedules for timely accomplishment of the actions in this
AD. Further, the FAA arrived at the proposed compliance time with
Boeing's concurrence. It is difficult to plan for every possible
storage scenario, and currently, the FAA does not have procedures that
would address every possible scenario to ensure that all airplanes will
be addressed in a timely manner once the airplanes are back in service.
If an operator is unable to accomplish the actions in this AD for
whatever reason or has the airplane in storage, it may request approval
of an AMOC under the provisions of paragraph (i)(1) of this AD, if
sufficient data are submitted to substantiate that the change would
provide an acceptable level of safety. 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, and any other changes
described previously, 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 Service Bulletin 767-25-
0550, Revision 1, dated December 4, 2019. The service information
describes procedures for replacement of cargo compartment insulation
blankets between stringers 29 and 33, on the left and right sides, with
new insulation blankets that incorporate fire stops; an inspection to
determine the insulation blanket part number installed between
stringers 29 and 33, on the left and right sides; a general visual
inspection of the replacement insulation blankets between stringers 29
and 33, on the left and right sides to determine if the insulation
blankets are in serviceable condition and correctly installed; and
applicable on-condition actions. On-condition actions include repair,
replacement, and correction of insulation blanket installations. 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 329 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
[[Page 33115]]
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost per product operators
----------------------------------------------------------------------------------------------------------------
Replacement (retained actions Up to 54 work-hours (\*\) Up to $4,590....... Up to $1,510,110.
from AD 2016[dash]25[dash]29). x $85 per hour =
Up to $4,590.
Inspections and replacements Up to 62 work-hour Up to $35,900 Up to $41,170...... Up to $13,944,530.
(new proposed action). x $85 per hour =
Up to $5,270.
----------------------------------------------------------------------------------------------------------------
* The FAA has received no definitive data that would enable providing parts cost estimates for the retained
actions specified in this AD.
The FAA has received no definitive data that would enable us to
provide cost estimates for the on-condition actions specified in this
AD.
According to the manufacturer, some of the costs of this AD may be
covered under warranty, thereby reducing the cost impact on affected
operators. The FAA does not control warranty coverage for affected
operators. As a result, the FAA has included all available costs in our
cost estimate.
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:
0
a. Removing Airworthiness Directive (AD) 2016-25-29, Amendment 39-18755
(81 FR 94956, December 27, 2016); and
0
b. Adding the following new AD:
2021-12-11 The Boeing Company: Amendment 39-21598; Docket No. FAA-
2020-0680; Project Identifier 2020-NM-079-AD.
(a) Effective Date
This airworthiness directive (AD) is effective July 29, 2021.
(b) Affected ADs
This AD replaces AD 2016-25-29, Amendment 39-18755 (81 FR 94956,
December 27, 2016) (AD 2016-25-29).
(c) Applicability
This AD applies to The Boeing Company Model 767-200, -300, -
300F, and -400ER series airplanes, certificated in any category, as
identified in Boeing Special Attention Service Bulletin 767-25-0550,
Revision 1, dated December 4, 2019.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
furnishings.
(e) Unsafe Condition
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. The FAA
is issuing this AD to address a fire in the bilge area of the cargo
compartment, which if not contained could lead to a possible smoke
and fire event in the passenger compartment.
(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 paragraph 1.E., ``Compliance,'' of
Boeing Special Attention Service Bulletin 767-25-0550, Revision 1,
dated December 4, 2019, do all applicable actions identified as
``RC'' (required for compliance) in, and in accordance with, the
Accomplishment Instructions of Boeing Special Attention Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019.
(h) Exceptions and Clarifications to Service Information Specifications
(1) Where Boeing Special Attention Service Bulletin 767-25-0550,
Revision 1, dated December 4, 2019, uses the phrase ``the Revision 1
date of this service bulletin,'' this AD requires using ``the
effective date of this AD.''
(2) Where Figure 42-A of Boeing Special Attention Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019, identifies
item 4 between stations 434 through 456, the correct item between
stations 434 through 456 is item 3.
(3) Figures 49, 50, and 51 of Boeing Special Attention Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019, are
missing the depiction of an insulation blanket, and an installation
blanket must be installed between station (STA) 1395 and 1417.
(4) The part numbers for the insulation blankets specified in
Boeing Special Attention Service Bulletin 767-25-0550, dated January
15, 2015, and Boeing Special Attention Service Bulletin 767-25-0550,
Revision 1, dated December 4, 2019, are acceptable for installation;
the new part numbers specified in Boeing Special Attention Service
Bulletin 767-25-0550, Revision 1, dated December 4, 2019, require
less work to install.
(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
[[Page 33116]]
principal inspector or local Flight Standards District 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 local flight standards district office/certificate holding
district 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.
(4) AMOCs approved previously for AD 2016-25-29 are approved as
AMOCs for the corresponding provisions of Boeing Special Attention
Service Bulletin 767-25-0550, Revision 1, dated December 4, 2019,
that are required by paragraph (g) of this AD.
(5) For service information that contains steps that are labeled
as Required for Compliance (RC), the provisions of paragraphs
(i)(5)(i) and (ii) of this AD apply.
(i) The steps labeled as RC, including substeps under an RC step
and any figures identified in an RC step, must be done to comply
with the AD. If a step or substep is labeled ``RC Exempt,'' then the
RC requirement is removed from that step or substep. An AMOC is
required for any deviations to RC steps, including substeps and
identified figures.
(ii) Steps not labeled as RC may be deviated from using accepted
methods in accordance with the operator's maintenance or inspection
program without obtaining approval of an AMOC, provided the RC
steps, including substeps and identified figures, can still be done
as specified, and the airplane can be put back in an airworthy
condition.
(j) Related Information
For more information about this AD, contact Julie Linn,
Aerospace Engineer, Cabin Safety and Environmental Systems Section,
FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198;
phone and fax: 206-231-3584; 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 Special Attention Service Bulletin 767-25-0550,
Revision 1, dated December 4, 2019.
(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. 2021-13097 Filed 6-23-21; 8:45 am]
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