Airworthiness Directives; The Boeing Company Airplanes, 2532-2534 [2022-00585]
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2532
Federal Register / Vol. 87, No. 11 / Tuesday, January 18, 2022 / Rules and Regulations
a yaw pedal adjuster, which could result in
reduced yaw 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, European Union Aviation
Safety Agency (EASA) AD 2021–0199, dated
August 27, 2021 (EASA AD 2021–0199).
(h) Exceptions to EASA AD 2021–0199
(1) Where EASA AD 2021–0199 refers to
flight hours, this AD requires using hours
time-in-service.
(2) Where EASA AD 2021–0199 refers to its
effective date, this AD requires using the
effective date of this AD.
(3) Where the service information
referenced in EASA AD 2021–0199 specifies
discarding certain parts, this AD requires
removing those parts from service.
(4) This AD does not mandate compliance
with the ‘‘Remarks’’ section of EASA AD
2021–0199.
(i) No Reporting Requirement
Although the service information
referenced in EASA AD 2021–0199 specifies
to submit certain information to the
manufacturer, this AD does not include that
requirement.
(j) Special Flight Permit
Special flight permits, as described in 14
CFR 21.197 and 21.199, are prohibited.
khammond on DSKJM1Z7X2PROD with RULES
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, International Validation
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 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 (l) 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.
(l) Related Information
For more information about this AD,
contact Kristi Bradley, Program Manager,
COS Program Management Section,
Operational Safety Branch, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177;
telephone (817) 222–5485; email
kristin.bradley@faa.gov.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference of
the service information listed in this
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51.
VerDate Sep<11>2014
16:23 Jan 14, 2022
Jkt 256001
(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 2021–0199, dated August 27,
2021.
(ii) [Reserved]
(3) For EASA AD 2021–0199, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; internet
www.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
at https://www.regulations.gov by searching
for and locating Docket No. FAA–2021–0570.
(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
fr.inspection@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective February 22,
2022.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of February 22, 2022.
ADDRESSES: For service information
identified in this final rule, contact
Boeing Commercial Airplanes,
Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC
110–SK57, Seal Beach, CA 90740–5600;
telephone 562–797–1717; internet
https://www.myboeingfleet.com. You
may view this service information at the
FAA, Airworthiness Products Section,
Operational Safety Branch, 2200 South
216th St., Des Moines, WA. For
information on the availability of this
material at the FAA, call 206–231–3195.
It is also available at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2021–
0794.
Issued on December 17, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–0794; 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: 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: 206–231–3684; email:
julie.linn@faa.gov.
SUPPLEMENTARY INFORMATION:
The FAA is adopting a new
airworthiness directive (AD) for certain
The Boeing Company Model 747–400,
–400D, and –400F series airplanes. This
AD was prompted by reports of burned
Boeing Material Specification (BMS) 8–
39 urethane foam, and a report from the
airplane manufacturer that airplanes
were assembled with seals throughout
various areas of the airplane (including
flight deck and cargo compartments)
made of BMS 8–39 urethane foam, a
material with fire-retardant properties
that deteriorate with age. This AD
requires replacing the system tube/wire
seals made of BMS 8–39 urethane foam
in certain areas of the airplane. The
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 747–400, –400D, and –400F
series airplanes. The NPRM published
in the Federal Register on October 14,
2021 (86 FR 57081). The NPRM was
prompted by reports of burned BMS 8–
39 urethane foam, and a report from the
airplane manufacturer that airplanes
were assembled with seals throughout
various areas of the airplane (including
flight deck and cargo compartments)
made of BMS 8–39 urethane foam, a
material with fire-retardant properties
[FR Doc. 2022–00757 Filed 1–14–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0794; Project
Identifier AD–2021–00400–T; Amendment
39–21869; AD 2021–26–10]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
AGENCY:
SUMMARY:
PO 00000
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Federal Register / Vol. 87, No. 11 / Tuesday, January 18, 2022 / Rules and Regulations
that deteriorate with age. In the NPRM,
the FAA proposed to require replacing
the system tube/wire seals made of BMS
8–39 urethane foam in certain areas of
the airplane. The FAA is issuing this AD
to prevent failure of the urethane seals
to maintain sufficient Halon
concentrations in the cargo
compartments to extinguish or contain
fire or smoke, and to prevent
penetration of fire or smoke in areas of
the airplane that are difficult to access
for fire and smoke detection or
suppression.
International (ALPA), and two
individuals, who supported the NPRM
without change.
Discussion of Final Airworthiness
Directive
The FAA reviewed Boeing Special
Attention Service Bulletin 747–25–
3381, Revision 3, dated February 19,
2021. This service information specifies
procedures for replacing BMS 8–39
urethane foam seals with BMS 1–68
Comments
The FAA received comments from
Boeing, the Air Line Pilots Association,
silicone foam rubber seals (including
doing a general visual inspection of the
foam for any tube or wire penetrations
and sealing any penetrations that go
through the insulation blankets). This
service information adds the work
instructions for Group 11, Configuration
2; Group 13 and 14, Configuration 4;
and Group 16, 17, and 19, Configuration
5 airplanes.
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.
Conclusion
The FAA reviewed the relevant data
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
Costs of Compliance
The FAA estimates that this AD
affects 131 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
ESTIMATED COSTS
Parts
cost
Action
Labor cost
Replacement (including GVI) ........................
Up to 32 work-hours × $85 per hour = Up to
$2,720.
*$
Cost per
product
Up to $2,720 .......
Cost on U.S.
operators
Up to $356,320.
khammond on DSKJM1Z7X2PROD with RULES
* The FAA has received no definitive data on which to base the parts cost estimates for this AD.
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.
(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.
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:
■
VerDate Sep<11>2014
16:23 Jan 14, 2022
Jkt 256001
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]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2021–26–10 The Boeing Company:
Amendment 39–21869; Docket No.
FAA–2021–0794; Project Identifier AD–
2021–00400–T.
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
(a) Effective Date
This airworthiness directive (AD) is
effective February 22, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company
Model 747–400, –400D, and –400F series
airplanes, certificated in any category,
identified as Group 11, Configuration 2;
Group 13 and 14, Configuration 4; and Group
16, 17, and 19, Configuration 5, in Boeing
Special Attention Service Bulletin 747–25–
3381, Revision 3, dated February 19, 2021.
(d) Subject
Air Transport Association (ATA) of
America Code 25, Equipment/Furnishings.
(e) Unsafe Condition
This AD was prompted by reports of
burned Boeing Material Specification (BMS)
8–39 urethane foam, and a report from the
airplane manufacturer that airplanes were
assembled with seals throughout various
areas of the airplane (including flight deck
and cargo compartments) made of BMS 8–39
urethane foam, a material with fire-retardant
properties that deteriorate with age. The FAA
is issuing this AD to prevent failure of the
urethane seals to maintain sufficient Halon
concentrations in the cargo compartments to
extinguish or contain fire or smoke, and to
prevent penetration of fire or smoke in areas
of the airplane that are difficult to access for
fire and smoke detection or suppression.
E:\FR\FM\18JAR1.SGM
18JAR1
2534
Federal Register / Vol. 87, No. 11 / Tuesday, January 18, 2022 / Rules and Regulations
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) BMS 8–39 Urethane Foam Seal
Replacements
Within 72 months after the effective date
of this AD: Replace the BMS 8–39 urethane
foam seals in the forward cargo compartment
system tube/wire (including doing a general
visual inspection of the foam for any tube or
wire penetrations and sealing any
penetrations that go through the insulation
blankets) with BMS 1–68 silicone foam
rubber seals, as applicable, in accordance
with the Accomplishment Instructions of
Boeing Special Attention Service Bulletin
747–25–3381, Revision 3, dated February 19,
2021.
(h) 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 Related Information.
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 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.
khammond on DSKJM1Z7X2PROD with RULES
(i) 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: 206–231–3684; email:
julie.linn@faa.gov.
(j) 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 747–25–3381, Revision 3, dated
February 19, 2021.
(ii) [Reserved]
(3) For service information identified in
this AD, contact Boeing Commercial
VerDate Sep<11>2014
16:23 Jan 14, 2022
Jkt 256001
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,
fr.inspection@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on December 9, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022–00585 Filed 1–14–22; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2021–0609; Project
Identifier AD–2021–00274–T; Amendment
39–21861; AD 2021–26–03]
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
Examining the AD Docket
You may examine the AD docket at
https://www.regulations.gov by
searching for and locating Docket No.
FAA–2021–0609; 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:
Wayne Ha, Aerospace Engineer,
Airframe Section, FAA, Los Angeles
ACO Branch, 3960 Paramount
Boulevard, Lakewood, CA 90712–4137;
phone: 562–627–5238; fax: 562–627–
5210; email: wayne.ha@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA is adopting a new
airworthiness directive (AD) for certain
The Boeing Company Model 737–300,
–400, and –500 series airplanes. This
AD was prompted by an evaluation by
the design approval holder (DAH)
indicating that the frame splice between
certain stringers is subject to
widespread fatigue damage (WFD). This
AD requires an inspection of certain
fuselage frame splices for existing
repairs, repetitive inspections of certain
fuselage frame splices for cracking, and
applicable on-condition actions. The
FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective February 22,
2022.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of February 22, 2022.
ADDRESSES: For service information
identified in this final rule, contact
Boeing Commercial Airplanes,
Attention: Contractual & Data Services
SUMMARY:
(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–
0609.
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 737–300, –400, and –500 series
airplanes. The NPRM published in the
Federal Register on August 24, 2021 (86
FR 47255). The NPRM was prompted by
an evaluation by the DAH indicating
that the frame splice between certain
stringers is subject to WFD. In the
NPRM, the FAA proposed to require an
inspection of certain fuselage frame
splices for existing repairs, repetitive
inspections of certain fuselage frame
splices for cracking, and applicable oncondition actions. The FAA is issuing
this AD to address upper frame cracking
common to the frame splice between
stringer S–13 and S–14, which could
interact with stringer S–14 skin lap
splice lower fastener row cracking in
lower skin and result in an uncontrolled
decompression of the airplane and loss
of structural integrity.
E:\FR\FM\18JAR1.SGM
18JAR1
Agencies
[Federal Register Volume 87, Number 11 (Tuesday, January 18, 2022)]
[Rules and Regulations]
[Pages 2532-2534]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-00585]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2021-0794; Project Identifier AD-2021-00400-T;
Amendment 39-21869; AD 2021-26-10]
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 747-400, -400D, and -400F series
airplanes. This AD was prompted by reports of burned Boeing Material
Specification (BMS) 8-39 urethane foam, and a report from the airplane
manufacturer that airplanes were assembled with seals throughout
various areas of the airplane (including flight deck and cargo
compartments) made of BMS 8-39 urethane foam, a material with fire-
retardant properties that deteriorate with age. This AD requires
replacing the system tube/wire seals made of BMS 8-39 urethane foam in
certain areas of the airplane. The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective February 22, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of February 22,
2022.
ADDRESSES: For service information identified in this final rule,
contact Boeing Commercial Airplanes, Attention: Contractual & Data
Services (C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA
90740-5600; telephone 562-797-1717; internet https://www.myboeingfleet.com. You may view this service information at the
FAA, Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability of
this material at the FAA, call 206-231-3195. It is also available at
https://www.regulations.gov by searching for and locating Docket No.
FAA-2021-0794.
Examining the AD Docket
You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0794; 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: 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: 206-231-3684;
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 747-400, -400D, and -400F series airplanes. The NPRM
published in the Federal Register on October 14, 2021 (86 FR 57081).
The NPRM was prompted by reports of burned BMS 8-39 urethane foam, and
a report from the airplane manufacturer that airplanes were assembled
with seals throughout various areas of the airplane (including flight
deck and cargo compartments) made of BMS 8-39 urethane foam, a material
with fire-retardant properties
[[Page 2533]]
that deteriorate with age. In the NPRM, the FAA proposed to require
replacing the system tube/wire seals made of BMS 8-39 urethane foam in
certain areas of the airplane. The FAA is issuing this AD to prevent
failure of the urethane seals to maintain sufficient Halon
concentrations in the cargo compartments to extinguish or contain fire
or smoke, and to prevent penetration of fire or smoke in areas of the
airplane that are difficult to access for fire and smoke detection or
suppression.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from Boeing, the Air Line Pilots
Association, International (ALPA), and two individuals, who supported
the NPRM without change.
Conclusion
The FAA reviewed the relevant data 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 Service Bulletin 747-25-
3381, Revision 3, dated February 19, 2021. This service information
specifies procedures for replacing BMS 8-39 urethane foam seals with
BMS 1-68 silicone foam rubber seals (including doing a general visual
inspection of the foam for any tube or wire penetrations and sealing
any penetrations that go through the insulation blankets). This service
information adds the work instructions for Group 11, Configuration 2;
Group 13 and 14, Configuration 4; and Group 16, 17, and 19,
Configuration 5 airplanes.
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 131 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Parts
Action Labor cost cost Cost per product Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Replacement (including GVI)... Up to 32 work- * $ Up to $2,720............ Up to $356,320.
hours x $85 per
hour = Up to
$2,720.
----------------------------------------------------------------------------------------------------------------
* The FAA has received no definitive data on which to base the parts cost estimates for this AD.
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:
2021-26-10 The Boeing Company: Amendment 39-21869; Docket No. FAA-
2021-0794; Project Identifier AD-2021-00400-T.
(a) Effective Date
This airworthiness directive (AD) is effective February 22,
2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to The Boeing Company Model 747-400, -400D, and
-400F series airplanes, certificated in any category, identified as
Group 11, Configuration 2; Group 13 and 14, Configuration 4; and
Group 16, 17, and 19, Configuration 5, in Boeing Special Attention
Service Bulletin 747-25-3381, Revision 3, dated February 19, 2021.
(d) Subject
Air Transport Association (ATA) of America Code 25, Equipment/
Furnishings.
(e) Unsafe Condition
This AD was prompted by reports of burned Boeing Material
Specification (BMS) 8-39 urethane foam, and a report from the
airplane manufacturer that airplanes were assembled with seals
throughout various areas of the airplane (including flight deck and
cargo compartments) made of BMS 8-39 urethane foam, a material with
fire-retardant properties that deteriorate with age. The FAA is
issuing this AD to prevent failure of the urethane seals to maintain
sufficient Halon concentrations in the cargo compartments to
extinguish or contain fire or smoke, and to prevent penetration of
fire or smoke in areas of the airplane that are difficult to access
for fire and smoke detection or suppression.
[[Page 2534]]
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) BMS 8-39 Urethane Foam Seal Replacements
Within 72 months after the effective date of this AD: Replace
the BMS 8-39 urethane foam seals in the forward cargo compartment
system tube/wire (including doing a general visual inspection of the
foam for any tube or wire penetrations and sealing any penetrations
that go through the insulation blankets) with BMS 1-68 silicone foam
rubber seals, as applicable, in accordance with the Accomplishment
Instructions of Boeing Special Attention Service Bulletin 747-25-
3381, Revision 3, dated February 19, 2021.
(h) 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 Related Information. 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.
(i) 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: 206-231-3684; email: [email protected].
(j) 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 747-25-3381,
Revision 3, dated February 19, 2021.
(ii) [Reserved]
(3) For service information identified in this AD, contact
Boeing Commercial Airplanes, Attention: Contractual & Data Services
(C&DS), 2600 Westminster Blvd., MC 110-SK57, Seal Beach, CA 90740-
5600; telephone 562-797-1717; internet https://www.myboeingfleet.com.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 2200
South 216th St., Des Moines, WA. For information on the availability
of this material at the FAA, call 206-231-3195.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on December 9, 2021.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-00585 Filed 1-14-22; 8:45 am]
BILLING CODE 4910-13-P