Airworthiness Directives; Gulfstream Aerospace Corporation Airplanes, 31152-31154 [2023-10328]
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31152
Federal Register / Vol. 88, No. 94 / Tuesday, May 16, 2023 / Rules and Regulations
Issued on April 8, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–10333 Filed 5–15–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1486; Project
Identifier AD–2022–01026–T; Amendment
39–22418; AD 2023–08–03]
RIN 2120–AA64
Airworthiness Directives; Gulfstream
Aerospace Corporation Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
Background
The FAA is adopting a new
airworthiness directive (AD) for certain
Gulfstream Aerospace Corporation
Model G–1159A and G–1159B airplanes
and all Model G–IV and GIV–X
airplanes. This AD was prompted by a
report that the ground spoiler actuator
installation does not preclude improper
hydraulic line connections that could
result in unintended asymmetrical
spoiler deployment. This AD requires
incorporating corrective actions that
physically prevent improper connection
of the hydraulic lines to the ground
spoiler actuator. The FAA is issuing this
AD to address the unsafe condition on
these products.
DATES: This AD is effective June 20,
2023.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of June 20, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2022–1486; 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.
Material Incorporated by Reference:
• For service information identified
in this final rule, contact Gulfstream
Aerospace Corporation, Technical
Publications Dept., P.O. Box 2206,
lotter on DSK11XQN23PROD with RULES1
SUMMARY:
VerDate Sep<11>2014
16:03 May 15, 2023
Savannah, GA 31402–2206; telephone
800–810–4853; email pubs@
gulfstream.com; website
gulfstream.com/en/customer-support/.
• 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
regulations.gov under Docket No. FAA–
2022–1486.
FOR FURTHER INFORMATION CONTACT:
Samuel Belete, Aerospace Engineer,
Systems and Equipment Section, FAA,
Atlanta ACO Branch, 1701 Columbia
Avenue, College Park, GA 30337; phone:
404–474–5580; email: 9-ASO-ATLACOADs@faa.gov.
SUPPLEMENTARY INFORMATION:
Jkt 259001
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain Gulfstream Aerospace
Corporation Model G–1159A and G–
1159B airplanes and all Model G–IV and
GIV–X airplanes. The NPRM published
in the Federal Register on November 25,
2022 (87 FR 72422). The NPRM was
prompted by a report, following a fatal
accident involving a Gulfstream Model
G–IV, that the ground spoiler actuator
configuration does not preclude
improper hydraulic line connections
that could result in unintended
asymmetrical spoiler deployment. In the
NPRM, the FAA proposed incorporating
corrective actions that physically
prevent improper connection of the
hydraulic lines to the ground spoiler
actuator. The FAA is issuing this AD to
address improper connection of the
ground spoiler hydraulic lines, which, if
not addressed, could result in
unintended asymmetrical spoiler
deployment leading to loss of control of
the airplane.
Discussion of Final Airworthiness
Directive
Comments
The FAA received comments from the
National Transportation Safety Board
(NTSB). The NTSB supported the NPRM
without change.
The FAA received comments from
Gulfstream Aerospace Corporation. The
following presents the comments
received on the NPRM and the FAA’s
response to each comment.
Request To Clarify Information in the
Preamble
Gulfstream requested that the FAA
revise the description of the incident
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that prompted the NPRM. Gulfstream
requested aligning the SUMMARY with the
Background details in the NPRM to state
that the proposed AD was prompted by
a report that the ground spoiler actuator
installation ‘‘does not preclude’’
improper hydraulic line connections,
instead of stating that the installation
‘‘allows’’ such improper connections.
The FAA agrees with the suggested
revision and has revised the SUMMARY of
this final rule accordingly.
Request To Clarify the Total Affected
Airplanes (Cost of Compliance)
Gulfstream requested that the FAA
revise the Cost of Compliance section of
the NPRM to reflect a total population
of affected airplanes of 1,045. This
includes airplanes of all registries. The
‘‘Cost of Compliance’’ section in the
NPRM identified a total of 550 airplanes
of U.S. Registry as affected.
The FAA does not agree because the
‘‘Cost of Compliance’’ section accounts
for the cost of AD compliance only for
affected airplanes that are certificated by
the FAA and included on the U.S.
Registry. Airplanes registered in other
countries are regulated by their civil
aviation authorities, who may or may
not adopt similar rulemaking. The FAA
has not changed this final rule as a
result of this comment.
Request To Change Compliance Time
Gulfstream requested that the FAA
change the compliance time for Model
G–1159A, G–1159B, and G–IV airplanes
from 18 months after the effective date
of this AD to 18 months from March 3,
2023. Gulfstream stated that if the AD
becomes effective prior to March 3,
2023, it will shorten the FAA and
Gulfstream agreed-on corrective action
timelines, and would increase an
already challenging compliance
window.
The FAA finds it unnecessary to
change the compliance time. The
effective date of this AD is after the
requested reference date of March 3,
2023, so this AD will provide the full 18
months for compliance for those
airplanes.
Additional Change to This Final Rule
Gulfstream has developed and
published service information that will
address the unsafe condition for certain
airplanes identified in this final rule.
This service information is described
under ‘‘Related Service Information
under 1 CFR part 51’’ in this final rule.
After reviewing this service information,
the FAA determined that it is acceptable
to use for compliance with the
requirements of this AD for the
identified airplanes. The FAA has
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Federal Register / Vol. 88, No. 94 / Tuesday, May 16, 2023 / Rules and Regulations
revised the proposed AD to present the
requirements for Model G–1159A, G–
1159B, and G–IV airplanes in paragraph
(g) of this AD, which also identifies this
service information as acceptable for
compliance with the requirements of the
AD for those airplanes. The
requirements for Model GIV–X airplanes
have not changed, and are restated in
new paragraph (h) of this AD. In
addition, the Costs of Compliance
section has been updated to reflect costs
specified in this service information.
Conclusion
The FAA reviewed the relevant data,
considered any comments received, and
determined that air safety requires
adopting this AD as proposed.
Accordingly, the FAA is issuing this AD
to address the unsafe condition on these
products. 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 the following
service information:
• Gulfstream G300 Customer Bulletin
No. 250, dated November 9, 2022
• Gulfstream G400 Customer Bulletin
No. 250, dated November 9, 2022
• Gulfstream GII–GIIB Customer
Bulletin No. 471, dated November 9,
2022
• Gulfstream GIII Customer Bulletin No.
189, dated November 9, 2022
31153
• Gulfstream GIV Customer Bulletin No.
250, dated November 9, 2022
This service information specifies
procedures for replacing the left and
right ground spoiler actuator hydraulic
hoses and associated fittings. These
documents are distinct since they apply
to different Model G–1159A, G–1159B,
and G–IV 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 550 airplanes of U.S. registry.
The FAA estimates the following costs
to comply with this AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Labor cost
Parts cost
Cost per
product
Cost on U.S.
operators
20 work-hours × $85 per hour = $1,700 .....................................................................................
$500
$2,200
$1,210,000
The FAA has included all known
costs in its cost estimate. According to
the manufacturer, however, some or all
of the costs of this AD may be covered
under warranty, thereby reducing the
cost impact on affected operators.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
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.
lotter on DSK11XQN23PROD with RULES1
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.
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
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
16:03 May 15, 2023
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
§ 39.13
Regulatory Findings
VerDate Sep<11>2014
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.
Jkt 259001
2023–08–03 Gulfstream Aerospace
Corporation: Amendment 39–22418;
Docket No. FAA–2022–1486; Project
Identifier AD–2022–01026–T.
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Fmt 4700
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(a) Effective Date
This airworthiness directive (AD) is
effective June 20, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the Gulfstream
Aerospace Corporation airplanes identified
in paragraphs (c)(1) through (4) of this AD,
certificated in any category.
(1) Model G–1159A airplanes having serial
numbers (S/Ns) 385, 387, 388, and 390
through 498 inclusive.
(2) Model G–1159B airplanes having S/Ns
009, 016, 042, 048, 054, 064, 086, 088, 095,
098, 102, 119, 123, 125, 131, 140, 151, 154,
155, 156, 165, 166, 189, 198, 199, 207, 219,
237, 245, 254, 255, and 257.
(3) Model G–IV airplanes, all serial
numbers.
(4) Model GIV–X airplanes, all serial
numbers.
Note 1 to paragraph (c): Some Model G–
IV airplanes are also referred to by the
marketing designations G300, G400, and
GIV–SP.
Note 2 to paragraph (c): Some Model GIV–
X airplanes are also referred to by the
marketing designations G350 and G450.
(d) Subject
Air Transport Association (ATA) of
America Code 27, Flight Controls.
(e) Unsafe Condition
This AD was prompted by a report that a
Gulfstream Model G–IV airplane was
involved in a fatal accident on December 15,
2021, after spoilers deployed in an
asymmetrical manner. The asymmetrical
spoiler deployment resulted in in-flight loss
of control of the airplane. The fatal flight was
E:\FR\FM\16MYR1.SGM
16MYR1
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Federal Register / Vol. 88, No. 94 / Tuesday, May 16, 2023 / Rules and Regulations
the first flight after maintenance actions
where the spoiler hydraulic lines were
improperly connected (reversed) to the
ground spoiler actuator. The ground spoiler
actuator configuration does not preclude
improper hydraulic line connections that
could result in unintended asymmetrical
spoiler deployment. The FAA is issuing this
AD to prevent incorrect connection of the
hydraulic lines to the ground spoiler
actuator. The unsafe condition, if not
addressed, could result in unintended
asymmetrical spoiler deployment leading to
loss of control of the airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions: Model G–1159A, G–
1159B, G–IV
For Model G–1159A, G–1159B, and G–IV
airplanes: Within 18 months after the
effective date of this AD, incorporate
corrective actions (includes replacing a
ground spoiler actuator hydraulic hose and
associated fittings) that physically prevent
improper connection of the hydraulic lines to
the ground spoiler actuator, in accordance
with a method approved by the Manager,
Atlanta ACO Branch, FAA. Accomplishment
of the actions specified in the applicable
service information in paragraphs (g)(1)
through (5) of this AD is acceptable for
compliance with the requirements of this
paragraph.
(1) Gulfstream G300 Customer Bulletin No.
250, dated November 9, 2022.
(2) Gulfstream G400 Customer Bulletin No.
250, dated November 9, 2022.
(3) Gulfstream GII–GIIB Customer Bulletin
No. 471, dated November 9, 2022.
(4) Gulfstream GIII Customer Bulletin No.
189, dated November 9, 2022.
(5) Gulfstream GIV Customer Bulletin No.
250, dated November 9, 2022.
lotter on DSK11XQN23PROD with RULES1
(h) Required Actions: Model GIV–X
For Model GIV–X airplanes: Within 60
months after the effective date of this AD,
incorporate corrective actions (includes
replacing a ground spoiler actuator hydraulic
hose and associated fittings) that physically
prevent improper connection of the
hydraulic lines to the ground spoiler
actuator, in accordance with a method
approved by the Manager, Atlanta ACO
Branch, FAA.
(i) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Atlanta ACO Branch,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. In accordance with
14 CFR 39.19, send your request to your
principal inspector or responsible Flight
Standards Office, as appropriate. If sending
information directly to the manager of the
certification office, send it to the attention of
the person identified in paragraph (j) of this
AD.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
or lacking a principal inspector, the manager
of the responsible Flight Standards Office.
VerDate Sep<11>2014
16:03 May 15, 2023
Jkt 259001
(3) For service information that contains
steps that are labeled as Required for
Compliance (RC), the provisions of
paragraphs (i)(3)(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. 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 Samuel Belete, Aerospace Engineer,
Systems and Equipment Section, FAA,
Atlanta ACO Branch, 1701 Columbia
Avenue, College Park, GA 30337; phone:
404–474–5580; email: 9-ASO-ATLACO-ADs@
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) Gulfstream G300 Customer Bulletin No.
250, dated November 9, 2022.
(ii) Gulfstream G400 Customer Bulletin No.
250, dated November 9, 2022.
(iii) Gulfstream GII–GIIB Customer Bulletin
No. 471, dated November 9, 2022.
(iv) Gulfstream GIII Customer Bulletin No.
189, dated November 9, 2022.
(v) Gulfstream GIV Customer Bulletin No.
250, dated November 9, 2022.
(3) For service information identified in
this AD, contact Gulfstream Aerospace
Corporation, Technical Publications Dept.,
P.O. Box 2206, Savannah, GA 31402–2206;
telephone 800–810–4853; email pubs@
gulfstream.com; website gulfstream.com/en/
customer-support/.
(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:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on April 14, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–10328 Filed 5–15–23; 8:45 am]
BILLING CODE 4910–13–P
PO 00000
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1474; Project
Identifier MCAI–2022–00888–T; Amendment
39–22409; AD 2023–07–07]
RIN 2120–AA64
Airworthiness Directives; MHI RJ
Aviation ULC (Type Certificate
Previously Held by Bombardier, Inc.)
Airplanes
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
MHI RJ Aviation ULC Model CL–600–
2B19 (Regional Jet Series 100 & 440),
CL–600–2C10 (Regional Jet Series 700,
701 & 702), CL–600–2C11 (Regional Jet
Series 550), CL–600–2D15 (Regional Jet
Series 705), CL–600–2D24 (Regional Jet
Series 900), and CL–600–2E25 (Regional
Jet Series 1000) airplanes. This AD was
prompted by reports from the supplier
that sensing elements of the bleed air
leak detection system were
manufactured with insufficient salt fill,
which can result in an inability to detect
hot bleed air leaks. This AD requires
testing of all affected overheat detection
sensing elements of the bleed air leak
detection system, and replacement if
necessary. This AD also prohibits the
installation of affected parts. The FAA
is issuing this AD to address the unsafe
condition on these products.
DATES: This AD is effective June 20,
2023.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of June 20, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2022–1474; 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, the mandatory
continuing airworthiness information
(MCAI), 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.
Material Incorporated by Reference:
• For service information identified
in this final rule, contact MHI RJ
SUMMARY:
E:\FR\FM\16MYR1.SGM
16MYR1
Agencies
[Federal Register Volume 88, Number 94 (Tuesday, May 16, 2023)]
[Rules and Regulations]
[Pages 31152-31154]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-10328]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1486; Project Identifier AD-2022-01026-T;
Amendment 39-22418; AD 2023-08-03]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace Corporation
Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Gulfstream Aerospace Corporation Model G-1159A and G-1159B
airplanes and all Model G-IV and GIV-X airplanes. This AD was prompted
by a report that the ground spoiler actuator installation does not
preclude improper hydraulic line connections that could result in
unintended asymmetrical spoiler deployment. This AD requires
incorporating corrective actions that physically prevent improper
connection of the hydraulic lines to the ground spoiler actuator. The
FAA is issuing this AD to address the unsafe condition on these
products.
DATES: This AD is effective June 20, 2023.
The Director of the Federal Register approved the incorporation by
reference of certain publications listed in this AD as of June 20,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1486; 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.
Material Incorporated by Reference:
For service information identified in this final rule,
contact Gulfstream Aerospace Corporation, Technical Publications Dept.,
P.O. Box 2206, Savannah, GA 31402-2206; telephone 800-810-4853; email
[email protected]; website gulfstream.com/en/customer-support/.
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
regulations.gov under Docket No. FAA-2022-1486.
FOR FURTHER INFORMATION CONTACT: Samuel Belete, Aerospace Engineer,
Systems and Equipment Section, FAA, Atlanta ACO Branch, 1701 Columbia
Avenue, College Park, GA 30337; phone: 404-474-5580; 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 Gulfstream
Aerospace Corporation Model G-1159A and G-1159B airplanes and all Model
G-IV and GIV-X airplanes. The NPRM published in the Federal Register on
November 25, 2022 (87 FR 72422). The NPRM was prompted by a report,
following a fatal accident involving a Gulfstream Model G-IV, that the
ground spoiler actuator configuration does not preclude improper
hydraulic line connections that could result in unintended asymmetrical
spoiler deployment. In the NPRM, the FAA proposed incorporating
corrective actions that physically prevent improper connection of the
hydraulic lines to the ground spoiler actuator. The FAA is issuing this
AD to address improper connection of the ground spoiler hydraulic
lines, which, if not addressed, could result in unintended asymmetrical
spoiler deployment leading to loss of control of the airplane.
Discussion of Final Airworthiness Directive
Comments
The FAA received comments from the National Transportation Safety
Board (NTSB). The NTSB supported the NPRM without change.
The FAA received comments from Gulfstream Aerospace Corporation.
The following presents the comments received on the NPRM and the FAA's
response to each comment.
Request To Clarify Information in the Preamble
Gulfstream requested that the FAA revise the description of the
incident that prompted the NPRM. Gulfstream requested aligning the
SUMMARY with the Background details in the NPRM to state that the
proposed AD was prompted by a report that the ground spoiler actuator
installation ``does not preclude'' improper hydraulic line connections,
instead of stating that the installation ``allows'' such improper
connections.
The FAA agrees with the suggested revision and has revised the
SUMMARY of this final rule accordingly.
Request To Clarify the Total Affected Airplanes (Cost of Compliance)
Gulfstream requested that the FAA revise the Cost of Compliance
section of the NPRM to reflect a total population of affected airplanes
of 1,045. This includes airplanes of all registries. The ``Cost of
Compliance'' section in the NPRM identified a total of 550 airplanes of
U.S. Registry as affected.
The FAA does not agree because the ``Cost of Compliance'' section
accounts for the cost of AD compliance only for affected airplanes that
are certificated by the FAA and included on the U.S. Registry.
Airplanes registered in other countries are regulated by their civil
aviation authorities, who may or may not adopt similar rulemaking. The
FAA has not changed this final rule as a result of this comment.
Request To Change Compliance Time
Gulfstream requested that the FAA change the compliance time for
Model G-1159A, G-1159B, and G-IV airplanes from 18 months after the
effective date of this AD to 18 months from March 3, 2023. Gulfstream
stated that if the AD becomes effective prior to March 3, 2023, it will
shorten the FAA and Gulfstream agreed-on corrective action timelines,
and would increase an already challenging compliance window.
The FAA finds it unnecessary to change the compliance time. The
effective date of this AD is after the requested reference date of
March 3, 2023, so this AD will provide the full 18 months for
compliance for those airplanes.
Additional Change to This Final Rule
Gulfstream has developed and published service information that
will address the unsafe condition for certain airplanes identified in
this final rule. This service information is described under ``Related
Service Information under 1 CFR part 51'' in this final rule. After
reviewing this service information, the FAA determined that it is
acceptable to use for compliance with the requirements of this AD for
the identified airplanes. The FAA has
[[Page 31153]]
revised the proposed AD to present the requirements for Model G-1159A,
G-1159B, and G-IV airplanes in paragraph (g) of this AD, which also
identifies this service information as acceptable for compliance with
the requirements of the AD for those airplanes. The requirements for
Model GIV-X airplanes have not changed, and are restated in new
paragraph (h) of this AD. In addition, the Costs of Compliance section
has been updated to reflect costs specified in this service
information.
Conclusion
The FAA reviewed the relevant data, considered any comments
received, and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these products. 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 the following service information:
Gulfstream G300 Customer Bulletin No. 250, dated November 9,
2022
Gulfstream G400 Customer Bulletin No. 250, dated November 9,
2022
Gulfstream GII-GIIB Customer Bulletin No. 471, dated November
9, 2022
Gulfstream GIII Customer Bulletin No. 189, dated November 9,
2022
Gulfstream GIV Customer Bulletin No. 250, dated November 9,
2022
This service information specifies procedures for replacing the
left and right ground spoiler actuator hydraulic hoses and associated
fittings. These documents are distinct since they apply to different
Model G-1159A, G-1159B, and G-IV 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 550 airplanes of U.S.
registry. The FAA estimates the following costs to comply with this AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
20 work-hours x $85 per hour = $1,700........................ $500 $2,200 $1,210,000
----------------------------------------------------------------------------------------------------------------
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this AD may be covered under warranty, thereby reducing the cost impact
on affected operators.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
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:
2023-08-03 Gulfstream Aerospace Corporation: Amendment 39-22418;
Docket No. FAA-2022-1486; Project Identifier AD-2022-01026-T.
(a) Effective Date
This airworthiness directive (AD) is effective June 20, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the Gulfstream Aerospace Corporation
airplanes identified in paragraphs (c)(1) through (4) of this AD,
certificated in any category.
(1) Model G-1159A airplanes having serial numbers (S/Ns) 385,
387, 388, and 390 through 498 inclusive.
(2) Model G-1159B airplanes having S/Ns 009, 016, 042, 048, 054,
064, 086, 088, 095, 098, 102, 119, 123, 125, 131, 140, 151, 154,
155, 156, 165, 166, 189, 198, 199, 207, 219, 237, 245, 254, 255, and
257.
(3) Model G-IV airplanes, all serial numbers.
(4) Model GIV-X airplanes, all serial numbers.
Note 1 to paragraph (c): Some Model G-IV airplanes are also
referred to by the marketing designations G300, G400, and GIV-SP.
Note 2 to paragraph (c): Some Model GIV-X airplanes are also
referred to by the marketing designations G350 and G450.
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
Controls.
(e) Unsafe Condition
This AD was prompted by a report that a Gulfstream Model G-IV
airplane was involved in a fatal accident on December 15, 2021,
after spoilers deployed in an asymmetrical manner. The asymmetrical
spoiler deployment resulted in in-flight loss of control of the
airplane. The fatal flight was
[[Page 31154]]
the first flight after maintenance actions where the spoiler
hydraulic lines were improperly connected (reversed) to the ground
spoiler actuator. The ground spoiler actuator configuration does not
preclude improper hydraulic line connections that could result in
unintended asymmetrical spoiler deployment. The FAA is issuing this
AD to prevent incorrect connection of the hydraulic lines to the
ground spoiler actuator. The unsafe condition, if not addressed,
could result in unintended asymmetrical spoiler deployment leading
to loss of control of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions: Model G-1159A, G-1159B, G-IV
For Model G-1159A, G-1159B, and G-IV airplanes: Within 18 months
after the effective date of this AD, incorporate corrective actions
(includes replacing a ground spoiler actuator hydraulic hose and
associated fittings) that physically prevent improper connection of
the hydraulic lines to the ground spoiler actuator, in accordance
with a method approved by the Manager, Atlanta ACO Branch, FAA.
Accomplishment of the actions specified in the applicable service
information in paragraphs (g)(1) through (5) of this AD is
acceptable for compliance with the requirements of this paragraph.
(1) Gulfstream G300 Customer Bulletin No. 250, dated November 9,
2022.
(2) Gulfstream G400 Customer Bulletin No. 250, dated November 9,
2022.
(3) Gulfstream GII-GIIB Customer Bulletin No. 471, dated
November 9, 2022.
(4) Gulfstream GIII Customer Bulletin No. 189, dated November 9,
2022.
(5) Gulfstream GIV Customer Bulletin No. 250, dated November 9,
2022.
(h) Required Actions: Model GIV-X
For Model GIV-X airplanes: Within 60 months after the effective
date of this AD, incorporate corrective actions (includes replacing
a ground spoiler actuator hydraulic hose and associated fittings)
that physically prevent improper connection of the hydraulic lines
to the ground spoiler actuator, in accordance with a method approved
by the Manager, Atlanta ACO Branch, FAA.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Atlanta ACO Branch, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request
to your principal inspector or responsible Flight Standards Office,
as appropriate. If sending information directly to the manager of
the certification office, send it to the attention of the person
identified in paragraph (j) of this AD.
(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) For service information that contains steps that are labeled
as Required for Compliance (RC), the provisions of paragraphs
(i)(3)(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. 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 Samuel Belete,
Aerospace Engineer, Systems and Equipment Section, FAA, Atlanta ACO
Branch, 1701 Columbia Avenue, College Park, GA 30337; phone: 404-
474-5580; 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) Gulfstream G300 Customer Bulletin No. 250, dated November 9,
2022.
(ii) Gulfstream G400 Customer Bulletin No. 250, dated November
9, 2022.
(iii) Gulfstream GII-GIIB Customer Bulletin No. 471, dated
November 9, 2022.
(iv) Gulfstream GIII Customer Bulletin No. 189, dated November
9, 2022.
(v) Gulfstream GIV Customer Bulletin No. 250, dated November 9,
2022.
(3) For service information identified in this AD, contact
Gulfstream Aerospace Corporation, Technical Publications Dept., P.O.
Box 2206, Savannah, GA 31402-2206; telephone 800-810-4853; email
[email protected]; website gulfstream.com/en/customer-support/.
(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: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on April 14, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-10328 Filed 5-15-23; 8:45 am]
BILLING CODE 4910-13-P