Airworthiness Directives; Gulfstream Aerospace LP (Type Certificate Previously Held by Israel Aircraft Industries, Ltd.) Airplanes, 50588-50590 [2022-17119]
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50588
Proposed Rules
Federal Register
Vol. 87, No. 158
Wednesday, August 17, 2022
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–0994; Project
Identifier MCAI–2022–00052–T]
RIN 2120–AA64
Airworthiness Directives; Gulfstream
Aerospace LP (Type Certificate
Previously Held by Israel Aircraft
Industries, Ltd.) Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain Gulfstream Aerospace LP Model
Gulfstream G200 airplanes. This
proposed AD was prompted by reports
that wing flap fairing debonding and
corrosion were discovered at certain
areas of the lower skin on both wings.
This proposed AD requires an
inspection for corrosion in certain areas
of the wing skin fairings, additional
inspections if necessary, resealing the
fairings with new fillet seal, and
applicable corrective actions, as
specified in the Civil Aviation Authority
of Israel (CAAI) AD, which is proposed
for incorporation by reference. The FAA
is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments
on this proposed AD by October 3, 2022.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
JSPEARS on DSK121TN23PROD with PROPOSALS
SUMMARY:
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16:26 Aug 16, 2022
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• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For CAAI service information
identified in this NPRM, contact Civil
Aviation Authority of Israel (CAAI),
P.O. Box 1101, Golan Street, Airport
City, 70100, Israel; telephone 972–3–
9774665; fax 972–3–9774592; email
aip@mot.gov.il. You may find this CAAI
AD on the CAAI website at
www.caa.gov.il. For Gulfstream service
information identified in this NPRM,
contact Gulfstream Aerospace
Corporation, P.O. Box 2206, Mail
Station D–25, Savannah, GA 31402–
2206; telephone 800–810–4853; fax
912–965–3520; email pubs@
gulfstream.com; internet
www.gulfstream.com/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.
Examining the AD Docket
You may examine the AD docket at
www.regulations.gov by searching for
and locating Docket No. FAA–2022–
0994; 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 NPRM, any
comments received, and other
information. The street address for
Docket Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Dan
Rodina, Aerospace Engineer, Large
Aircraft Section, International
Validation Branch, FAA, 2200 South
216th Street, Des Moines, WA 98198;
telephone and fax 206–231–3225; email
dan.rodina@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under ADDRESSES. Include ‘‘Docket No.
FAA–2022–0994; Project Identifier
MCAI–2022–00052–T’’ at the beginning
of your comments. The most helpful
comments reference a specific portion of
the proposal, explain the reason for any
recommended change, and include
supporting data. The FAA will consider
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Fmt 4702
Sfmt 4702
all comments received by the closing
date and may amend the proposal
because of those comments.
Except for Confidential Business
Information (CBI) as described in the
following paragraph, and other
information as described in 14 CFR
11.35, the FAA will post all comments
received, without change, to
www.regulations.gov, including any
personal information you provide. The
agency will also post a report
summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial
information that is both customarily and
actually treated as private by its owner.
Under the Freedom of Information Act
(FOIA) (5 U.S.C. 552), CBI is exempt
from public disclosure. If your
comments responsive to this NPRM
contain commercial or financial
information that is customarily treated
as private, that you actually treat as
private, and that is relevant or
responsive to this NPRM, it is important
that you clearly designate the submitted
comments as CBI. Please mark each
page of your submission containing CBI
as ‘‘PROPIN.’’ The FAA will treat such
marked submissions as confidential
under the FOIA, and they will not be
placed in the public docket of this
NPRM. Submissions containing CBI
should be sent to Dan Rodina,
Aerospace Engineer, Large Aircraft
Section, International Validation
Branch, FAA, 2200 South 216th Street,
Des Moines, WA 98198; telephone and
fax 206–231–3225; email dan.rodina@
faa.gov. Any commentary that the FAA
receives which is not specifically
designated as CBI will be placed in the
public docket for this rulemaking.
Background
The CAAI, which is the aviation
authority for Israel, has issued AD ISR
I–57–2021–12–4, dated January 1, 2022
(CAAI AD ISR I–57–2021–12–4) (also
referred to after this as the Mandatory
Continuing Airworthiness Information,
or the MCAI), to correct an unsafe
condition for certain Gulfstream
Aerospace LP Model Gulfstream G200
airplanes.
This proposed AD was prompted by
reports that wing flap fairing debonding
and corrosion were discovered at the
lower skin of rib 3 and rib 11 on both
wings. The FAA is proposing this AD to
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50589
Federal Register / Vol. 87, No. 158 / Wednesday, August 17, 2022 / Proposed Rules
address flap fairing debonding and
moisture intrusion that might lead to
lower wing skin corrosion and cracking
on both wings, and reduced structural
integrity of the wings. See the MCAI for
additional background information.
Related Service Information Under 1
CFR Part 51
CAAI AD ISR I–57–2021–12–4, dated
January 1, 2022, describes procedures
for an inspection for corrosion in the
area of the wing skin (or doubler if
installed) under the rib 3 and rib 11
fairings, a penetration or eddy current
inspection for cracks if corrosion was
found, a measurement of the thickness
of remaining wing skin (or doubler) if
no cracks were found, resealing of rib 3
and rib 11 fairings with new fillet seal,
and applicable corrective actions.
Corrective actions include cleaning and
removing corrosion, crack repair, and
repair of fairing installation locations
with a certain thickness reduction. 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 the ADDRESSES section.
FAA’s Determination
This product has been approved by
the aviation authority of another
country, and is approved for operation
in the United States. Pursuant to the
FAA’s bilateral agreement with the State
of Design Authority, the FAA has been
notified of the unsafe condition
described in the MCAI and service
information referenced above. The FAA
is proposing this AD because the FAA
evaluated all the relevant information
and determined the unsafe condition
described previously is likely to exist or
develop on other products of the same
type design.
Proposed AD Requirements in This
NPRM
This proposed AD requires
accomplishing the actions specified in
CAAI AD ISR I–57–2021–12–4
described previously, except for any
differences identified as exceptions in
the regulatory text of this proposed AD.
Costs of Compliance
The FAA estimates that this AD, if
adopted as proposed, would affect 168
airplanes of U.S. registry. The FAA
estimates the following costs to comply
with this proposed AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Cost per
product
Labor cost
Parts cost
29 work-hours × $85 per hour = $2,465 ......................
Minimal .........................................................................
The FAA estimates the following
costs to do any necessary on-condition
action that would be required based on
the results of any required actions. The
FAA has no way of determining the
Cost on U.S.
operators
$2,465
$414,120
number of aircraft that might need these
on-condition actions:
ESTIMATED COSTS OF ON-CONDITION ACTIONS
[*]
Labor cost
Parts cost
Up to 10 work-hours × $85 per hour = $850 .............................................................................................................
$0
Cost per
product
Up to $850.
* The FAA has received no definitive data on which to base the cost estimates for the on-condition repairs specified in this proposed AD.
The FAA has included all known
costs in its cost estimate. According to
the manufacturer, however, some or all
of the costs of this proposed AD may be
covered under warranty, thereby
reducing the cost impact on affected
operators.
JSPEARS on DSK121TN23PROD with PROPOSALS
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
VerDate Sep<11>2014
16:26 Aug 16, 2022
Jkt 256001
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
The FAA determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would 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 this proposed regulation:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Would not affect intrastate
aviation in Alaska, and
(3) Would 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 Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 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:
■
Gulfstream Aerospace LP (Type Certificate
Previously Held by Israel Aircraft
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Federal Register / Vol. 87, No. 158 / Wednesday, August 17, 2022 / Proposed Rules
Industries, Ltd.): Docket No. FAA–2022–
0994; Project Identifier MCAI–2022–
00052–T.
(a) Comments Due Date
The FAA must receive comments on this
airworthiness directive (AD) by October 3,
2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Gulfstream Aerospace
LP Model Gulfstream G200 airplanes,
certificated in any category, as identified in
The Civil Aviation Authority of Israel (CAAI)
AD ISR I–57–2021–12–4, dated January 1,
2022 (CAAI AD ISR I–57–2021–12–4).
(d) Subject
Air Transport Association (ATA) of
America Code 57, Wings.
(e) Unsafe Condition
This AD was prompted by reports that
wing flap fairing debonding and corrosion
were discovered at lower skin of rib 3 and
rib 11 on both wings. The FAA is issuing this
AD to address flap fairing debonding and
moisture intrusion that might lead to lower
wing skin corrosion and cracking on both
wings, and reduced structural integrity of the
wings.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
JSPEARS on DSK121TN23PROD with PROPOSALS
(g) Required Actions
Except as specified in paragraph (h) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, CAAI AD ISR I–57–2021–
12–4.
(h) Exceptions to Service Information
Specifications
(1) Where CAAI AD ISR I–57–2021–12–4
refers to its effective date, this AD requires
using the effective date of this AD.
(2) Where the Compliance paragraph of
CAAI AD ISR I–57–2021–12–4 requires
compliance at a certain time, replace the text
‘‘at the next suitable planned maintenance
inspection within the next 24 months from
the effective date of this AD’’ with ‘‘within
24 months after the effective date of this
AD.’’
(3) Where the Action paragraph of CAAI
AD ISR I–57–2021–12–4 refers to certain
service information, replace the text
‘‘Gulfstream Service Bulletin No. 200–57–
426, dated January 01, 2022, or later
approved revision,’’ with ‘‘Gulfstream
Service Bulletin No. 200–57–426, Revision 1,
dated June 16, 2022, or later approved
revision.’’
(4) Where the service information specified
in CAAI AD ISR I–57–2021–12–4 specifies to
report to Gulfstream if ‘‘cracks were
discovered’’ and ‘‘for any fairing installation
location with one or more grid squares with
thickness reduction of greater than 10%,’’ for
this AD, cracks and fairing installation
locations with one or more grid squares with
VerDate Sep<11>2014
18:18 Aug 16, 2022
Jkt 256001
thickness reduction of greater than 10% must
be repaired before further flight using a
method approved by the Manager, Large
Aircraft Section, International Validation
Branch, FAA; or CAAI; or CAAI’s authorized
Designee. If approved by the authorized
Designee, the approval must include the
Designee’s authorized signature.
Issued on August 4, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
(i) No Reporting Requirement
DEPARTMENT OF TRANSPORTATION
Although the service information
referenced in CAAI AD ISR I–57–2021–12–4
specifies to submit certain information to the
manufacturer, this AD does not include that
requirement.
(j) Other FAA AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): The Manager, Large Aircraft
Section, 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 responsible Flight
Standards Office, as appropriate. If sending
information directly to the Large Aircraft
Section, International Validation Branch,
send it to the attention of the person
identified in paragraph (k)(2) of this AD.
Information may be emailed to: 9-AVS-AIR730-AMOC@faa.gov. Before using any
approved AMOC, notify your appropriate
principal inspector, or lacking a principal
inspector, the manager of the responsible
Flight Standards Office.
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain instructions
from a manufacturer, the instructions must
be accomplished using a method approved
by the Manager, Large Aircraft Section,
International Validation Branch, FAA; or the
Civil Aviation Authority of Israel (CAAI); or
the CAAI’s authorized Designee. If approved
by the CAAI Designee, the approval must
include the Designee’s authorized signature.
(k) Related Information
(1) For CAAI AD ISR I–57–2021–12–4,
dated January 1, 2022, contact Civil Aviation
Authority of Israel (CAAI), P.O. Box 1101,
Golan Street, Airport City, 70100, Israel;
telephone 972–3–9774665; fax 972–3–
9774592; email aip@mot.gov.il. You may find
this CAAI AD on the CAAI website at
www.caa.gov.il. You may view this material
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. This material may be found
in the AD docket at www.regulations.gov by
searching for and locating Docket No. FAA–
2022–0994.
(2) For more information about this AD,
contact Dan Rodina, Aerospace Engineer,
Large Aircraft Section, International
Validation Branch, FAA–2022–0994. 2200
South 216th Street, Des Moines, WA 98198;
telephone and fax 206–231–3225; email
dan.rodina@faa.gov.
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[FR Doc. 2022–17119 Filed 8–16–22; 8:45 am]
BILLING CODE 4910–13–P
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2022–0970; Airspace
Docket No. 22–ASW–18]
RIN 2120–AA66
Proposed Revocation of Class E
Airspace; Stratford, TX
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
This action proposes to
remove the Class E airspace at Stratford,
TX. The FAA is proposing this action
due to the cancellation of the
instrument procedures at the associated
airport, and the airspace no longer being
required.
DATES: Comments must be received on
or before October 3, 2022.
ADDRESSES: Send comments on this
proposal to the U.S. Department of
Transportation, Docket Operations,
West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590; telephone (202)
366–9826, or (800) 647–5527. You must
identify FAA Docket No. FAA–2022–
0970/Airspace Docket No. 22–ASW–18,
at the beginning of your comments. You
may also submit comments through the
internet at www.regulations.gov. You
may review the public docket
containing the proposal, any comments
received, and any final disposition in
person in the Dockets Office between
9:00 a.m. and 5:00 p.m., Monday
through Friday, except federal holidays.
FAA Order JO 7400.11F, Airspace
Designations and Reporting Points, and
subsequent amendments can be viewed
online at www.faa.gov/air_traffic/
publications/. For further information,
you can contact the Airspace Policy
Group, Federal Aviation
Administration, 800 Independence
Avenue SW, Washington, DC 20591;
telephone: (202) 267–8783.
FOR FURTHER INFORMATION CONTACT:
Jeffrey Claypool, Federal Aviation
Administration, Operations Support
Group, Central Service Center, 10101
Hillwood Parkway, Fort Worth, TX
76177; telephone (817) 222–5711.
SUMMARY:
E:\FR\FM\17AUP1.SGM
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Agencies
[Federal Register Volume 87, Number 158 (Wednesday, August 17, 2022)]
[Proposed Rules]
[Pages 50588-50590]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-17119]
========================================================================
Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
========================================================================
Federal Register / Vol. 87, No. 158 / Wednesday, August 17, 2022 /
Proposed Rules
[[Page 50588]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-0994; Project Identifier MCAI-2022-00052-T]
RIN 2120-AA64
Airworthiness Directives; Gulfstream Aerospace LP (Type
Certificate Previously Held by Israel Aircraft Industries, Ltd.)
Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain Gulfstream Aerospace LP Model Gulfstream G200 airplanes.
This proposed AD was prompted by reports that wing flap fairing
debonding and corrosion were discovered at certain areas of the lower
skin on both wings. This proposed AD requires an inspection for
corrosion in certain areas of the wing skin fairings, additional
inspections if necessary, resealing the fairings with new fillet seal,
and applicable corrective actions, as specified in the Civil Aviation
Authority of Israel (CAAI) AD, which is proposed for incorporation by
reference. The FAA is proposing this AD to address the unsafe condition
on these products.
DATES: The FAA must receive comments on this proposed AD by October 3,
2022.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to www.regulations.gov.
Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For CAAI service information identified in this NPRM, contact Civil
Aviation Authority of Israel (CAAI), P.O. Box 1101, Golan Street,
Airport City, 70100, Israel; telephone 972-3-9774665; fax 972-3-
9774592; email [email protected]. You may find this CAAI AD on the CAAI
website at www.caa.gov.il. For Gulfstream service information
identified in this NPRM, contact Gulfstream Aerospace Corporation, P.O.
Box 2206, Mail Station D-25, Savannah, GA 31402-2206; telephone 800-
810-4853; fax 912-965-3520; email [email protected]; internet
www.gulfstream.com/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.
Examining the AD Docket
You may examine the AD docket at www.regulations.gov by searching
for and locating Docket No. FAA-2022-0994; 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 NPRM, any comments
received, and other information. The street address for Docket
Operations is listed above.
FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, Large
Aircraft Section, International Validation Branch, FAA, 2200 South
216th Street, Des Moines, WA 98198; telephone and fax 206-231-3225;
email [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under ADDRESSES. Include ``Docket No. FAA-2022-0994; Project Identifier
MCAI-2022-00052-T'' at the beginning of your comments. The most helpful
comments reference a specific portion of the proposal, explain the
reason for any recommended change, and include supporting data. The FAA
will consider all comments received by the closing date and may amend
the proposal because of those comments.
Except for Confidential Business Information (CBI) as described in
the following paragraph, and other information as described in 14 CFR
11.35, the FAA will post all comments received, without change, to
www.regulations.gov, including any personal information you provide.
The agency will also post a report summarizing each substantive verbal
contact received about this NPRM.
Confidential Business Information
CBI is commercial or financial information that is both customarily
and actually treated as private by its owner. Under the Freedom of
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public
disclosure. If your comments responsive to this NPRM contain commercial
or financial information that is customarily treated as private, that
you actually treat as private, and that is relevant or responsive to
this NPRM, it is important that you clearly designate the submitted
comments as CBI. Please mark each page of your submission containing
CBI as ``PROPIN.'' The FAA will treat such marked submissions as
confidential under the FOIA, and they will not be placed in the public
docket of this NPRM. Submissions containing CBI should be sent to Dan
Rodina, Aerospace Engineer, Large Aircraft Section, International
Validation Branch, FAA, 2200 South 216th Street, Des Moines, WA 98198;
telephone and fax 206-231-3225; email [email protected]. Any
commentary that the FAA receives which is not specifically designated
as CBI will be placed in the public docket for this rulemaking.
Background
The CAAI, which is the aviation authority for Israel, has issued AD
ISR I-57-2021-12-4, dated January 1, 2022 (CAAI AD ISR I-57-2021-12-4)
(also referred to after this as the Mandatory Continuing Airworthiness
Information, or the MCAI), to correct an unsafe condition for certain
Gulfstream Aerospace LP Model Gulfstream G200 airplanes.
This proposed AD was prompted by reports that wing flap fairing
debonding and corrosion were discovered at the lower skin of rib 3 and
rib 11 on both wings. The FAA is proposing this AD to
[[Page 50589]]
address flap fairing debonding and moisture intrusion that might lead
to lower wing skin corrosion and cracking on both wings, and reduced
structural integrity of the wings. See the MCAI for additional
background information.
Related Service Information Under 1 CFR Part 51
CAAI AD ISR I-57-2021-12-4, dated January 1, 2022, describes
procedures for an inspection for corrosion in the area of the wing skin
(or doubler if installed) under the rib 3 and rib 11 fairings, a
penetration or eddy current inspection for cracks if corrosion was
found, a measurement of the thickness of remaining wing skin (or
doubler) if no cracks were found, resealing of rib 3 and rib 11
fairings with new fillet seal, and applicable corrective actions.
Corrective actions include cleaning and removing corrosion, crack
repair, and repair of fairing installation locations with a certain
thickness reduction. 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 the ADDRESSES section.
FAA's Determination
This product has been approved by the aviation authority of another
country, and is approved for operation in the United States. Pursuant
to the FAA's bilateral agreement with the State of Design Authority,
the FAA has been notified of the unsafe condition described in the MCAI
and service information referenced above. The FAA is proposing this AD
because the FAA evaluated all the relevant information and determined
the unsafe condition described previously is likely to exist or develop
on other products of the same type design.
Proposed AD Requirements in This NPRM
This proposed AD requires accomplishing the actions specified in
CAAI AD ISR I-57-2021-12-4 described previously, except for any
differences identified as exceptions in the regulatory text of this
proposed AD.
Costs of Compliance
The FAA estimates that this AD, if adopted as proposed, would
affect 168 airplanes of U.S. registry. The FAA estimates the following
costs to comply with this proposed AD:
Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
29 work-hours x $85 per hour = $2,465......... Minimal......................... $2,465 $414,120
----------------------------------------------------------------------------------------------------------------
The FAA estimates the following costs to do any necessary on-
condition action that would be required based on the results of any
required actions. The FAA has no way of determining the number of
aircraft that might need these on-condition actions:
Estimated Costs of On-Condition Actions \[*]\
------------------------------------------------------------------------
Labor cost Parts cost Cost per product
------------------------------------------------------------------------
Up to 10 work-hours x $85 per $0 Up to $850.
hour = $850.
------------------------------------------------------------------------
* The FAA has received no definitive data on which to base the cost
estimates for the on-condition repairs specified in this proposed AD.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some or all of the costs of
this proposed 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
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would 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 this proposed
regulation:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Would not affect intrastate aviation in Alaska, and
(3) Would 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 Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 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:
Gulfstream Aerospace LP (Type Certificate Previously Held by Israel
Aircraft
[[Page 50590]]
Industries, Ltd.): Docket No. FAA-2022-0994; Project Identifier
MCAI-2022-00052-T.
(a) Comments Due Date
The FAA must receive comments on this airworthiness directive
(AD) by October 3, 2022.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Gulfstream Aerospace LP Model Gulfstream G200
airplanes, certificated in any category, as identified in The Civil
Aviation Authority of Israel (CAAI) AD ISR I-57-2021-12-4, dated
January 1, 2022 (CAAI AD ISR I-57-2021-12-4).
(d) Subject
Air Transport Association (ATA) of America Code 57, Wings.
(e) Unsafe Condition
This AD was prompted by reports that wing flap fairing debonding
and corrosion were discovered at lower skin of rib 3 and rib 11 on
both wings. The FAA is issuing this AD to address flap fairing
debonding and moisture intrusion that might lead to lower wing skin
corrosion and cracking on both wings, and reduced structural
integrity of the wings.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, CAAI AD ISR I-57-2021-12-4.
(h) Exceptions to Service Information Specifications
(1) Where CAAI AD ISR I-57-2021-12-4 refers to its effective
date, this AD requires using the effective date of this AD.
(2) Where the Compliance paragraph of CAAI AD ISR I-57-2021-12-4
requires compliance at a certain time, replace the text ``at the
next suitable planned maintenance inspection within the next 24
months from the effective date of this AD'' with ``within 24 months
after the effective date of this AD.''
(3) Where the Action paragraph of CAAI AD ISR I-57-2021-12-4
refers to certain service information, replace the text ``Gulfstream
Service Bulletin No. 200-57-426, dated January 01, 2022, or later
approved revision,'' with ``Gulfstream Service Bulletin No. 200-57-
426, Revision 1, dated June 16, 2022, or later approved revision.''
(4) Where the service information specified in CAAI AD ISR I-57-
2021-12-4 specifies to report to Gulfstream if ``cracks were
discovered'' and ``for any fairing installation location with one or
more grid squares with thickness reduction of greater than 10%,''
for this AD, cracks and fairing installation locations with one or
more grid squares with thickness reduction of greater than 10% must
be repaired before further flight using a method approved by the
Manager, Large Aircraft Section, International Validation Branch,
FAA; or CAAI; or CAAI's authorized Designee. If approved by the
authorized Designee, the approval must include the Designee's
authorized signature.
(i) No Reporting Requirement
Although the service information referenced in CAAI AD ISR I-57-
2021-12-4 specifies to submit certain information to the
manufacturer, this AD does not include that requirement.
(j) Other FAA AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): The Manager,
Large Aircraft Section, 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 responsible Flight
Standards Office, as appropriate. If sending information directly to
the Large Aircraft Section, International Validation Branch, send it
to the attention of the person identified in paragraph (k)(2) of
this AD. Information may be emailed to: [email protected].
Before using any approved AMOC, notify your appropriate principal
inspector, or lacking a principal inspector, the manager of the
responsible Flight Standards Office.
(2) Contacting the Manufacturer: For any requirement in this AD
to obtain instructions from a manufacturer, the instructions must be
accomplished using a method approved by the Manager, Large Aircraft
Section, International Validation Branch, FAA; or the Civil Aviation
Authority of Israel (CAAI); or the CAAI's authorized Designee. If
approved by the CAAI Designee, the approval must include the
Designee's authorized signature.
(k) Related Information
(1) For CAAI AD ISR I-57-2021-12-4, dated January 1, 2022,
contact Civil Aviation Authority of Israel (CAAI), P.O. Box 1101,
Golan Street, Airport City, 70100, Israel; telephone 972-3-9774665;
fax 972-3-9774592; email [email protected]. You may find this CAAI AD
on the CAAI website at www.caa.gov.il. You may view this material 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. This
material may be found in the AD docket at www.regulations.gov by
searching for and locating Docket No. FAA-2022-0994.
(2) For more information about this AD, contact Dan Rodina,
Aerospace Engineer, Large Aircraft Section, International Validation
Branch, FAA-2022-0994. 2200 South 216th Street, Des Moines, WA
98198; telephone and fax 206-231-3225; email [email protected].
Issued on August 4, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2022-17119 Filed 8-16-22; 8:45 am]
BILLING CODE 4910-13-P