Airworthiness Directives; Saab AB, Support and Services (Formerly Known as Saab AB, Saab Aeronautics) Airplanes, 63009-63011 [2023-19899]
Download as PDF
Federal Register / Vol. 88, No. 177 / Thursday, September 14, 2023 / Rules and Regulations
request to your principal inspector or
responsible Flight Standards Office, as
appropriate. If sending information directly
to the International Validation Branch, send
it to the attention of the person identified in
paragraph (j) of this AD. Information may be
emailed to: 9-AVS-AIR-730-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, International Validation
Branch, FAA; or EASA; or ATR—GIE Avions
de Transport Re´gional’s EASA Design
Organization Approval (DOA). If approved by
the DOA, the approval must include the
DOA-authorized signature.
(j) Additional Information
For more information about this AD,
contact Shahram Daneshmandi, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; phone: 206–
231–3220; email: shahram.daneshmandi@
faa.gov.
lotter on DSK11XQN23PROD with RULES1
(k) 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.
(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 2023–0010, dated January 17,
2023.
(ii) Safran Landing Systems SAS Service
Bulletin 631–32–286, dated October 28, 2022.
(3) For EASA AD 2023–0010, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; website
easa.europa.eu. You may find this EASA AD
on the EASA website at ad.easa.europa.eu.
(4) For Safran Landing Systems SAS
service information, contact Safran Landing
Systems SAS, Inovel Parc Sud—7, rue
Ge´ne´ral Vale´rie Andre´, 78140 VELIZY–
VILLACOUBLAY—FRANCE; telephone +33
(0) 1 46 29 81 00, website safran-landingsystems.com.
(5) 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.
(6) 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:
www.archives.gov/federal-register/cfr/ibrlocations.html.
VerDate Sep<11>2014
15:54 Sep 13, 2023
Jkt 259001
Issued on September 7, 2023.
Ross Landes,
Deputy Director for Regulatory Operations,
Compliance & Airworthiness Division,
Aircraft Certification Service.
[FR Doc. 2023–19900 Filed 9–13–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2023–1215; Project
Identifier MCAI–2023–00196–T; Amendment
39–22528; AD 2023–17–02]
RIN 2120–AA64
Airworthiness Directives; Saab AB,
Support and Services (Formerly
Known as Saab AB, Saab Aeronautics)
Airplanes
Frm 00017
Fmt 4700
Sfmt 4700
FOR FURTHER INFORMATION CONTACT:
Shahram Daneshmandi, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590;
telephone 206–231–3220; email
Shahram.Daneshmandi@faa.gov.
Background
The FAA is adopting a new
airworthiness directive (AD) for certain
Saab AB, Support and Services Model
340A (SAAB/SF340A) and SAAB 340B
airplanes. This AD was prompted by
reports of a high number of events
related to stall warnings upon landing,
following introduction of the ice speed
function within the stall warning
system. This AD requires modification
of the stall warning/identification
system, as specified in a European
Union Aviation Safety Agency (EASA)
AD, which is incorporated by reference.
The FAA is issuing this AD to address
the unsafe condition on these products.
DATES: This AD is effective October 19,
2023.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of October 19, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–1215; 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 EASA material incorporated by
reference in this AD, contact EASA,
PO 00000
Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221
8999 000; email ADs@easa.europa.eu;
website easa.europa.eu. You may find
this material on the EASA website at
ad.easa.europa.eu.
• 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 in
the AD docket at regulations.gov under
Docket No. FAA–2023–1215.
SUPPLEMENTARY INFORMATION:
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY:
63009
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain SAAB/SF340A and
SAAB 340B airplanes. The NPRM
published in the Federal Register on
June 20, 2023 (88 FR 39794). The NPRM
was prompted by AD 2022–0216R1,
dated February 1, 2023; corrected
February 2, 2023, issued by EASA,
which is the Technical Agent for the
Member States of the European Union
(EASA AD 2022–0216R1) (also referred
to as the MCAI). The MCAI states that
following the introduction of the ice
speed function within the SAAB 340
stall warning system, a high number of
events have been reported related to
stall warnings upon landing.
Subsequent investigation determined
that the margin to stall warning is lower
when ice speed is ON than with ice
speed OFF. This condition, if not
corrected, could lead to inappropriate
stall warnings during the landing phase
and result in increased pilot workload
during a critical phase of flight.
In the NPRM, the FAA proposed to
require accomplishing the actions
specified in EASA AD 2022–0216R1,
except for any differences identified as
exceptions in the regulatory text of this
AD. The FAA is issuing this AD to
address the unsafe condition on these
products.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2023–1215.
E:\FR\FM\14SER1.SGM
14SER1
63010
Federal Register / Vol. 88, No. 177 / Thursday, September 14, 2023 / Rules and Regulations
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the NPRM or on the determination of
the cost to the public.
Conclusion
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 this State of
Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI referenced above. The FAA
reviewed the relevant data and
determined that air safety requires
adopting this AD as proposed.
Accordingly, the FAA is issuing this AD
to address the unsafe condition on this
product. 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
EASA AD 2022–0216R1 specifies
procedures for modifying the stall
warning/identification system to
introduce an ice speed cancel logic.
This material 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 79 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
Up to 30 work-hours × $85 per hour = $2,550 ...............................................
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
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
VerDate Sep<11>2014
15:54 Sep 13, 2023
Jkt 259001
$7,900
Cost per product
Up to $10,450 ........
under the criteria of the Regulatory
Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA amends 14 CFR part 39 as
follows:
PART 39—AIRWORTHINESS
DIRECTIVES
1. The authority citation for part 39
continues to read as follows:
■
Authority: 49 U.S.C. 106(g), 40113, 44701.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive:
■
2023–17–02 Saab AB, Support and Services
(Formerly Known as Saab AB, Saab
Aeronautics): Amendment 39–22528;
Docket No. FAA–2023–1215; Project
Identifier MCAI–2023–00196–T.
(a) Effective Date
This airworthiness directive (AD) is
effective October 19, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Saab AB, Support and
Services (formerly known as Saab AB, Saab
Aeronautics) Model 340A (SAAB/SF340A)
and SAAB 340B airplanes, certificated in any
category, as identified in European Union
Aviation Safety Agency (EASA) AD 2022–
0216R1, dated February 1, 2023; corrected
February 2, 2023 (EASA AD 2022–0216R1).
PO 00000
Frm 00018
Fmt 4700
Sfmt 4700
Cost on U.S. operators
Up to $825,550.
(d) Subject
Air Transport Association (ATA) of
America Code 27, Flight controls.
(e) Unsafe Condition
This AD was prompted by reports of a high
number of events related to stall warnings
upon landing, following introduction of the
ice speed function within the stall warning
system. The FAA is issuing this AD to
address a margin to stall warning that is
lower when ice speed is ON than with ice
speed OFF. The unsafe condition, if not
addressed, could lead to inappropriate stall
warnings during the landing phase and result
in increased pilot workload during a critical
phase of flight.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Requirements
Except as specified in paragraph (h) of this
AD: Comply with all required actions and
compliance times specified in, and in
accordance with, EASA AD 2022–0216R1.
(h) Exceptions to EASA AD 2022–0216R1
(1) Where EASA AD 2022–0216R1 refers to
November 16, 2022 (the effective date of
EASA AD 2022–0216), this AD requires using
the effective date of this AD.
(2) The ‘‘Remarks’’ section of EASA AD
2022–0216R1 does not apply to this AD.
(i) Additional AD Provisions
The following provisions also apply to this
AD:
(1) Alternative Methods of Compliance
(AMOCs): 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
responsible Flight Standards Office, as
appropriate. If sending information directly
to the International Validation Branch, send
E:\FR\FM\14SER1.SGM
14SER1
Federal Register / Vol. 88, No. 177 / Thursday, September 14, 2023 / Rules and Regulations
it to the attention of the person identified in
paragraph (j) of this AD. Information may be
emailed to: 9-AVS-AIR-730-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, International Validation
Branch, FAA; or EASA; or Saab AB, Support
and Services’ EASA Design Organization
Approval (DOA). If approved by the DOA,
the approval must include the DOAauthorized signature.
DEPARTMENT OF TRANSPORTATION
(j) Additional Information
The FAA is adopting a new
airworthiness directive (AD) for all
Airbus SAS Model A330–200 series
airplanes, Model A330–200 Freighter
series airplanes, Model A330–300 series
airplanes, Model A340–200 series
airplanes, and Model A340–300 series
airplanes. This AD was prompted by a
report that certain overheat detection
system (OHDS) sensing elements,
produced before January 31, 2021, may
not properly detect thermal bleed leak
events due to a quality escape during
the manufacturing process. This AD
requires a one-time special detailed
inspection (SDI) for discrepancies of
each affected part installed at an
affected position, and replacement of
discrepant parts, as specified in a
European Union Aviation Safety Agency
(EASA) AD, which is incorporated by
reference. This AD would also prohibit
the installation of affected parts. The
FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective October 19,
2023.
The Director of the Federal Register
approved the incorporation by reference
of certain publications listed in this AD
as of October 19, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2023–1051; 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 EASA material incorporated by
reference in this AD, contact EASA,
Konrad-Adenauer-Ufer 3, 50668
(k) Material Incorporated by Reference
lotter on DSK11XQN23PROD with RULES1
(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.
(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 2022–0216R1, dated February 1,
2023; corrected February 2, 2023.
(ii) [Reserved]
(3) For EASA AD 2022–0216R1, contact
EASA, Konrad-Adenauer-Ufer 3, 50668
Cologne, Germany; telephone +49 221 8999
000; email ADs@easa.europa.eu; website
easa.europa.eu. You may find this EASA AD
on the EASA website at ad.easa.europa.eu.
(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 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:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on August 17, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–19899 Filed 9–13–23; 8:45 am]
BILLING CODE 4910–13–P
15:54 Sep 13, 2023
14 CFR Part 39
[Docket No. FAA–2023–1051; Project
Identifier MCAI–2022–01565–T; Amendment
39–22529; AD 2023–17–03]
RIN 2120–AA64
Airworthiness Directives; Airbus SAS
Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY:
For more information about this AD,
contact Shahram Daneshmandi, Aviation
Safety Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone
206–231–3220; email
Shahram.Daneshmandi@faa.gov.
VerDate Sep<11>2014
Federal Aviation Administration
Jkt 259001
PO 00000
Frm 00019
Fmt 4700
Sfmt 4700
63011
Cologne, Germany; telephone +49 221
8999 000; email ADs@easa.europa.eu;
website easa.europa.eu. You may find
this material on the EASA website at
ad.easa.europa.eu.
• For Kidde Aerospace & Defense
service information incorporated by
reference in this AD, contact Kidde
Aerospace & Defense, 4200 Airport
Drive NW, Building B, Wilson, NC
27896; telephone 319–295–5000;
website kiddetechnologies.com/
aviation.com.
• 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.
It is also available in the AD docket at
regulations.gov under Docket No. FAA–
2023–1051.
FOR FURTHER INFORMATION CONTACT:
Timothy Dowling, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590;
telephone 206–231–3667; email
Timothy.P.Dowling@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to all Airbus SAS Model A330–
200 1 series airplanes, Model A330–200
Freighter series airplanes, Model A330–
300 series airplanes, Model A340–200
series airplanes, and Model A340–300
series airplanes. The NPRM published
in the Federal Register on May 26, 2023
(88 FR 34097). The NPRM was
prompted by AD 2022–0243, dated
December 8, 2022, issued by EASA,
which is the Technical Agent for the
Member States of the European Union
(EASA AD 2022–0243) (also referred to
as the MCAI). The MCAI states that the
affected part manufacturer, Kidde
Aerospace & Defense, reported that
certain OHDS sensing elements,
produced before January 31, 2021, may
not properly detect thermal bleed leak
events due to a quality escape during
the manufacturing process.
In the NPRM, the FAA proposed to
require a one-time SDI for discrepancies
of each affected part installed at an
affected position, and replacement of
discrepant parts, as specified in EASA
AD 2022–0243. The NPRM also
proposed to prohibit the installation of
1 In the preamble of the NPRM, the FAA
inadvertently referred to model ‘‘A320–200’’ series
airplanes. The affected airplane models, however,
were correctly described in the Applicability
paragraph. The preamble of this final rule has been
corrected to reference the correct model, ‘‘A330–
200’’ series airplanes.
E:\FR\FM\14SER1.SGM
14SER1
Agencies
[Federal Register Volume 88, Number 177 (Thursday, September 14, 2023)]
[Rules and Regulations]
[Pages 63009-63011]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-19899]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2023-1215; Project Identifier MCAI-2023-00196-T;
Amendment 39-22528; AD 2023-17-02]
RIN 2120-AA64
Airworthiness Directives; Saab AB, Support and Services (Formerly
Known as Saab AB, Saab Aeronautics) Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Saab AB, Support and Services Model 340A (SAAB/SF340A) and SAAB
340B airplanes. This AD was prompted by reports of a high number of
events related to stall warnings upon landing, following introduction
of the ice speed function within the stall warning system. This AD
requires modification of the stall warning/identification system, as
specified in a European Union Aviation Safety Agency (EASA) AD, which
is incorporated by reference. The FAA is issuing this AD to address the
unsafe condition on these products.
DATES: This AD is effective October 19, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of October 19,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2023-1215; 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 EASA material incorporated by reference in this AD,
contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone
+49 221 8999 000; email [email protected]; website easa.europa.eu. You
may find this material on the EASA website at ad.easa.europa.eu.
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 in the AD
docket at regulations.gov under Docket No. FAA-2023-1215.
FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aviation Safety
Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590;
telephone 206-231-3220; 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 SAAB/SF340A and
SAAB 340B airplanes. The NPRM published in the Federal Register on June
20, 2023 (88 FR 39794). The NPRM was prompted by AD 2022-0216R1, dated
February 1, 2023; corrected February 2, 2023, issued by EASA, which is
the Technical Agent for the Member States of the European Union (EASA
AD 2022-0216R1) (also referred to as the MCAI). The MCAI states that
following the introduction of the ice speed function within the SAAB
340 stall warning system, a high number of events have been reported
related to stall warnings upon landing. Subsequent investigation
determined that the margin to stall warning is lower when ice speed is
ON than with ice speed OFF. This condition, if not corrected, could
lead to inappropriate stall warnings during the landing phase and
result in increased pilot workload during a critical phase of flight.
In the NPRM, the FAA proposed to require accomplishing the actions
specified in EASA AD 2022-0216R1, except for any differences identified
as exceptions in the regulatory text of this AD. The FAA is issuing
this AD to address the unsafe condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2023-1215.
[[Page 63010]]
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
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 this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
referenced above. The FAA reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on this product.
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
EASA AD 2022-0216R1 specifies procedures for modifying the stall
warning/identification system to introduce an ice speed cancel logic.
This material 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 79 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
----------------------------------------------------------------------------------------------------------------
Up to 30 work-hours x $85 per $7,900 Up to $10,450.............. Up to $825,550.
hour = $2,550.
----------------------------------------------------------------------------------------------------------------
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:
2023-17-02 Saab AB, Support and Services (Formerly Known as Saab AB,
Saab Aeronautics): Amendment 39-22528; Docket No. FAA-2023-1215;
Project Identifier MCAI-2023-00196-T.
(a) Effective Date
This airworthiness directive (AD) is effective October 19, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Saab AB, Support and Services (formerly known
as Saab AB, Saab Aeronautics) Model 340A (SAAB/SF340A) and SAAB 340B
airplanes, certificated in any category, as identified in European
Union Aviation Safety Agency (EASA) AD 2022-0216R1, dated February
1, 2023; corrected February 2, 2023 (EASA AD 2022-0216R1).
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
controls.
(e) Unsafe Condition
This AD was prompted by reports of a high number of events
related to stall warnings upon landing, following introduction of
the ice speed function within the stall warning system. The FAA is
issuing this AD to address a margin to stall warning that is lower
when ice speed is ON than with ice speed OFF. The unsafe condition,
if not addressed, could lead to inappropriate stall warnings during
the landing phase and result in increased pilot workload during a
critical phase of flight.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Requirements
Except as specified in paragraph (h) of this AD: Comply with all
required actions and compliance times specified in, and in
accordance with, EASA AD 2022-0216R1.
(h) Exceptions to EASA AD 2022-0216R1
(1) Where EASA AD 2022-0216R1 refers to November 16, 2022 (the
effective date of EASA AD 2022-0216), this AD requires using the
effective date of this AD.
(2) The ``Remarks'' section of EASA AD 2022-0216R1 does not
apply to this AD.
(i) Additional AD Provisions
The following provisions also apply to this AD:
(1) Alternative Methods of Compliance (AMOCs): 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 responsible Flight Standards Office, as
appropriate. If sending information directly to the International
Validation Branch, send
[[Page 63011]]
it to the attention of the person identified in paragraph (j) 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, International
Validation Branch, FAA; or EASA; or Saab AB, Support and Services'
EASA Design Organization Approval (DOA). If approved by the DOA, the
approval must include the DOA-authorized signature.
(j) Additional Information
For more information about this AD, contact Shahram Daneshmandi,
Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410,
Westbury, NY 11590; telephone 206-231-3220; email
[email protected].
(k) 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.
(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 2022-0216R1,
dated February 1, 2023; corrected February 2, 2023.
(ii) [Reserved]
(3) For EASA AD 2022-0216R1, contact EASA, Konrad-Adenauer-Ufer
3, 50668 Cologne, Germany; telephone +49 221 8999 000; email
[email protected]; website easa.europa.eu. You may find this EASA
AD on the EASA website at ad.easa.europa.eu.
(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 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
[email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on August 17, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-19899 Filed 9-13-23; 8:45 am]
BILLING CODE 4910-13-P