Published 2023-09-14 · Federal Register document 2023-19899
Airworthiness Directives; Saab AB, Support and Services (Formerly Known as Saab AB, Saab Aeronautics) Airplanes
Publication 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.
Why this record is shown
Source: Federal Register annual FAA metadata. Acquired 2026-09-03T22:24:14.395624+00:00. The title, summary and date are source facts.
- Source revision
- federal_register_ad_metadata_2023-81e907e5105d0f2c
- Source row
- results[248]
- Raw source SHA-256
- 81e907e5105d0f2c522e15b6fa8c7277117367b7f70b363862619549836b75e8
Final-rule publication
Recorded publication clauses
- AD identifier printed in this edition
- 2023-17-02
- Effective date printed in this edition
- 2023-10-19
Read 11 complete recorded clauses
Effective Date
(a) Effective Date
This airworthiness directive (AD) is effective October 19, 2023.
Exact source excerpt. Text positions 8624–8714, end exclusive, in the original decoded publication. SHA-256: b74e60219c9630eaa98e2bb7f32feb09af0a9175d701b9349f54275a7014848b
Affected ADs
(b) Affected ADs
None.
Exact source excerpt. Text positions 8714–8743, end exclusive, in the original decoded publication. SHA-256: 871a4afc60ceeae06e8010585055188633d616078500c45937092bfe892239c0
Applicability wording · Applicability
(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).
Exact source excerpt. Text positions 8743–9098, end exclusive, in the original decoded publication. SHA-256: 33ae599329d7576011f4028be4ec641d9cf3e7ab3a062b4701e69b2f7adeace2
Subject
(d) Subject
Air Transport Association (ATA) of America Code 27, Flight
controls.
Exact source excerpt. Text positions 9098–9186, end exclusive, in the original decoded publication. SHA-256: 5df668a44f125df3e991e4d0d4055a7abf4e497975e862633d97c2c7cacf4016
Unsafe Condition
(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.
Exact source excerpt. Text positions 9186–9707, end exclusive, in the original decoded publication. SHA-256: 774512cfe4906bd32896485843eb4213b3048327cd9b250ce2f78d0c3e2e5a22
Compliance
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
Exact source excerpt. Text positions 9707–9809, end exclusive, in the original decoded publication. SHA-256: 00fbfa31932483f627d0ce0a11cbd2e35e15d9231842b91ac85623ce533912d3
Requirements
(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.
Exact source excerpt. Text positions 9809–9996, end exclusive, in the original decoded publication. SHA-256: afa16e28e4cb5e2237813912a9fb5bd4f1d9685924fcce5cd3f5e617120eb964
Exceptions to 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.
Exact source excerpt. Text positions 9996–10280, end exclusive, in the original decoded publication. SHA-256: 70dda8905808cc2d5306e63d002ef7063891ad69c7a7eda66f0ba016c426b212
Additional AD Provisions
(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.
Exact source excerpt. Text positions 10280–11497, end exclusive, in the original decoded publication. SHA-256: 8ef56985a6c182c778c49614ff244d8c297a2322d8859c3f781480786b7fc224
Additional Information
(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].
Exact source excerpt. Text positions 11497–11730, end exclusive, in the original decoded publication. SHA-256: f3a877a1b7de4ae70a161e3b92beaedda748b2ebde9b99318f085359bda833f0
Material Incorporated by Reference
(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.
Exact source excerpt. Text positions 11730–13001, end exclusive, in the original decoded publication. SHA-256: 21dc5f23694adcfc40206d0f3d44a556163471b30a2031bad2fbd7abf73061e3
No replacement link has been established from this edition. The complete historical rule chain and current legal effect remain unknown.
Find all recorded historical references to AD 2023-17-02 · 0 printed reference observations in this pinned collection.
These are observations from one dated publication. Current legal status is unknown; aircraft applicability, installed configuration, compliance and burden require separate evidence. Missing or unparsed conditions remain unknown.
Why these observations are shown
They were extracted offline from the same immutable official HTML source as the complete recorded text. The dated source wording, original text coordinates and exact quote digests are retained. PDF/text agreement and current regulatory effect have not been qualified.
Observation revision: whole-ad-publication-clause-observations-1.0.1. Text SHA-256: 79c7cb6888616281a274d23f75cb5db42ab5cb718c6ca8bf4ee33f0fabe7452a. Source manifest: 8217c16af11276b2ec19c1cf213df845db051f352dd4f68f21702d8b3a52f5bc.
Official source · 2023-09-14
Publication text
This is the complete recorded text of this dated publication.
Current legal effect is unknown. Aircraft applicability, installed configuration and compliance require separate evidence. PDF/text agreement has not been evaluated.
Read the complete official publication text
[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:
<bullet> 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.
<bullet> 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
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These are dated publication metadata, recorded clauses and literal source observations. Word, model-label, header and reference matches do not establish current legal effect, manufacturer/model identity, aircraft applicability, installed configuration or compliance.
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