Airworthiness directive · Standard practices/structures · Saab AB Support and Services SAAB 340B

Effective
April 18, 2024
Published
April 18, 2024 · 89 FR 27651–27652
Issued
April 11, 2024
Supersedes
AD2023-13-07
Model
SAAB 340B
Data sheet
TCDSA52EU
Registered aircraft
58 matched by model
Product
Aircraft · Large airplane
ATA chapter
51 · Standard practices and structures
Amendment
39-22733
Docket
FAA-2024-0220
Project
MCAI-2023-00760-T
Issued as
Final rule; removal

Unofficial copy from the Federal Register XML, document 2024-08153. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.

On this page

Summary

The FAA is removing Airworthiness Directive (AD) 2023-13-07, which applied to certain Saab AB, Support and Services Model SAAB 340B airplanes. AD 2023-13-07 required amending the applicable airplane flight manual (AFM) by incorporating a temporary revision (TR) to reduce the maximum take-off weight (MTOW). The FAA issued AD 2023-13-07 to address the possibility of flight in an uncertified envelope, which could result in reduced structural capability and reduced controllability of the airplane. Since the FAA issued AD 2023-13-07, a determination was made that affected airplanes can be safely operated up to the initially published MTOW. Accordingly, AD 2023-13-07 is removed.

The airworthiness directive

2023-13-07R1 Saab AB, Support and Services (formerly known as Saab AB, Saab Aeronautics): Amendment 39-22733; Docket No. FAA-2024-0220; Project Identifier MCAI-2023-00760-T.

(a) Effective Date

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This AD is effective April 18, 2024.

(b) Affected AD

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This AD replaces AD 2023-13-07, Amendment 39-22492 (88 FR 43052, July 6, 2023) (AD 2023-13-07).

(c) Applicability

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This AD applies to Saab AB, Support and Services (formerly known as Saab AB, Saab Aeronautics) Model SAAB 340B airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2023-0121, dated June 13, 2023: airplanes not having SAAB modification 2571 (extended wingtip modification) embodied and having GE Aviation Systems LTD (Dowty Propellers) installed.

(d) Subject

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Air Transport Association (ATA) of America Code 51, Standard practices/structures.

(e) Terminating Action

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This AD terminates all requirements of AD 2023-13-07.

(f) Related Information

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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.

(g) Material Incorporated by Reference

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None.

Rule preamble

The FAA’s background, reasoning and cost estimate, published with the AD.

DatesPage 1

This AD becomes effective April 18, 2024.

AddressesPage 1

AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2024-0220; 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.

Related Service Information:

• For EASA material, 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 material on the EASA website at ad.easa.europa.eu.

• 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.

For further information contactPage 1

Shahram Daneshmandi, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206-231-3220; email shahram.daneshmandi@faa.gov.

BackgroundPage 1

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by removing AD 2023-13-07, Amendment 39-22492 (88 FR 43052, July 6, 2023) (AD 2023-13-07). AD 2023-13-07 applied to certain Saab AB, Support and Services Model SAAB 340B airplane. The NPRM was published in the Federal Register on February 9, 2024 (89 FR 9077). AD 2023-13-07 was prompted by AD 2023-0121, dated June 12, 2023 (EASA AD 2023-0121) (also referred to as the MCAI), issued by the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union. The NPRM was prompted by EASA issuing AD Cancellation Notice 2023-0121-CN, dated December 8, 2023 (EASA AD Cancellation Notice 2023-0121-CN), to cancel EASA AD 2023-0121. EASA AD Cancellation Notice 2023-0121-CN states that since EASA AD 2023-0121 was issued, Saab provided evidence that affected airplanes can be safely operated up to the initially published MTOW of 30,000 pounds. The NPRM proposed to remove AD 2023-13-07. The FAA is issuing this AD to remove AD 2023-13-07.

CommentsPage 1

The FAA received no comments on the NPRM or on the determination of the cost to the public.

Justification for Immediate Adoption and Determination of the Effective DatePage 1

Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5 U.S.C. 551 et seq.) authorizes agencies to dispense with notice and comment procedures for rules when the agency, for “good cause,” finds that those procedures are “impracticable, unnecessary, or contrary to the public interest.” Under this section, an agency, upon finding good cause, may issue a final rule without providing notice and seeking comment prior to issuance. Further, section 553(d) of the APA authorizes agencies to make rules effective in less than 30 days, upon a finding of good cause.

Since the FAA issued AD 2023-13-07, Saab provided evidence demonstrating that affected airplanes can be operated safely up to the initially published MTOW of 30,000 pounds. Therefore, the FAA is issuing this AD to remove AD 2023-13-07, and the FAA did not receive any adverse comments or useful information about this AD from U.S. operators that necessitates waiting 30 days for relief from this requirement. Accordingly, the FAA finds that good cause exists pursuant to 5 U.S.C. 553(d) for making this amendment effective in less than 30 days.

ConclusionPage 1

The FAA reviewed the relevant data and determined that air safety requires adopting this AD as proposed. Except for minor editorial changes, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator.

This AD removes all actions of AD 2023-13-07. Therefore, the requirements of AD 2023-13-07 are terminated.

Related Costs of CompliancePage 1

This AD adds no costs. This AD removes AD 2023-13-07 from 14 CFR part 39; therefore, operators are no longer required to show compliance with that AD.

Authority for This RulemakingPage 2

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.

Regulatory findingsPage 2

The FAA determined that 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.

The amendmentPage 2

Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows:

Adoption of the amendmentPage 2

1. The authority citation for part 39 continues to read as follows:

2. The FAA amends § 39.13 by:

a. Removing Airworthiness Directive (AD) 2023-13-07, Amendment 39-22492 (88 FR 43052, July 6, 2023), and

b. Adding the following new AD:

Affected TCDS · 1

The type certificate data sheets for the models this AD names, matched by model and maker.

Registered aircraft · 58

Registered aircraft whose airframe or engine model this AD names. Matched by model only, so check each against the AD’s applicability.

By aircraft maker
  • Saab-Scania42 aircraft
  • Saab15 aircraft
  • Saabscania1 aircraft
By year built
19891999
Registered aircraft by year built: 34 aircraft
19891
19908
19913
19923
19934
19941
19961
19975
19987
19991

24 with no year recorded

By model

Aircraft

See all 58 aircraft