AD 2024-17-09

Airworthiness directive · Cabin Equipment/Furnishings · Embraer EMB-505

Effective
November 12, 2024
Published
October 8, 2024 · 89 FR 81336–81338
Issued
October 3, 2024
Model
EMB-505
Data sheet
TCDSA60CE
Registered aircraft
677 matched by model
Product
Aircraft · Small airplane
ATA chapter
25 · Equipment and furnishings
Amendment
39-22834
Docket
FAA-2024-1484
Project
MCAI-2023-00968-A
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 2024-23248. Only the govinfo PDF is the legal edition. DRS record last changed November 21, 2025.

On this page

Summary

The FAA is adopting a new airworthiness directive (AD) for certain Embraer S.A. (Embraer) Model EMB-505 airplanes. This AD was prompted by analysis of the left-hand (LH) refreshment center and LH forward cabinet that identified the need for installing structural reinforcements. This AD requires installing structural reinforcements as specified in an Agência Nacional de Aviação Civil (ANAC) AD, which is incorporated by reference. The FAA is issuing this AD to address the unsafe condition on these products.

The airworthiness directive

2024-17-09 Embraer S.A.: Amendment 39-22834; Docket No. FAA-2024-1484; Project Identifier MCAI-2023-00968-A.

(a) Effective Date

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This airworthiness directive (AD) is effective November 12, 2024.

(b) Affected ADs

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None.

(c) Applicability

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This AD applies to Embraer S.A. Model EMB-505 airplanes, certificated in any category, as identified in Agência Nacional de Aviação Civil (ANAC) AD 2023-07-01, effective August 10, 2023, as corrected by ANAC Airworthiness Directive Errata, effective August 10, 2023 (ANAC AD 2023-07-01).

(d) Subject

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Joint Aircraft System Component (JASC) Code 2500, Cabin Equipment/Furnishings.

(e) Unsafe Condition

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This AD was prompted by an analysis that the left-hand (LH) refreshment center and LH forward cabinet might not withstand the loads expected for specific emergency landing conditions. The FAA is issuing this AD to address the possibility of detachment of mass items during specific emergency landing conditions. The unsafe condition, if not addressed, could result in injuries to the airplane occupants.

(f) Compliance

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Comply with this AD within the compliance times specified, unless already done.

(g) Required Actions

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Except as specified in paragraphs (h) and (i) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, ANAC AD 2023-07-01.

(h) Exceptions to ANAC AD 2023-07-01

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(1) Where ANAC AD 2023-07-01 refers to its effective date, this AD requires using the effective date of this AD.

(2) Although the material referenced in ANAC AD 2023-07-01 allows the use of alternative or similar parts in place of the ones specified in the kits provided, this AD requires that alternative or similar parts be approved by the Manager, International Validation Branch, FAA; ANAC; or ANAC's authorized Designee. If approved by the ANAC Designee, the approval must include the Designee's authorized signature.

(3) Where the material referenced in ANAC AD 2023-07-01 specifies to “discard” certain parts, for this AD replace that text with “remove from service.”

(4) This AD does not adopt paragraphs (c) and (d) of ANAC AD 2023-07-01.

(i) No Reporting Requirement

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Although the material referenced in ANAC AD 2023-07-01 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

(j) Alternative Methods of Compliance (AMOCs)

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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 local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Validation Branch, mail it to the address identified in paragraph (k) of this AD or email to: AMOC@faa.gov. If mailing information, also submit information by email. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local Flight Standards District Office/certificate holding district office.

(k) Additional Information

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For more information about this AD, contact Jim Rutherford, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (816) 329-4165; email: jim.rutherford@faa.gov.

(l) Material Incorporated by Reference

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(1) The Director of the Federal Register approved the incorporation by reference of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.

(2) You must use this material as applicable to do the actions required by this AD, unless the AD specifies otherwise.

(i) Agência Nacional de Aviação Civil (ANAC) AD 2023-07-01, effective August 10, 2023, as corrected by ANAC Airworthiness Directive Errata, effective August 10, 2023.

(ii) [Reserved]

(3) For ANAC material identified in this AD, contact ANAC, Continuing Airworthiness Technical Branch (GTAC), Rua Doutor Orlando Feirabend Filho, 230—Centro Empresarial Aquarius—Torre B—Andares 14 a 18, Parque Residencial Aquarius, CEP 12.246-190—São José dos Campos—SP, Brazil; phone: 55 (12) 3203-6600; email: pac@anac.gov.br; website: anac.gov.br/en/. You may find this material on the ANAC website at sistemas.anac.gov.br/certificacao/DA/DAE.asp.

(4) You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110.

(5) You may view this material at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, visit www.archives.gov/federal-register/cfr/ibr-locations or email fr.inspection@nara.gov.

Rule preamble

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

DatesPage 1

This AD is effective November 12, 2024.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 12, 2024.

AddressesPage 1

AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA-2024-1484; 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 ANAC material identified in this AD, contact ANAC, Continuing Airworthiness Technical Branch (GTAC), Rua Doutor Orlando Feirabend Filho, 230—Centro Empresarial Aquarius—Torre B—Andares 14 a 18, Parque Residencial Aquarius, CEP 12.246-190—São José dos Campos—SP, Brazil; phone: 55 (12) 3203-6600; email: pac@anac.gov.br; website: anac.gov.br/en/. You may find this material on the ANAC website at sistemas.anac.gov.br/certificacao/DA/DAE.asp. It is also available at regulations.gov under Docket No. FAA-2024-1484.

• You may view this material at the FAA, Airworthiness Products Section, Operational Safety Branch, 901 Locust, Kansas City, MO 64106. For information on the availability of this material at the FAA, call (817) 222-5110. It is also available at regulations.gov under Docket No. FAA-2024-1484.

For further information contactPage 1

Jim Rutherford, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; phone: (816) 329-4165; email: jim.rutherford@faa.gov.

BackgroundPage 1

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain serial-numbered Embraer Model EMB-505 airplanes. The NPRM published in the Federal Register on June 20, 2024 (89 FR 51853). The NPRM was prompted by ANAC AD 2023-07-01, effective August 10, 2023, as corrected by ANAC Airworthiness Directive Errata, effective August 10, 2023 (ANAC AD 2023-07-01) (also referred to as the MCAI) issued by National Civil Aviation Agency of Brazil, which is the aviation authority for Brazil. The MCAI states that analysis identified that the LH refreshment center and LH forward cabinet might not withstand the loads expected for specific emergency landing conditions, which may cause the detachment of mass items and cause injuries to the airplane occupants. In addition, the MCAI includes errata to correct a printing error in the original English version of the MCAI. The MCAI requires installing structural reinforcements.

In the NPRM, the FAA proposed to require installing structural reinforcements, as specified in ANAC AD 2023-07-01. 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-2024-1484.

CommentsPage 1

The FAA received no comments on the NPRM or on the determination of the costs.

ConclusionPage 1

These products have been approved by the aviation authority of another country and are 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 these products. This AD is adopted as proposed in the NPRM.

Material Incorporated by Reference Under 1 CFR Part 51Page 1

The FAA reviewed ANAC AD 2023-07-01, which specifies procedures for installing structural reinforcements.

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 the ADDRESSES section.

Differences Between This AD and the MCAIPage 1

The material specified in ANAC AD 2023-07-01 allows the use of alternative or similar parts in place of the ones specified in the kits, provided these alternative or similar parts are approved by Embraer, but this AD requires approval from either the Manager, International Validation Branch, FAA; ANAC; or ANAC's authorized Designee.

Costs of CompliancePage 1

The FAA estimates that this AD affects 229 airplanes of U.S. registry.

The FAA estimates the following costs to comply with this AD:

Estimated Costs
ActionLabor costParts costCost per productCost on U.S. operators
Install structural reinforcements11 work-hours × $85 per hour = $935$1,600$2,535$580,515

The FAA has included all known costs in its cost estimate. According to the manufacturer, however, some or all of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected operators.

Authority for This 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 because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action.

Regulatory findingsPage 2

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 adding the following new airworthiness directive:

Affected TCDS · 1

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

Registered aircraft · 677

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
  • Embraer Executive531 aircraft
  • Embraer S A113 aircraft
  • Embraer-Empresa Brasileira De33 aircraft
By year built
20092026
Registered aircraft by year built: 619 aircraft
20091
201018
201126
201233
201333
201449
201544
201642
201734
201837
201939
202028
202132
202240
202350
202447
202538
202628

58 with no year recorded

By model

Aircraft

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