AD 2021-20-14

Airworthiness directive · Equipment/Furnishings · Dassault Falcon 7X, Falcon 900EX and FALCON 2000EX

Effective
November 18, 2021
Published
October 14, 2021 · 86 FR 57022–57024
Issued
September 21, 2021
Models
Falcon 7X, Falcon 900EX, FALCON 2000EX
Registered aircraft
754 matched by model
Product
Aircraft · Large airplane
ATA chapter
25 · Equipment and furnishings
Amendment
39-21752
Docket
FAA-2021-0569
Project
MCAI-2020-01692-T
Issued as
Final rule

Unofficial copy from the Federal Register XML, document 2021-22294. Only the govinfo PDF is the legal edition. DRS record last changed May 30, 2024.

On this page

Summary

The FAA is adopting a new airworthiness directive (AD) for all Dassault Aviation Model FALCON 7X, FALCON 900EX, and FALCON 2000EX airplanes. This AD was prompted by a report of a manufacturing issue involving misalignment of a cabin seat pin and plate that can prevent the recline locking mechanism from properly engaging when the seat is in taxi, take-off, or landing position. This AD requires an inspection of certain cabin seats for discrepancies and corrective action, as specified in 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.

The airworthiness directive

2021-20-14 Dassault Aviation: Amendment 39-21752; Docket No. FAA-2021-0569; Project Identifier MCAI-2020-01692-T.

(a) Effective Date

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This airworthiness directive (AD) is effective November 18, 2021.

(b) Affected ADs

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None.

(c) Applicability

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This AD applies to all Dassault Aviation Model FALCON 7X, FALCON 900EX, and FALCON 2000EX airplanes, certificated in any category.

(d) Subject

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Air Transport Association (ATA) of America Code 25, Equipment/Furnishings.

(e) Reason

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This AD was prompted by a report of a manufacturing issue involving misalignment of a seat pin and plate that can prevent the recline locking mechanism from properly engaging when the seat is in taxi, take-off, or landing position. The FAA is issuing this AD to address cabin seats having improper or no engagement of the recline locking mechanism during taxi, take-off, or landing, which could result in reduced seat performance under crash loads and possible injury to seat occupants.

(f) Compliance

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

(g) Requirements

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Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, European Union Aviation Safety Agency (EASA) AD 2020-0284, dated December 18, 2020 (EASA AD 2020-0284).

(h) Exceptions to EASA AD 2020-0284

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(1) Where EASA AD 2020-0284 refers to its effective date, this AD requires using the effective date of this AD.

(2) This AD does not mandate compliance with the “Remarks” section of EASA AD 2020-0284.

(3) Where paragraph (2) of EASA AD 2020-0284 specifies action if “any discrepancy” is detected for this AD, a discrepancy is a gap between the seat pin and plate.

(i) No Reporting Requirement

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Although the service information referenced in EASA AD 2020-0284 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

(j) Additional AD Provisions

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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 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) 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, Large Aircraft Section, International Validation Branch, FAA; or EASA; or Dassault Aviation's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature.

(k) Related Information

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For more information about this AD, contact Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226; email tom.rodriguez@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 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 2020-0284, dated December 18, 2020.

(ii) [Reserved]

(3) For EASA AD 2020-0284, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https://ad.easa.europa.eu.

(4) 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.

(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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

Rule preamble

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

DatesPage 1

This AD is effective November 18, 2021.

The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of November 18, 2021.

AddressesPage 2

For material incorporated by reference (IBR) in this AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this IBR material on the EASA website at https://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. It is also available in the AD docket at https://www.regulations.gov by searching for and locating Docket No. FAA-2021-0569.

For further information contactPage 2

Tom Rodriguez, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3226; email tom.rodriguez@faa.gov.

BackgroundPage 2

EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2020-0284, dated December 18, 2020 (EASA AD 2020-0284) (also referred to as the MCAI), to correct an unsafe condition for Dassault Aviation Model FALCON 7X, FALCON 900EX, and FALCON 2000EX airplanes.

The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to Dassault Aviation Model FALCON 7X, FALCON 900EX, and FALCON 2000EX airplanes. The NPRM published in the Federal Register on July 15, 2021 (86 FR 37255). The NPRM was prompted by a report of a manufacturing issue involving misalignment of a cabin seat pin and plate that can prevent the recline locking mechanism from properly engaging when the seat is in taxi, take-off, or landing position. The NPRM proposed to require an inspection of certain cabin seats for discrepancies and corrective action, as specified in EASA AD 2020-0284.

The FAA is issuing this AD to address cabin seats having improper or no engagement of the recline locking mechanism during taxi, take-off, or landing, which could result in reduced seat performance under crash loads and possible injury to seat occupants. See the MCAI for additional background information.

CommentsPage 2

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

ConclusionPage 2

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. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products.

Related Service Information Under 1 CFR Part 51Page 2

EASA AD 2020-0284 specifies procedures for an inspection of certain cabin seats for discrepancies (a gap between the seat pin and plate), and corrective action (adjustment, deactivation, or repair), as applicable. EASA AD 2020-0284 also prohibits installation of certain cabin seats. 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.

Costs of CompliancePage 2

The FAA estimates that this AD affects 565 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD:

Estimated Costs for Required Actions
Labor costParts costCost per productCost on U.S. operators
1 work-hour × $85 per hour = $85None$85$48,025

The FAA estimates the following costs to do any necessary on-condition adjustments or deactivations 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 costParts costCost per product
1 work-hour × $85 per hour = $85$0$85

The FAA has received no definitive data on which to base the cost estimates for the on-condition repairs specified in this AD.

According to the manufacturer, some or all of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected operators. The FAA does not control warranty coverage for affected operators. As a result, the FAA has included all known costs in the cost estimate.

Authority for This RulemakingPage 3

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 3

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 3

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

Adoption of the amendmentPage 3

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 · 3

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

Registered aircraft · 754

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
  • Dassault754 aircraft
By year built
19882026
Registered aircraft by year built: 722 aircraft
19881
19951
19967
199713
199816
199916
20009
200114
200212
200319
200434
200529
200634
200753
200862
200946
201026
201140
201233
201343
201431
201540
201621
201715
201820
201916
202014
202115
20227
202313
202410
202510
20262

32 with no year recorded

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