2024-03137. Airworthiness Directives; Airbus Helicopters  

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    AGENCY:

    Federal Aviation Administration (FAA), DOT.

    ACTION:

    Final rule; request for comments.

    SUMMARY:

    The FAA is adopting a new airworthiness directive (AD) for certain Airbus Helicopters Model EC225LP helicopters. This AD was prompted by a report of incorrect door opening instructions on the placards located on the right hand (RH) side of the VIP flap door. This AD requires installing a placard specifying jettisoning instructions, 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 March 1, 2024.

    The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of March 1, 2024.

    The FAA must receive comments on this AD by April 1, 2024.

    ADDRESSES:

    You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:

    Federal eRulemaking Portal: Go to regulations.gov. Follow the instructions for submitting comments.

    Fax: (202) 493–2251.

    Mail: U.S. Department of Transportation, Docket Operations, M–30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590.

    Hand Delivery: Deliver to Mail address above between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays.

    AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2024–0039; 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 EASA AD, any comments received, and other information. The street address for Docket Operations is listed above.

    Material Incorporated by Reference:

    • For EASA material incorporated by reference in this final rule, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu. You may find this material on the EASA website at https://ad.easa.europa.eu.

    • You may view this material at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. For information on the availability of this material at the FAA, call (817) 222–5110. The EASA material is also available at regulations.gov under Docket No. FAA–2024–0039.

    Other Related Service Information: For Airbus Helicopters service information identified in this final rule, contact Airbus Helicopters, 2701 North Forum Drive, Grand Prairie, TX 75052; telephone (972) 641–0000 or (800) 232–0323; fax (972) 641–3775; or at airbus.com/en/products-services/helicopters/hcare-services/airbusworld. You may also view this service information at the FAA contact information under Material Incorporated by Reference above.

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    FOR FURTHER INFORMATION CONTACT:

    William McCully, Aviation Safety Engineer, FAA, International Validation Branch, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; phone (404) 474–5548; email william.mccully@faa.gov.

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    SUPPLEMENTARY INFORMATION:

    Comments Invited

    The FAA invites you to send any written data, views, or arguments about this final rule. Send your comments to an address listed under ADDRESSES . Include “Docket No. FAA–2024–0039; Project Identifier MCAI–2023–00966–R” at the beginning of your comments. The most helpful comments reference a specific portion of the final rule, explain the reason for any recommended change, and include supporting data. The FAA will consider all comments received by the closing date and may amend this final rule because of those comments.

    Except for Confidential Business Information (CBI) as described in the following paragraph, and other information as described in 14 CFR 11.35, the FAA will post all comments received, without change, to regulations.gov, including any personal information you provide. The agency will also post a report summarizing each substantive verbal contact received about this final rule.

    Confidential Business Information

    CBI is commercial or financial information that is both customarily and actually treated as private by its owner. Under the Freedom of Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public disclosure. If your comments responsive to this AD contain commercial or financial information that is customarily treated as private, that you actually treat as private, and that is relevant or responsive to this AD, it is important that you clearly designate the submitted comments as CBI. Please mark each page of your submission containing CBI as “PROPIN.” The FAA will treat such marked submissions as confidential under the FOIA, and they will not be placed in the public docket of this AD. Submissions containing CBI should be sent to William McCully, Aviation Safety Engineer, FAA, International Validation Branch, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; phone (404) 474–5548; email william.mccully@faa.gov. Any commentary that the FAA receives which is not specifically designated as CBI will be placed in the public docket for this rulemaking.

    Background

    EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2022–0072, dated April 26, 2022 (EASA AD 2022–0072), to correct an unsafe condition on Airbus Helicopters Model EC 225 LP helicopters, serial numbers 2650, 2651, 2653, 2684, 2712, and 2796.

    This AD was prompted by a report that placards located on the RH side of the VIP flap door of the passenger cabin do not provide adequate door opening instructions necessary to operate the RH side VIP flap door in case of the helicopter ditching. The unsafe condition, if not addressed, could prevent jettisoning of the RH side VIP flap door during an emergency situation, possibly obstructing evacuation and resulting in injury to occupants.

    You may examine the EASA AD in the AD docket at regulations.gov under Docket No. FAA–2024–0039.

    Related Service Information Under 1 CFR Part 51

    EASA AD 2022–0072 requires installing a placard over the current placard, which correctly specifies Start Printed Page 11719 jettisoning instructions for the RH side of the VIP flap door.

    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 .

    Other Related Service Information

    The FAA reviewed Airbus Helicopters Alert Service Bulletin (ASB) No. EC225–52A023, Revision 0, dated January 22, 2020 for Model EC225LP helicopters. This service information specifies instructions for covering the existing incorrect placard with a correct placard, and reporting certain information to the manufacturer.

    FAA's Determination

    These helicopters have been approved by EASA and are approved for operation in the United States. Pursuant to the FAA's bilateral agreement with the European Union, EASA has notified the FAA about the unsafe condition described in its AD. The FAA is issuing this AD after evaluating all known relevant information and determining that the unsafe condition described previously is likely to exist or develop on other helicopters of the same type design.

    AD Requirements

    This AD requires accomplishing the actions specified in EASA AD 2022–0072, described previously, as incorporated by reference, except for any differences identified as exceptions in the regulatory text of this AD and except as discussed under “Differences Between this AD and the EASA AD.”

    Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD process, the FAA developed a process to use some civil aviation authority (CAA) ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has been coordinating this process with manufacturers and CAAs. As a result, EASA AD 2022–0072 will be incorporated by reference in this FAA final rule. This AD would, therefore, require compliance with EASA AD 2022–0072 in its entirety through that incorporation, except for any differences identified as exceptions in the regulatory text of this AD. Using common terms that are the same as the heading of a particular section in EASA AD 2022–0072 does not mean that operators need comply only with that section. For example, where the AD requirement refers to “all required actions and compliance times,” compliance with this AD requirement is not limited to the section titled “Required Action(s) and Compliance Time(s)” in EASA AD 2022–0072. Service information referenced in EASA AD 2022–0072 for compliance will be available at regulations.gov under Docket No. FAA–2024–0039.

    Differences Between This AD and the EASA AD

    Service information referenced in EASA AD 2022–0072 specified reporting certain information to Airbus Helicopters, including sending pictures, whereas this AD does not require reporting any information or sending any pictures.

    Justification for Immediate Adoption and Determination of the Effective Date

    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 thirty days, upon a finding of good cause.

    There are currently no domestic operators of these products. Accordingly, notice and opportunity for prior public comment are unnecessary, pursuant to 5 U.S.C. 553(b)(3)(B). In addition, for the foregoing reasons, 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.

    Regulatory Flexibility Act

    The requirements of the Regulatory Flexibility Act (RFA) do not apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt a rule without prior notice and comment. Because the FAA has determined that it has good cause to adopt this rule without prior notice and comment, RFA analysis is not required.

    Costs of Compliance

    There are no costs of compliance with this AD because there are no helicopters with this type certificate on the U.S. Registry.

    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, and

    (2) Will not affect intrastate aviation in Alaska.

    Start List of Subjects

    List of Subjects in 14 CFR Part 39

    • Air transportation
    • Aircraft
    • Aviation safety
    • Incorporation by reference
    • Safety
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    The Amendment

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

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    PART 39—AIRWORTHINESS DIRECTIVES

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

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    Authority: 49 U.S.C. 106(g), 40113, 44701.

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    [Amended]
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    2. The FAA amends § 39.13 by adding the following new airworthiness directive:

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    2024–02–01 Airbus Helicopters:  Amendment 39–22665; Docket No. FAA–2024–0039; Project Identifier MCAI–2023–00966–R.

    (a) Effective Date

    This airworthiness directive (AD) is effective March 1, 2024. Start Printed Page 11720

    (b) Affected ADs

    None.

    (c) Applicability

    This AD applies to Airbus Helicopters Model EC225LP helicopters, serial numbers 2650, 2651, 2653, 2684, 2712, and 2796, certificated in any category.

    (d) Subject

    Joint Aircraft System Component (JASC) Code: 5210, Passenger crew doors.

    (e) Unsafe Condition

    This AD was prompted by a report of incorrect door opening instructions on the placard located on the right-hand (RH) side of the VIP flap door. The FAA is issuing this AD to address and correct placards on the RH side VIP flap door. The unsafe condition, if not addressed, could prevent jettisoning of the RH side VIP flap door during an emergency situation, possibly obstructing evacuation and resulting in injury to occupants.

    (f) Compliance

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

    (g) Required Actions

    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, European Union Aviation Safety Agency (EASA) AD 2022–0072, dated April 26, 2022 (EASA AD 2022–0072).

    (h) Exceptions to EASA AD 2022–0072

    (1) Where EASA AD 2022–0072 refers to its effective date, this AD requires using the effective date of this AD.

    (2) Where EASA AD 2022–0072 refers to flight hours, this AD requires using hours time-in-service.

    (3) Where the paragraph defined as placard installation in EASA AD 2022–0072 states “in accordance with the instructions of the ASB,” for this AD, replace that text with “in accordance with the Accomplishment Instructions, paragraph 3.B of the ASB.”

    (i) No Reporting Requirement

    Although the service information referenced in EASA AD 2022–0072 specifies to submit certain information to the manufacturer, this AD does not include that requirement.

    (j) 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 § 39.19. In accordance with § 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, 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.

    (1) 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) Related Information

    For more information about this AD, contact William McCully, Aviation Safety Engineer, FAA, International Validation Branch, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 11590; phone (404) 474–5548; email william.mccully@faa.gov.

    (l) 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 the AD specifies otherwise.

    (i) European Union Aviation Safety Agency (EASA) AD 2022–0072, dated April 26, 2022.

    (ii) [Reserved]

    (3) For EASA AD 2022–0072, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet easa.europa.eu. You may find the EASA material on the EASA website at ad.easa.europa.eu.

    (4) You may view this service information at the FAA, Office of the Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N–321, Fort Worth, TX 76177. 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.

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    Issued on January 24, 2024.

    Victor Wicklund,

    Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service.

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    [FR Doc. 2024–03137 Filed 2–14–24; 8:45 am]

    BILLING CODE 4910–13–P

Document Information

Effective Date:
3/1/2024
Published:
02/15/2024
Department:
Federal Aviation Administration
Entry Type:
Rule
Action:
Final rule; request for comments.
Document Number:
2024-03137
Dates:
This AD is effective March 1, 2024.
Pages:
11718-11720 (3 pages)
Docket Numbers:
Docket No. FAA-2024-0039, Project Identifier MCAI-2023-00966-R, Amendment 39-22665, AD 2024-02-01
RINs:
2120-AA64: Airworthiness Directives
RIN Links:
https://www.federalregister.gov/regulations/2120-AA64/airworthiness-directives
Topics:
Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety
PDF File:
2024-03137.pdf
Supporting Documents:
» U.S. DOT/FAA - Supplemental AD Documents
CFR: (1)
14 CFR 39.13