[Federal Register Volume 89, Number 63 (Monday, April 1, 2024)]
[Rules and Regulations]
[Pages 22333-22334]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-06817]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-0459; Project Identifier MCAI-2024-00117-T; 
Amendment 39-22696; AD 2024-05-05]
RIN 2120-AA64


Airworthiness Directives; ATR--GIE Avions de Transport 
R[eacute]gional Airplanes; Correction

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comment; correction.

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SUMMARY: The FAA is correcting an airworthiness directive (AD) that was 
published in the Federal Register. That AD applies to all ATR-GIE 
Avions de Transport Regional Model ATR42 and ATR72 airplanes. As 
published, the effective, incorporation by reference approval, and 
comment submittal dates specified in the preamble of the preceding 
correction are incorrect. This document corrects those errors. In all 
other respects, the original document remains the same.

DATES: This correction is effective March 29, 2024. The effective date 
of AD 2024-05-05 remains March 29, 2024. The date for submitting 
comments on AD 2024-05-05 remains April 29, 2024.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of March 29, 
2024 (89 FR 18534, March 14, 2024; corrected March 26, 2024 (89 FR 
20849)).

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2024-0459; 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; request for comment; correction, 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 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 IBR 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. It is also available in the AD docket at 
regulations.gov under Docket No. FAA-2024-0459.

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:

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about AD 2024-05-05. Submit comments as instructed in AD 
2024-05-05, Amendment 39-22696 (89 FR 18534, March 14, 2024; corrected 
March 26, 2024 (89 FR 20849)) (AD 2024-05-05).

Background

    AD 2024-05-05 requires accomplishing a functional check of an 
affected part, replacing an affected part if necessary, and reporting 
the functional check results, and prohibits the installation of 
affected parts. That AD applies to all ATR--GIE Avions de Transport 
R[eacute]gional Model ATR42 and ATR72 airplanes.

Need for the Correction

    As published, the effective, incorporation by reference approval, 
and comment submittal dates specified in the preamble of the preceding 
correction to AD 2024-05-05 are incorrect. The correct effective and 
incorporation by reference approval date is March 29, 2024. The correct 
date for submitting comments is April 29, 2024.

Related Service Information Under 1 CFR Part 51

    EASA Emergency AD 2024-0044-E specifies the following procedures:
     Accomplishing a functional check of an affected part.
     Replacing an affected part with a serviceable part, if any 
discrepancy is detected during the functional check. (A discrepancy is 
any amount of air that flows through either connector of the right 
engine extinguishing system when compressed air is passed through 
either connector of the left engine extinguishing system, and vice 
versa.)
     Reporting inspection (i.e., functional check) results to 
the airplane manufacturer.
     Prohibiting the installation of affected parts.
    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.

Correction of Publication

    This document corrects errors in the preceding correction to AD 
2024-05-05 and correctly adds the AD as an amendment to 14 CFR 39.13. 
Although no other part of the preamble or regulatory information has 
been corrected, the FAA is publishing the entire rule in the Federal 
Register.
    The effective date of this AD remains March 29, 2024.
    Since this action only corrects the preceding correction for AD 
2024-05-05, it has no adverse economic impact and imposes no additional 
burden on any person. Therefore, the FAA has determined that notice and 
public procedures are unnecessary.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

    Accordingly, pursuant to the authority delegated to me by the

[[Page 22334]]

Administrator, the FAA amends part 39 of the Federal Aviation 
Regulations (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  [Corrected]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive:

2024-05-05 ATR--GIE Avions de Transport R[eacute]gional: Amendment 
39-22696; Docket No. FAA-2024-0459; Project Identifier MCAI-2024-
00117-T.

(a) Effective Date

    This airworthiness directive (AD) is effective March 29, 2024.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all ATR--GIE Avions de Transport 
R[eacute]gional airplanes specified in paragraphs (c)(1) and (2) of 
this AD, certificated in any category.
    (1) Model ATR42-200, -300, -320, and -500 airplanes.
    (2) Model ATR72-101, -102, -201, -202, -211, -212, and -212A 
airplanes.

(d) Subject

    Air Transport Association (ATA) of America Code 26, Fire 
Protection.

(e) Unsafe Condition

    This AD was prompted by a report of incorrect marking and 
assembly of the two-way valves for the left- and right-hand engine 
fire extinguishing systems. The FAA is issuing this AD to address 
inoperative two-way valves in both engine fire extinguishing 
systems. This condition, if not addressed, could lead to reduced 
performance of the engine fire extinguishing system, which could 
result in loss of control of the airplane.

(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, European Union Aviation Safety Agency (EASA) 
Emergency AD 2024-0044-E, dated February 15, 2024 (EASA AD 2024-
0044-E).

(h) Exceptions to EASA AD 2024-0044-E

    (1) Where EASA AD 2024-0044-E refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) Paragraph (4) of EASA AD 2024-0044-E specifies to report 
inspection results to ATR--GIE Avions de Transport R[eacute]gional 
within a certain compliance time. For this AD, report inspection 
(i.e., functional check) results at the applicable time specified in 
paragraph (h)(2)(i) or (ii) of this AD.
    (i) If the inspection was done on or after the effective date of 
this AD: Submit the report within 30 days after the inspection.
    (ii) If the inspection was done before the effective date of 
this AD: Submit the report within 30 days after the effective date 
of this AD.
    (3) This AD does not adopt the ``Remarks'' section of EASA AD 
2024-0044-E.

(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 manager of the 
International Validation Branch, mail it to the address 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 ATR--GIE Avions de Transport 
R[eacute]gional's 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 (IBR) 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.
    (3) The following service information was approved for IBR on 
March 29, 2024 (89 FR 18534, March 14, 2024; corrected March 26, 
2024 (89 FR 20849)).
    (i) European Union Aviation Safety Agency (EASA) Emergency AD 
2024-0044-E, dated February 15, 2024.
    (ii) [Reserved]
    (4) For EASA AD 2024-0044-E, 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 
ADs on the EASA website at ad.easa.europa.eu.
    (5) 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.
    (6) 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 [email protected].

    Issued on March 27, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2024-06817 Filed 3-29-24; 8:45 am]
BILLING CODE 4910-13-P