Rule2024-06817
Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes; Correction
Primary source
Metadata and text below are from the Federal Register, a public-domain U.S. government work. Always verify the official published version before relying on it for any legal matter.
Published
April 1, 2024
Effective
March 29, 2024
Issuing agencies
Transportation DepartmentFederal Aviation Administration
Abstract
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.
Full Text
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<title>Federal Register, Volume 89 Issue 63 (Monday, April 1, 2024)</title>
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[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 [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[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 <a href="http://regulations.gov">regulations.gov</a> 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:
<bullet> For material incorporated by reference in this AD, contact
EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221
8999 000; email <a href="/cdn-cgi/l/email-protection#f5b4b186b590948694db9080879a8594db9080"><span class="__cf_email__" data-cfemail="37767344775256445619524245584756195242">[email protected]</span></a>; website easa.europa.eu. You may
find this IBR material on the EASA website at ad.easa.europa.eu.
<bullet> 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
<a href="http://regulations.gov">regulations.gov</a> 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: <a href="/cdn-cgi/l/email-protection#702318111802111d5e34111e1503181d111e1419301611115e171f06"><span class="__cf_email__" data-cfemail="95c6fdf4fde7f4f8bbd1f4fbf0e6fdf8f4fbf1fcd5f3f4f4bbf2fae3">[email protected]</span></a>.
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:
<bullet> Accomplishing a functional check of an affected part.
<bullet> 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.)
<bullet> Reporting inspection (i.e., functional check) results to
the airplane manufacturer.
<bullet> 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: <a href="/cdn-cgi/l/email-protection#0e37234f585d234f475c23393d3e234f43414d4e686f6f20696178"><span class="__cf_email__" data-cfemail="94adb9d5c2c7b9d5ddc6b9a3a7a4b9d5d9dbd7d4f2f5f5baf3fbe2">[email protected]</span></a>. 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:
<a href="/cdn-cgi/l/email-protection#93c0fbf2fbe1f2febdd7f2fdf6e0fbfef2fdf7fad3f5f2f2bdf4fce5"><span class="__cf_email__" data-cfemail="cf9ca7aea7bdaea2e18baea1aabca7a2aea1aba68fa9aeaee1a8a0b9">[email protected]</span></a>.
(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
<a href="/cdn-cgi/l/email-protection#a7e6e3d4e7c2c6d4c689c2d2d5c8d7c689c2d2"><span class="__cf_email__" data-cfemail="0342477043666270622d6676716c73622d6676">[email protected]</span></a>; 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 <a href="http://www.archives.gov/federal-register/cfr/ibr-locations">www.archives.gov/federal-register/cfr/ibr-locations</a> or email <a href="/cdn-cgi/l/email-protection#5a3c28743334292a3f392e3335341a343b283b743d352c"><span class="__cf_email__" data-cfemail="5432267a3d3a27243137203d3b3a143a3526357a333b22">[email protected]</span></a>.
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
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