
[Federal Register Volume 88, Number 155 (Monday, August 14, 2023)]
[Proposed Rules]
[Pages 54944-54946]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-17354]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2023-1713; Project Identifier MCAI-2023-00781-T]
RIN 2120-AA64


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

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for certain ATR--GIE Avions de Transport R[eacute]gional Model ATR42-
500 and ATR72-212A airplanes. This proposed AD was prompted by reports 
of loose fasteners and cracks in the horizontal stabilizer (HS) left- 
and right-hand leading edge lateral ribs, the box in between, the 
center box upper panel, and HS forward back-up fitting. This proposed 
AD would require an inspection of the HS affected areas for 
discrepancies and applicable corrective action, as specified in a 
European Union Aviation Safety Agency (EASA), which is proposed for 
incorporation by reference (IBR). The FAA is proposing this AD to 
address the unsafe condition on these products.

DATES: The FAA must receive comments on this proposed AD by September 
28, 2023.

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-2023-1713; 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 NPRM, the mandatory continuing airworthiness 
information (MCAI), any comments received, and other information. The 
street address for Docket Operations is listed above.
    Material Incorporated by Reference:
     For EASA material that is proposed for IBR in this NPRM, 
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 material on the EASA website ad.easa.europa.eu. It is 
also available at regulations.gov under Docket No. FAA-2023-1713.
     For ATR--GIE Avions de Transport R[eacute]gional service 
information identified in this NPRM, contact ATR--GIE Avions de 
Transport R[eacute]gional, 1 All[eacute]e Pierre Nadot, 31712 Blagnac 
Cedex, France; telephone +33 (0) 5 62 21 62 21; fax +33 (0) 5 62 21 67 
18; email continued.airworthiness@atr aircraft.com; website atr-
aircraft.com.
     You may view this service information at the FAA, 
Airworthiness Products Section, Operational Safety Branch, 2200 South 
216th Street, Des Moines, WA. For information on the availability of 
this material at the FAA, call 206-231-3195.

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 this proposal. Send your comments to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2023-1713; Project Identifier 
MCAI-2023-00781-T'' at the beginning of your comments. The most helpful 
comments reference a specific portion of the proposal, 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 proposal 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 NPRM.

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 NPRM 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 NPRM, 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 NPRM. Submissions containing CBI should be sent to 
Shahram Daneshmandi, Aviation Safety Engineer, FAA, 1600 Stewart 
Avenue, Suite 410, Westbury, NY 11590; telephone 206-231-3220; email 
[email protected]. Any commentary that the FAA receives which 
is not specifically designated as CBI will be placed in the public 
docket for this rulemaking.

[[Page 54945]]

Background

    EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2023-0125, dated June 22, 2023 (EASA 
AD 2023-0125) (also referred to as the MCAI), to correct an unsafe 
condition for certain ATR--GIE Avions de Transport R[eacute]gional 
Model ATR42-500 and ATR72-212A airplanes. The MCAI states that several 
occurrences of loose fasteners and cracks on the HS left- and right-
hand leading edge lateral ribs, the box in between, the center box 
upper panel, and HS forward back-up fitting have been reported. 
Subsequent investigations identified possible manufacturing errors and 
a list of horizontal tail planes that could be affected by similar 
issues. This condition, if not detected and corrected, could reduce the 
structural integrity of the airplane.
    The FAA is proposing 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-2023-1713.

Related Service Information Under 1 CFR Part 51

    EASA AD 2023-0125 specifies procedures for a one-time detailed 
inspection of the HS left- and right-hand leading edge lateral ribs, 
the box in between, the center box upper panel, and HS forward back-up 
fitting for discrepancies (i.e., loose, missing, or incorrectly 
installed fasteners, composite delamination, and a cracked fitting); 
and applicable corrective action. The corrective action includes 
contacting the manufacturer for repair instructions if any discrepancy 
is detected during any inspection.
    ATR Service Bulletin ATR42-55-0020, dated March 2, 2023; and ATR 
Service Bulletin ATR72-55-1013, dated March 2, 2023; identify the 
affected airplane serial numbers.
    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 section.

FAA's Determination

    This product has been approved by the aviation authority of another 
country and is 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 and 
service information referenced above. The FAA is issuing this NPRM 
after determining that the unsafe condition described previously is 
likely to exist or develop in other products of the same type design.

Proposed AD Requirements in this NPRM

    This proposed AD would require accomplishing the actions specified 
in EASA AD 2023-0125 described previously, except for any differences 
identified as exceptions in the regulatory text of this proposed 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, the 
FAA proposes to incorporate EASA AD 2023-0125 by reference in the FAA 
final rule. This proposed AD would, therefore, require compliance with 
EASA AD 2023-0125 in its entirety through that incorporation, except 
for any differences identified as exceptions in the regulatory text of 
this proposed AD. Using common terms that are the same as the heading 
of a particular section in EASA AD 2023-0125 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 2023-
0125. Service information required by EASA AD 2023-0125 for compliance 
will be available at regulations.gov under Docket No. FAA-2023-1713 
after the FAA final rule is published.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would 
affect 16 airplanes of U.S. registry. The FAA estimates the following 
costs to comply with this proposed AD:
    Estimated costs for required actions

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                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
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8 work-hours x $85 per hour = $680...........................              $0             $680          $10,880
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    The FAA has received no definitive data on which to base the cost 
estimates for the on-condition repairs specified in this proposed AD.

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

    The FAA determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 this proposed 
regulation:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

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

[[Page 54946]]

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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  [Amended]

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

ATR--GIE Avions de Transport R[eacute]gional: Docket No. FAA-2023-
1713; Project Identifier MCAI-2023-00781-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by September 28, 2023.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to ATR--GIE Avions de Transport R[eacute]gional 
Model ATR42-500 and ATR72-212A airplanes, certificated in any 
category, as identified in ATR Service Bulletin ATR42-55-0020, dated 
March 2, 2023; or ATR Service Bulletin ATR72-55-1013, dated March 2, 
2023; as applicable.

(d) Subject

    Air Transport Association (ATA) of America Code: 55, 
Stabilizers.

(e) Unsafe Condition

    This AD was prompted by reports of loose fasteners and cracks in 
the horizontal stabilizer (HS) left- and right-hand leading edge 
lateral ribs, the box in between, the center box upper panel, and HS 
forward back-up fitting. The FAA is issuing this AD to address 
loose, missing, or incorrectly installed fasteners, composite 
delamination, and cracks in the HS. The unsafe condition, if not 
addressed, could result in reduced structural integrity of the 
airplane.

(f) Compliance

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

(g) Requirements

    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 
2023-0125, dated June 22, 2023 (EASA AD 2023-0125).

(h) Exceptions to EASA AD 2023-0125

    (1) Where paragraph (1) of EASA AD 2023-0125 refers to its 
effective date, this AD requires using the effective date of this 
AD.
    (2) Where paragraph (2) of EASA AD 2023-0125 specifies to 
``contact ATR for approved repair instructions and, within the 
compliance time specified therein, accomplish those instructions 
accordingly'' if any discrepancy is detected, for this AD if any 
crack is detected, the crack must be repaired before further flight 
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.
    (3) This AD does not adopt the ``Remarks'' section of EASA AD 
2023-0125.

(i) No Reporting Requirement

    Although the service information referenced in EASA AD 2023-0125 
specifies to submit certain information to the manufacturer, this AD 
does not include that requirement.

(j) 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 International 
Validation Branch, send it to the attention of the person identified 
in paragraph (k) 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.

(k) 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].

(l) 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.
    (i) European Union Aviation Safety Agency (EASA) AD 2023-0125, 
dated June 22, 2023.
    (ii) ATR Service Bulletin ATR42-55-0020, dated March 2, 2023.
    (iii) ATR Service Bulletin ATR72-55-1013, dated March 2, 2023.
    (3) For EASA AD 2023-0125, 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 
AD on the EASA website ad.easa.europa.eu.
    (4) For ATR service information identified in this AD, contact 
ATR--GIE Avions de Transport R[eacute]gional, 1 All[eacute]e Pierre 
Nadot, 31712 Blagnac Cedex, France; telephone +33 (0) 5 62 21 62 21; 
fax +33 (0) 5 62 21 67 18; email continued.airworthiness@atr 
aircraft.com; website atr-aircraft.com.
    (5) You may view this material at the FAA, Airworthiness 
Products Section, Operational Safety Branch, 2200 South 216th 
Street, Des Moines, WA. For information on the availability of this 
material at the FAA, call 206-231-3195.
    (6) 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 
[email protected], or go to: www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on August 8, 2023.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2023-17354 Filed 8-11-23; 8:45 am]
BILLING CODE 4910-13-P


