Airworthiness Directives; ATR-GIE Avions de Transport Régional Airplanes, 97477-97480 [2024-28789]

Download as PDF Federal Register / Vol. 89, No. 236 / Monday, December 9, 2024 / Rules and Regulations certification for failure to participate in an audit. § § 4270.16–4270.98 § 4270.99 [Reserved] OMB control number. FOR FURTHER INFORMATION CONTACT: The information collection requirements in this part are approved by the Office of Management and Budget (OMB) and assigned OMB control number 0570–0083. Xochitl Torres Small, Deputy Secretary, United States Department of Agriculture. Susan Woolard, Regulations Management Division, Rural Development Innovation Center, U.S. Department of Agriculture, 1400 Independence Ave. SW, Stop 1522, Washington, DC 20250; telephone (202) 720–9631; email susan.woolard@ usda.gov. Rural Utilities Service Rural Development’s Rural BusinessCooperative Service, Rural Housing Service, and Rural Utilities Service are issuing corrections to the final rule that published September 30, 2024, at 89 FR 79698. Rural Housing Service List of Subjects in 7 CFR Part 5001 SUPPLEMENTARY INFORMATION: [FR Doc. 2024–28431 Filed 12–6–24; 8:45 am] BILLING CODE 3410–XY–P DEPARTMENT OF AGRICULTURE Business and industry, Community facility, Energy efficiency improvement, Loan programs, Renewable energy, Rural areas, Rural development, Water and waste disposal. In FR Doc. 2024–21920 published September 30, 2024, beginning on page 79698, make the following corrections: ■ 1. On page 79699, in the third column, item 11, the title is corrected to read ‘‘11. § 5001.116 Ineligible CF Projects’’. Rural Business-Cooperative Service 7 CFR Part 5001 [Docket No. RUS–19–Agency–0030] RIN 0572–AC56 OneRD Guaranteed Loan Regulation Rural Business-Cooperative Service, Rural Housing Service, Rural Utilities Service, USDA. ACTION: Final rule, correction and correcting amendments. AGENCY: VerDate Sep<11>2014 15:13 Dec 06, 2024 Jkt 265001 2. On page 79702, in the third column, item 39a, is corrected to read: ■ a. § 5001.516(c) is updated to inform lenders that payment of real estate taxes is considered a protective advance but does not require advanced Agency approval. § 5001.3 Definitions. * * * * * Affiliate means a person that is connected with or controlled by another organization. Factors such as ownership, management, current and previous relationships with or ties to another person, and contractual relationships, may be considered in determining whether affiliation exists. Affiliation is determined using the principles outlined in 13 CFR 121.301(f). * * * * * ■ 3. Amend § 5001.516 by revising paragraph (c) to read as follows: § 5001.516 Protective advances. * * * * * (c) A lender must obtain written Agency approval for any protective advance that will cumulatively amount to more than $200,000, or 10 percent of the aggregate outstanding balance of principal and interest, whichever is less, to the same borrower. Payment of real estate taxes by the lender is considered a protective advance, subject to the requirements of this section, and does not require Agency advance approval. Basil I. Gooden, Deputy Under Secretary, Rural Development. [FR Doc. 2024–28031 Filed 12–6–24; 8:45 am] BILLING CODE 3410–15–P ■ On September 30, 2024, Rural Development’s Rural BusinessCooperative Service, Rural Housing Service, and Rural Utilities Service, agencies of the United States Department of Agriculture (USDA), published a final rule with comment for the OneRD Guarantee Loan Program (OneRD). The final rule made necessary revisions to the policy and procedures that strengthened the oversight and management of the growing Community Facilities, Water and Waste Disposal, Business and Industry, and Rural Energy for America guarantee portfolios. The final rule had a misspelled subject heading in the preamble. The final rule also contained information in an instruction that was not ultimately in the final rule, an incomplete definition of affiliate, and a misstatement regarding protective advances. This document corrects the final regulation. DATES: This rule is effective December 9, 2024. ADDRESSES: Address all comments concerning this correction to Susan Woolard, Regulations Management Division, Rural Development Innovation Center, U.S. Department of Agriculture, SUMMARY: ddrumheller on DSK120RN23PROD with RULES1 1400 Independence Ave. SW, Stop 1522, Washington, DC 20250; telephone (202) 720–9631; email susan.woolard@ usda.gov. 97477 3. On page 79704, in the third column, Instruction 4 for § 5001.3, is corrected by removing the words ‘‘commercially available’’. ■ 4. On page 79711, in the second column, Instruction 14 is corrected to read: ■ 14. Amend § 5001.106 by revising the first sentence of the introductory text, paragraphs (d)(2), (e)(2) and (e)(3) introductory text to read as follows: For the reasons discussed in the preamble, 7 CFR 5001 is corrected by making the following correcting amendments: DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2024–2129; Project Identifier MCAI–2024–00066–T; Amendment 39–22889; AD 2024–23–10] RIN 2120–AA64 ■ PART 5001—GUARANTEED LOANS. 1. The authority citation for part 5001 continues to read as follows: ■ Authority: 5 U.S.C. 301; 7 U.S.C. 1926(a); 7 U.S.C. 1932(a); and 7 U.S.C. 8107. 2. Amend § 5001.3 by revising the definition of ‘‘affiliate’’ to read as follows: ■ PO 00000 Frm 00019 Fmt 4700 Sfmt 4700 Airworthiness Directives; ATR—GIE Avions de Transport Régional Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: The FAA is adopting a new airworthiness directive (AD) for certain ATR—GIE Avions de Transport Régional Model ATR42 and ATR72 airplanes. This AD was prompted by a report that for airplanes converted from passenger to cargo configuration using certain supplemental type certificates, no height limitation for the cargo, when loaded in the cargo compartment, is defined, and that as a consequence, cargo might be loaded up to the ceiling of the cargo compartment. This AD SUMMARY: E:\FR\FM\09DER1.SGM 09DER1 97478 Federal Register / Vol. 89, No. 236 / Monday, December 9, 2024 / Rules and Regulations requires modification of the cargo compartment and implementation of updated cargo loading procedures. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective January 13, 2025. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of January 13, 2025. ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2024–2129; 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 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 Sabena Technics material identified in this AD, contact Sabena Technics BGC, Le Galilée, 9 Bd Henri Ziegler, 31700 Blagnac France; telephone 33 (0)1 56 54 42 30; email airworthiness.office@ sabenatechnics.com. • 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 at regulations.gov under Docket No. FAA–2024–2129. FOR FURTHER INFORMATION CONTACT: Shahram Daneshmandi, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206–231–3220; email shahram.daneshmandi@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain ATR—GIE Avions de Transport Régional Model ATR42 and ATR72 airplanes. The NPRM published in the Federal Register on August 22, 2024 (89 FR 67908). The NPRM was prompted by AD 2024–0025, dated January 24, 2024, issued by the European Union Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union (referred to after this as the MCAI). The MCAI states that it was identified that for airplanes converted from passenger to cargo configuration using EASA Supplemental Type Certificate (STC) 10069551, Revision 1 (EASA STC 10069551, Revision 0, corresponds to FAA STC ST04602NY), or the previous EASA STC 2004–2872 (which corresponds to FAA STC S116– 004NM, Revision 1), no height limitation for the cargo, when loaded in the cargo compartment, is defined. Consequently, operators of such airplanes may load the cargo up to the ceiling of the cargo compartment and, therefore, potentially affect the proper functioning of the smoke detectors. This condition, if not corrected, could lead to smoke not being detected in time, possibly resulting in an uncontrolled fire. In the NPRM, the FAA proposed to require modification of the cargo compartment and implementation of updated cargo loading procedures. The FAA is issuing 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–2024–2129. Discussion of Final Airworthiness Directive Comments The FAA received a comment from Air Line Pilots Association, International (ALPA), who supported the NPRM without change. Conclusion 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 referenced above. The FAA reviewed the relevant data, considered the comments received, and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on this product. 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. Material Incorporated by Reference Under 1 CFR Part 51 The FAA reviewed Sabena Technics Airworthiness Technical Instructions 0110–09–A–ATI–F01–R00, and 0110– 11–A–ATI–F01–R00, both dated September 19, 2023. This material describes procedures for modifying the cargo compartment (installing a label and tape to indicate maximum cargo height). These documents are distinct since they apply to different airplane models. The FAA also reviewed Sabena Technics Weight & Balance Manual Supplement 0110–09–A–2305–R06, Revision 06, dated September 15, 2023; and Sabena Technics Weight & Balance Manual Supplement 0110–11–A–2305– R07, Revision 07, dated September 15, 2023. The maximum cargo height in the cargo compartment is described in Section 2.9., ‘‘Cargo Compartment— Loading Limitation,’’ of Sabena Technics Weight & Balance Manual Supplement 0110–09–A–2305–R06, Revision 06, dated September 15, 2023; and section 2.11., ‘‘Cargo CompartmentLoading Limitation,’’ of Sabena Technics Weight & Balance Manual Supplement 0110–11–A–2305–R07, Revision 07, dated September 15, 2023. These documents are distinct since they apply to different airplane models. 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 Compliance The FAA estimates that this AD affects 2 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: ddrumheller on DSK120RN23PROD with RULES1 ESTIMATED COSTS FOR REQUIRED ACTIONS Labor cost Parts cost Cost per product Cost on U.S. operators 8 work-hours × $85 per hour = $680 ...................................................................................... $100 $780 $1,560 The FAA has included all known costs in its cost estimate. According to VerDate Sep<11>2014 15:13 Dec 06, 2024 Jkt 265001 the manufacturer, however, some or all of the costs of this AD may be covered PO 00000 Frm 00020 Fmt 4700 Sfmt 4700 under warranty, thereby reducing the cost impact on affected operators. E:\FR\FM\09DER1.SGM 09DER1 Federal Register / Vol. 89, No. 236 / Monday, December 9, 2024 / Rules and Regulations 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, (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. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. The Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: ddrumheller on DSK120RN23PROD with RULES1 PART 39—AIRWORTHINESS DIRECTIVES 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. § 39.13 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive: ■ VerDate Sep<11>2014 15:13 Dec 06, 2024 Jkt 265001 2024–23–10 ATR—GIE Avions de Transport Régional: Amendment 39– 22889; Docket No. FAA–2024–2129; Project Identifier MCAI–2024–00066–T. (a) Effective Date This airworthiness directive (AD) is effective January 13, 2025. (b) Affected ADs None. (c) Applicability This AD applies to ATR—GIE Avions de Transport Régional airplanes identified in paragraphs (c)(1) and (2) of this AD, certificated in any category, modified in accordance with FAA Supplemental Type Certificate (STC) ST116–004NM or STC ST04602NY. (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 11, Placards and Marking. (e) Unsafe Condition This AD was prompted by a report that for airplanes converted from passenger to cargo configuration using certain supplemental type certificates, no height limitation for the cargo, when loaded in the cargo compartment, is defined, and that as a consequence, cargo may be loaded up to the ceiling of the cargo compartment. The FAA is issuing this AD to address cargo being loaded up to the ceiling of the cargo compartment, which could affect the proper functioning of the smoke detectors. This condition, if not corrected, could lead to smoke not being detected in time, possibly resulting in an uncontrolled fire. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Modification of Cargo Compartment Within 6 months after the effective date of this AD, modify the cargo compartment in accordance with the Accomplishment Instructions of Sabena Technics Airworthiness Technical Instructions 0110– 09–A–ATI–F01–R00, dated September 19, 2023 (for Model ATR42 airplanes); or Sabena Technics Airworthiness Technical Instructions 0110–11–A–ATI–F01–R00, dated September 19, 2023 (for Model ATR72 airplanes). (h) Revision of Weight and Balance Manual Prior to or concurrently with accomplishing the actions required by paragraph (g) of this AD, implement the cargo loading procedures specified in Section 2.9., ‘‘Cargo Compartment—Loading Limitation,’’ of Sabena Technics Weight & Balance Manual Supplement 0110–09–A–2305–R06, Revision 06, dated September 15, 2023 (for Model ATR42 airplanes); or Section 2.11., ‘‘Cargo Compartment-Loading Limitation,’’ of Sabena Technics Weight & Balance Manual Supplement 0110–11–A–2305–R07, Revision PO 00000 Frm 00021 Fmt 4700 Sfmt 4700 97479 07, dated September 15, 2023 (for Model ATR72 airplanes). (i) No Reporting Requirement Although Sabena Technics Airworthiness Technical Instructions 0110–09–A–ATI–F01– R00, and 0110–11–A–ATI–F01–R00, both dated September 19, 2023, specify 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 manager of the International Validation Branch, mail it to the address identified in paragraph (k) of this AD. Information may be emailed to: 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, International Validation Branch, FAA; or the European Union Aviation Safety Agency (EASA); or Sabena Technic BGC’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOAauthorized 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 shahram.daneshmandi@faa.gov. (l) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the material listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this material as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Sabena Technics Airworthiness Technical Instructions 0110–09–A–ATI–F01– R00, dated September 19, 2023. (ii) Sabena Technics Airworthiness Technical Instructions 0110–11–A–ATI–F01– R00, dated September 19, 2023. (iii) Sabena Technics Weight & Balance Manual Supplement 0110–09–A–2305–R06, Revision 06, dated September 15, 2023. This document has the revision level and date on page 2; no other page of the document has this information. (iv) Sabena Technics Weight & Balance Manual Supplement 0110–11–A–2305–R07, Revision 07, dated September 15, 2023. This document has the revision level and date on page 2; no other page of the document has this information. E:\FR\FM\09DER1.SGM 09DER1 97480 Federal Register / Vol. 89, No. 236 / Monday, December 9, 2024 / Rules and Regulations (3) For Sabena Technics material identified in this AD, contact Sabena Technics BGC, Le Galilée, 9 Bd Henri Ziegler, 31700 Blagnac France; telephone 33 (0)1 56 54 42 30; email airworthiness.office@sabenatechnics.com. (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 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. Issued on November 21, 2024. Victor Wicklund, Deputy Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2024–28789 Filed 12–6–24; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2024–2025; Project Identifier MCAI–2024–00120–T; Amendment 39–22888; AD 2024–23–09] RIN 2120–AA64 Airworthiness Directives; Airbus SAS Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: The FAA is adopting a new airworthiness directive (AD) for all Airbus SAS Model A321–251NX, –252NX, –253NX, –271NX, and –272NX airplanes. This AD was prompted by the discovery during a quality review performed during manufacturing, that a torque strip indicator (material ‘‘Dykem’’) had been applied on the orifice fitting on certain slides’ inflation reservoirs’ venting holes. This AD requires an inspection for discrepancies of affected parts (certain reservoirs having certain orifices) and replacement of discrepant affected parts, and prohibits installing affected parts, 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 January 13, 2025. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of January 13, 2025. ddrumheller on DSK120RN23PROD with RULES1 SUMMARY: VerDate Sep<11>2014 15:13 Dec 06, 2024 Jkt 265001 ADDRESSES: AD Docket: You may examine the AD docket at regulations.gov under Docket No. FAA–2024–2025; 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 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 EASA material identified in this AD, contact EASA, Konrad-AdenauerUfer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; website easa.europa.eu. You may find this 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 at regulations.gov under Docket No. FAA–2024–2025. FOR FURTHER INFORMATION CONTACT: Timothy Dowling, Aviation Safety Engineer, FAA, 1600 Stewart Avenue, Suite 410, Westbury, NY 11590; telephone 206–231–3667; email timothy.p.dowling@faa.gov. SUPPLEMENTARY INFORMATION: Background The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Airbus SAS Model A321– 251NX, –252NX, –253NX, –271NX, and –272NX airplanes. The NPRM published in the Federal Register on August 21, 2024 (89 FR 67575). The NPRM was prompted by AD 2024–0057, dated February 28, 2024, issued by EASA, which is the Technical Agent for the Member States of the European Union (EASA AD 2024–0057) (also referred to as the MCAI). The MCAI states that during a quality review performed during manufacturing, a quality escape was identified on the Model A321NX door 3 slide and offwing slide inflation reservoirs’ venting holes, where a torque strip indicator (material ‘‘Dykem’’) had been applied on the orifice fitting (clogging the vent hole). This condition, in combination with a slide reservoir pressure loss, if not detected and corrected, could lead to PO 00000 Frm 00022 Fmt 4700 Sfmt 4700 deployment in flight of a non-inflated slide, possibly resulting in damage to, and reduced control of, the airplane. In the NPRM, the FAA proposed to require an inspection for discrepancies of affected parts (certain reservoirs having certain orifices) and replacement of discrepant affected parts, and prohibit installing affected parts, as specified in EASA AD 2024–0057. The FAA is issuing 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–2024–2025. Discussion of Final Airworthiness Directive Comments The FAA received comments from the Air Line Pilots Association, International (ALPA), and United Airlines, who supported the NPRM without change. Conclusion 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 referenced above. The FAA reviewed the relevant data, considered the comments received, and determined that air safety requires adopting this AD as proposed. Accordingly, the FAA is issuing this AD to address the unsafe condition on this product. 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. Material Incorporated by Reference Under 1 CFR Part 51 EASA AD 2024–0057 specifies a general visual inspection of affected parts (certain reservoirs having certain orifices) for discrepancies (the presence of ‘‘Dykem’’ material on the orifice fitting) and replacement of discrepant affected parts, and prohibits installing 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. Costs of Compliance The FAA estimates that this AD affects 227 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: E:\FR\FM\09DER1.SGM 09DER1

Agencies

[Federal Register Volume 89, Number 236 (Monday, December 9, 2024)]
[Rules and Regulations]
[Pages 97477-97480]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2024-28789]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2024-2129; Project Identifier MCAI-2024-00066-T; 
Amendment 39-22889; AD 2024-23-10]
RIN 2120-AA64


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

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

-----------------------------------------------------------------------

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain ATR--GIE Avions de Transport R[eacute]gional Model ATR42 and 
ATR72 airplanes. This AD was prompted by a report that for airplanes 
converted from passenger to cargo configuration using certain 
supplemental type certificates, no height limitation for the cargo, 
when loaded in the cargo compartment, is defined, and that as a 
consequence, cargo might be loaded up to the ceiling of the cargo 
compartment. This AD

[[Page 97478]]

requires modification of the cargo compartment and implementation of 
updated cargo loading procedures. The FAA is issuing this AD to address 
the unsafe condition on these products.

DATES: This AD is effective January 13, 2025.
    The Director of the Federal Register approved the incorporation by 
reference of certain publications listed in this AD as of January 13, 
2025.

ADDRESSES: 
    AD Docket: You may examine the AD docket at regulations.gov under 
Docket No. FAA-2024-2129; 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 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 Sabena Technics material identified in this AD, 
contact Sabena Technics BGC, Le Galil[eacute]e, 9 Bd Henri Ziegler, 
31700 Blagnac France; telephone 33 (0)1 56 54 42 30; email 
[email protected].
     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 at regulations.gov under 
Docket No. FAA-2024-2129.

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: 

Background

    The FAA issued a notice of proposed rulemaking (NPRM) to amend 14 
CFR part 39 by adding an AD that would apply to certain ATR--GIE Avions 
de Transport R[eacute]gional Model ATR42 and ATR72 airplanes. The NPRM 
published in the Federal Register on August 22, 2024 (89 FR 67908). The 
NPRM was prompted by AD 2024-0025, dated January 24, 2024, issued by 
the European Union Aviation Safety Agency (EASA), which is the 
Technical Agent for the Member States of the European Union (referred 
to after this as the MCAI). The MCAI states that it was identified that 
for airplanes converted from passenger to cargo configuration using 
EASA Supplemental Type Certificate (STC) 10069551, Revision 1 (EASA STC 
10069551, Revision 0, corresponds to FAA STC ST04602NY), or the 
previous EASA STC 2004-2872 (which corresponds to FAA STC S116-004NM, 
Revision 1), no height limitation for the cargo, when loaded in the 
cargo compartment, is defined. Consequently, operators of such 
airplanes may load the cargo up to the ceiling of the cargo compartment 
and, therefore, potentially affect the proper functioning of the smoke 
detectors. This condition, if not corrected, could lead to smoke not 
being detected in time, possibly resulting in an uncontrolled fire.
    In the NPRM, the FAA proposed to require modification of the cargo 
compartment and implementation of updated cargo loading procedures. The 
FAA is issuing 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-2024-2129.

Discussion of Final Airworthiness Directive

Comments

    The FAA received a comment from Air Line Pilots Association, 
International (ALPA), who supported the NPRM without change.

Conclusion

    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 
referenced above. The FAA reviewed the relevant data, considered the 
comments received, and determined that air safety requires adopting 
this AD as proposed. Accordingly, the FAA is issuing this AD to address 
the unsafe condition on this product. 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.

Material Incorporated by Reference Under 1 CFR Part 51

    The FAA reviewed Sabena Technics Airworthiness Technical 
Instructions 0110-09-A-ATI-F01-R00, and 0110-11-A-ATI-F01-R00, both 
dated September 19, 2023. This material describes procedures for 
modifying the cargo compartment (installing a label and tape to 
indicate maximum cargo height). These documents are distinct since they 
apply to different airplane models.
    The FAA also reviewed Sabena Technics Weight & Balance Manual 
Supplement 0110-09-A-2305-R06, Revision 06, dated September 15, 2023; 
and Sabena Technics Weight & Balance Manual Supplement 0110-11-A-2305-
R07, Revision 07, dated September 15, 2023. The maximum cargo height in 
the cargo compartment is described in Section 2.9., ``Cargo 
Compartment--Loading Limitation,'' of Sabena Technics Weight & Balance 
Manual Supplement 0110-09-A-2305-R06, Revision 06, dated September 15, 
2023; and section 2.11., ``Cargo Compartment-Loading Limitation,'' of 
Sabena Technics Weight & Balance Manual Supplement 0110-11-A-2305-R07, 
Revision 07, dated September 15, 2023. These documents are distinct 
since they apply to different airplane models.
    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 Compliance

    The FAA estimates that this AD affects 2 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                                   Cost on U.S.
                         Labor cost                            Parts cost     Cost per product      operators
----------------------------------------------------------------------------------------------------------------
8 work-hours x $85 per hour = $680..........................         $100                 $780           $1,560
----------------------------------------------------------------------------------------------------------------

    The FAA has included all known costs in its cost estimate. 
According to the manufacturer, however, some or all of the costs of 
this AD may be covered under warranty, thereby reducing the cost impact 
on affected operators.

[[Page 97479]]

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,
    (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.

List of Subjects in 14 CFR Part 39

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

The Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 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:

2024-23-10 ATR--GIE Avions de Transport R[eacute]gional: Amendment 
39-22889; Docket No. FAA-2024-2129; Project Identifier MCAI-2024-
00066-T.

(a) Effective Date

    This airworthiness directive (AD) is effective January 13, 2025.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to ATR--GIE Avions de Transport R[eacute]gional 
airplanes identified in paragraphs (c)(1) and (2) of this AD, 
certificated in any category, modified in accordance with FAA 
Supplemental Type Certificate (STC) ST116-004NM or STC ST04602NY.
    (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 11, Placards and 
Marking.

(e) Unsafe Condition

    This AD was prompted by a report that for airplanes converted 
from passenger to cargo configuration using certain supplemental 
type certificates, no height limitation for the cargo, when loaded 
in the cargo compartment, is defined, and that as a consequence, 
cargo may be loaded up to the ceiling of the cargo compartment. The 
FAA is issuing this AD to address cargo being loaded up to the 
ceiling of the cargo compartment, which could affect the proper 
functioning of the smoke detectors. This condition, if not 
corrected, could lead to smoke not being detected in time, possibly 
resulting in an uncontrolled fire.

(f) Compliance

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

(g) Modification of Cargo Compartment

    Within 6 months after the effective date of this AD, modify the 
cargo compartment in accordance with the Accomplishment Instructions 
of Sabena Technics Airworthiness Technical Instructions 0110-09-A-
ATI-F01-R00, dated September 19, 2023 (for Model ATR42 airplanes); 
or Sabena Technics Airworthiness Technical Instructions 0110-11-A-
ATI-F01-R00, dated September 19, 2023 (for Model ATR72 airplanes).

(h) Revision of Weight and Balance Manual

    Prior to or concurrently with accomplishing the actions required 
by paragraph (g) of this AD, implement the cargo loading procedures 
specified in Section 2.9., ``Cargo Compartment--Loading 
Limitation,'' of Sabena Technics Weight & Balance Manual Supplement 
0110-09-A-2305-R06, Revision 06, dated September 15, 2023 (for Model 
ATR42 airplanes); or Section 2.11., ``Cargo Compartment-Loading 
Limitation,'' of Sabena Technics Weight & Balance Manual Supplement 
0110-11-A-2305-R07, Revision 07, dated September 15, 2023 (for Model 
ATR72 airplanes).

(i) No Reporting Requirement

    Although Sabena Technics Airworthiness Technical Instructions 
0110-09-A-ATI-F01-R00, and 0110-11-A-ATI-F01-R00, both dated 
September 19, 2023, specify 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 manager of the 
International Validation Branch, mail it to the address 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 the European Union Aviation Safety Agency 
(EASA); or Sabena Technic BGC'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 material listed in this 
paragraph under 5 U.S.C. 552(a) and 1 CFR part 51.
    (2) You must use this material as applicable to do the actions 
required by this AD, unless this AD specifies otherwise.
    (i) Sabena Technics Airworthiness Technical Instructions 0110-
09-A-ATI-F01-R00, dated September 19, 2023.
    (ii) Sabena Technics Airworthiness Technical Instructions 0110-
11-A-ATI-F01-R00, dated September 19, 2023.
    (iii) Sabena Technics Weight & Balance Manual Supplement 0110-
09-A-2305-R06, Revision 06, dated September 15, 2023. This document 
has the revision level and date on page 2; no other page of the 
document has this information.
    (iv) Sabena Technics Weight & Balance Manual Supplement 0110-11-
A-2305-R07, Revision 07, dated September 15, 2023. This document has 
the revision level and date on page 2; no other page of the document 
has this information.

[[Page 97480]]

    (3) For Sabena Technics material identified in this AD, contact 
Sabena Technics BGC, Le Galil[eacute]e, 9 Bd Henri Ziegler, 31700 
Blagnac France; telephone 33 (0)1 56 54 42 30; email 
[email protected].
    (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 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 November 21, 2024.
Victor Wicklund,
Deputy Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2024-28789 Filed 12-6-24; 8:45 am]
BILLING CODE 4910-13-P

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