Airworthiness Directives; Airbus SAS Airplanes, 56561-56563 [2022-19808]

Download as PDF 56561 Rules and Regulations Federal Register Vol. 87, No. 178 Thursday, September 15, 2022 This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2022–0391; Project Identifier MCAI–2021–00980–T; Amendment 39–22163; AD 2022–18–12] 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 A330–841 and –941 airplanes. This AD was prompted by a report of erroneous electronic centralized airplane monitoring (ECAM) warnings for low engine oil pressure, which can lead to a commanded shutdown of an engine. This AD requires installing serviceable engine electronic control (EEC) software or EEC units having the serviceable software, limiting certain parts installation configurations, and prior or concurrent modification of EEC software, 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 October 20, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 20, 2022. ADDRESSES: For EASA material incorporated by reference (IBR) in this AD, contact EASA, Konrad-AdenauerUfer 3, 50668 Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu; internet easa.europa.eu. You may find this IBR material on the EASA website at ad.easa.europa.eu. You may view this lotter on DSK11XQN23PROD with RULES1 SUMMARY: VerDate Sep<11>2014 16:37 Sep 14, 2022 Jkt 256001 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 by searching for and locating Docket No. FAA–2022–0391. software, as specified in EASA AD 2021–0198. The FAA is issuing this AD to address erroneous ECAM engine oil pressure warnings, which could lead to dual engine in-flight shutdown and result in reduced control of the airplane. See the MCAI for additional background information. Examining the AD Docket Discussion of Final Airworthiness Directive You may examine the AD docket at regulations.gov by searching for and locating Docket No. FAA–2022–0391; 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. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3229; email vladimir.ulyanov@faa.gov. SUPPLEMENTARY INFORMATION: Background EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2021–0198, dated August 27, 2021 (EASA AD 2021– 0198) (also referred to as the MCAI), to correct an unsafe condition for all Airbus SAS Model A330–841 and –941 airplanes. 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 A330– 841 and –941 airplanes. The NPRM published in the Federal Register on April 5, 2022 (87 FR 19651). The NPRM was prompted by a report of erroneous ECAM warnings for low engine oil pressure, which can lead to a commanded shutdown of an engine. The NPRM proposed to require installing serviceable EEC software or EEC units having the serviceable software, limiting certain parts installation configurations, and prior or concurrent modification of EEC PO 00000 Frm 00001 Fmt 4700 Sfmt 4700 Comments The FAA received comments from three commenters, including Delta Air Lines and two individuals. The following presents the comments received on the NPRM and the FAA’s response to each comment. Request for Incorporation by Reference Paragraph Delta Air Lines (Delta) requested adding paragraph (k), ‘‘Material Incorporated by Reference,’’ to the proposed AD that states the incorporation by reference of EASA AD 2021–0198. Delta supported the improved efficiency of FAA ADs that reference EASA ADs as a primary source of information for accomplishing the requirements of FAA ADs. The FAA agrees to add paragraph (k) to this AD to identify the material that is incorporated by reference. In ADs, whenever there is material to be incorporated by reference, the paragraph that states which material has been approved by the Director of the Federal Register for incorporation by reference is typically added to final rules, not NPRMs. General Statement of Disagreement Two individuals generally disagreed with the proposed AD without any further justification. The FAA infers that these individuals are requesting that the FAA withdraw the proposed AD. The FAA disagrees with withdrawing the proposed AD. The FAA has determined that the issuance of an airworthiness directive is the appropriate method to correct the unsafe condition described in this AD. The FAA has not changed the AD in this regard. Conclusion The FAA reviewed the relevant data, considered the comments received, and determined that air safety requires E:\FR\FM\15SER1.SGM 15SER1 56562 Federal Register / Vol. 87, No. 178 / Thursday, September 15, 2022 / Rules and Regulations adopting this AD as proposed. Except for minor editorial changes, and any other changes described previously, this AD is adopted as proposed in the NPRM. None of the changes will increase the economic burden on any operator. Accordingly, the FAA is issuing this AD to address the unsafe condition on these products. Related Service Information Under 1 CFR Part 51 EASA AD 2021–0198 specifies procedures for installing serviceable EEC software or EEC units having the serviceable software, limiting certain parts installation configurations, and prior or concurrent modification of EEC software. 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 11 airplanes of U.S. registry. The FAA estimates the following costs to comply with this AD: ESTIMATED COSTS FOR REQUIRED ACTIONS Labor cost Parts cost Cost per product Cost on U.S. operators 21 work-hours × $85 per hour = $1,785 ..................................................................................... $0 $1,785 $19,635 The FAA has received no definitive data on which to base the cost estimates for the software update specified in this AD. According to the manufacturer, some or all of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. The FAA does not control warranty coverage for affected individuals. As a result, the FAA has included all known costs in the cost estimate. 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. lotter on DSK11XQN23PROD with RULES1 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. VerDate Sep<11>2014 16:37 Sep 14, 2022 Jkt 256001 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 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: ■ 2022–18–12 Airbus SAS: Amendment 39– 22163; Docket No. FAA–2022–0391; Project Identifier MCAI–2021–00980–T. (a) Effective Date This airworthiness directive (AD) is effective October 20, 2022. (b) Affected ADs None. (c) Applicability This AD applies to all Airbus SAS Model A330–841 and –941 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 73, Engine Fuel & Control. PO 00000 Frm 00002 Fmt 4700 Sfmt 4700 (e) Unsafe Condition This AD was prompted by a report of erroneous electronic centralized airplane monitoring (ECAM) warnings for low engine oil pressure, which can lead to a commanded shutdown of an engine. The FAA is issuing this AD to address erroneous ECAM engine oil pressure warnings, which could lead to dual engine in-flight shutdown and result in reduced 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) AD 2021–0198, dated August 27, 2021 (EASA AD 2021–0198). (h) Exceptions to EASA AD 2021–0198 (1) Where EASA AD 2021–0198 refers to its effective date or ‘‘10 September 2021,’’ this AD requires using the effective date of this AD. (2) Where paragraphs (5) and (6) of EASA AD 2021–0198 refers to ‘‘From 10 September 2021 . . . until 09 September 2023,’’ this AD requires using ‘‘from the effective date of this AD up to 24 months after the effective date of this AD.’’ (3) Where paragraph (7) of EASA AD 2021– 0198 refers to ‘‘10 September 2023,’’ this AD requires using 24 months after the effective date of this AD. (4) This AD does not mandate compliance with the ‘‘Remarks’’ section of EASA AD 2021–0198. (i) Additional AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, Large Aircraft Section, 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 Large Aircraft E:\FR\FM\15SER1.SGM 15SER1 Federal Register / Vol. 87, No. 178 / Thursday, September 15, 2022 / Rules and Regulations Section, International Validation Branch, send it to the attention of the person identified in paragraph (j) of this AD. Information may be emailed to: 9-AVS-AIR730-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, Large Aircraft Section, International Validation Branch, FAA; or EASA; or Airbus SAS’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (3) Required for Compliance (RC): Except as required by paragraph (i)(2) of this AD, if any service information contains procedures or tests that are identified as RC, those procedures and tests must be done to comply with this AD; any procedures or tests that are not identified as RC are recommended. Those procedures and tests that are not identified as RC may be deviated from using accepted methods in accordance with the operator’s maintenance or inspection program without obtaining approval of an AMOC, provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to procedures or tests identified as RC require approval of an AMOC. lotter on DSK11XQN23PROD with RULES1 (j) Related Information For more information about this AD, contact Vladimir Ulyanov, Aerospace Engineer, Large Aircraft Section, FAA, International Validation Branch, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3229; email vladimir.ulyanov@faa.gov. (k) 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 this AD specifies otherwise. (i) European Union Aviation Safety Agency (EASA) AD 2021–0198, dated August 27, 2021. (ii) [Reserved] (3) For EASA AD 2021–0198, 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 this EASA AD on the EASA website at ad.easa.europa.eu. (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 that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, email VerDate Sep<11>2014 16:37 Sep 14, 2022 Jkt 256001 fr.inspection@nara.gov, or go to: archives.gov/federal-register/cfr/ibrlocations.html. Issued on August 23, 2022. Christina Underwood, Acting Director, Compliance & Airworthiness Division, Aircraft Certification Service. [FR Doc. 2022–19808 Filed 9–14–22; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2021–1168; Project Identifier AD–2021–00825–T; Amendment 39–22138; AD 2022–16–09] RIN 2120–AA64 Airworthiness Directives; The Boeing Company Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule. AGENCY: The FAA is adopting a new airworthiness directive (AD) for certain The Boeing Company Model 737–8 airplanes. This AD was prompted by a report that, during production, a small number of fasteners in certain locations of the center fuel tank were cap sealed on top of a black stripe of ink with a clear overcoat. This clear overcoat is not an approved surface for sealing and can potentially compromise sealant adhesion. Compromised sealant adhesion can, over time, affect the lightning-protection properties of the airplane. This AD requires preparation of the affected surface areas to ensure that there is adequate sealant adhesion, and complete encapsulation of the discrepant fastener locations with the approved production sealant. The FAA is issuing this AD to address the unsafe condition on these products. DATES: This AD is effective October 20, 2022. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of October 20, 2022. ADDRESSES: For service information identified in this final rule, contact Boeing Commercial Airplanes, Attention: Contractual & Data Services (C&DS), 2600 Westminster Blvd., MC 110–SK57, Seal Beach, CA 90740–5600; telephone 562–797–1717; internet www.myboeingfleet.com. You may view this service information at the FAA, Airworthiness Products Section, Operational Safety Branch, 2200 South 216th St., Des Moines, WA. For SUMMARY: PO 00000 Frm 00003 Fmt 4700 Sfmt 4700 56563 information on the availability of this material at the FAA, call 206–231–3195. It is also available at www.regulations.gov by searching for and locating Docket No. FAA–2021– 1168. Examining the AD Docket You may examine the AD docket at www.regulations.gov by searching for and locating Docket No. FAA–2021– 1168; 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, 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. FOR FURTHER INFORMATION CONTACT: Chris Baker, Aerospace Engineer, Propulsion Section, FAA, Seattle ACO Branch, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206– 231–3552; email: christopher.r.baker@ 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 The Boeing Company Model 737–8 airplanes. The NPRM published in the Federal Register on February 23, 2022 (87 FR 10110). The NPRM was prompted by a report that, during production, a small number of fasteners common to upper wing panel stringers U–S1, U–S10, U–S12, U–S20, and U–S21 and lower wing panel stringer L–S14 were cap sealed on top of a black stripe of ink with a clear overcoat. The black stripe of ink and clear overcoat were applied during airplane assembly to certain interior areas of the center fuel tank to ensure proper alignment of components, and this discrepancy was not identified by Boeing prior to the delivery of certain airplanes. The purpose of cap sealing is to provide a secondary layer of lightning protection to the metal-to-metal rivet installation bond. The clear overcoat is not an approved surface for sealing and can potentially compromise sealant adhesion. Compromised sealant adhesion can, over time, affect the lightning protection properties of the airplane. In the NPRM, the FAA proposed to require preparation of the affected surface areas to ensure that there is adequate sealant adhesion, and complete encapsulation of the discrepant fastener locations with E:\FR\FM\15SER1.SGM 15SER1

Agencies

[Federal Register Volume 87, Number 178 (Thursday, September 15, 2022)]
[Rules and Regulations]
[Pages 56561-56563]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-19808]



========================================================================
Rules and Regulations
                                                Federal Register
________________________________________________________________________

This section of the FEDERAL REGISTER contains regulatory documents 
having general applicability and legal effect, most of which are keyed 
to and codified in the Code of Federal Regulations, which is published 
under 50 titles pursuant to 44 U.S.C. 1510.

The Code of Federal Regulations is sold by the Superintendent of Documents. 

========================================================================


Federal Register / Vol. 87, No. 178 / Thursday, September 15, 2022 / 
Rules and Regulations

[[Page 56561]]



DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0391; Project Identifier MCAI-2021-00980-T; 
Amendment 39-22163; AD 2022-18-12]
RIN 2120-AA64


Airworthiness Directives; Airbus SAS Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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

SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all 
Airbus SAS Model A330-841 and -941 airplanes. This AD was prompted by a 
report of erroneous electronic centralized airplane monitoring (ECAM) 
warnings for low engine oil pressure, which can lead to a commanded 
shutdown of an engine. This AD requires installing serviceable engine 
electronic control (EEC) software or EEC units having the serviceable 
software, limiting certain parts installation configurations, and prior 
or concurrent modification of EEC software, 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 October 20, 2022.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of October 20, 
2022.

ADDRESSES: For EASA material incorporated by reference (IBR) in this 
AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; 
telephone +49 221 8999 000; email [email protected]; internet 
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 by searching for and locating Docket No. FAA-2022-0391.

Examining the AD Docket

    You may examine the AD docket at regulations.gov by searching for 
and locating Docket No. FAA-2022-0391; 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.

FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, 
Large Aircraft Section, FAA, International Validation Branch, 2200 
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229; 
email [email protected].

SUPPLEMENTARY INFORMATION: 

Background

    EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2021-0198, dated August 27, 2021 
(EASA AD 2021-0198) (also referred to as the MCAI), to correct an 
unsafe condition for all Airbus SAS Model A330-841 and -941 airplanes.
    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 
A330-841 and -941 airplanes. The NPRM published in the Federal Register 
on April 5, 2022 (87 FR 19651). The NPRM was prompted by a report of 
erroneous ECAM warnings for low engine oil pressure, which can lead to 
a commanded shutdown of an engine. The NPRM proposed to require 
installing serviceable EEC software or EEC units having the serviceable 
software, limiting certain parts installation configurations, and prior 
or concurrent modification of EEC software, as specified in EASA AD 
2021-0198.
    The FAA is issuing this AD to address erroneous ECAM engine oil 
pressure warnings, which could lead to dual engine in-flight shutdown 
and result in reduced control of the airplane. See the MCAI for 
additional background information.

Discussion of Final Airworthiness Directive

Comments

    The FAA received comments from three commenters, including Delta 
Air Lines and two individuals. The following presents the comments 
received on the NPRM and the FAA's response to each comment.

Request for Incorporation by Reference Paragraph

    Delta Air Lines (Delta) requested adding paragraph (k), ``Material 
Incorporated by Reference,'' to the proposed AD that states the 
incorporation by reference of EASA AD 2021-0198. Delta supported the 
improved efficiency of FAA ADs that reference EASA ADs as a primary 
source of information for accomplishing the requirements of FAA ADs.
    The FAA agrees to add paragraph (k) to this AD to identify the 
material that is incorporated by reference. In ADs, whenever there is 
material to be incorporated by reference, the paragraph that states 
which material has been approved by the Director of the Federal 
Register for incorporation by reference is typically added to final 
rules, not NPRMs.

General Statement of Disagreement

    Two individuals generally disagreed with the proposed AD without 
any further justification.
    The FAA infers that these individuals are requesting that the FAA 
withdraw the proposed AD. The FAA disagrees with withdrawing the 
proposed AD. The FAA has determined that the issuance of an 
airworthiness directive is the appropriate method to correct the unsafe 
condition described in this AD. The FAA has not changed the AD in this 
regard.

Conclusion

    The FAA reviewed the relevant data, considered the comments 
received, and determined that air safety requires

[[Page 56562]]

adopting this AD as proposed. Except for minor editorial changes, and 
any other changes described previously, this AD is adopted as proposed 
in the NPRM. None of the changes will increase the economic burden on 
any operator. Accordingly, the FAA is issuing this AD to address the 
unsafe condition on these products.

Related Service Information Under 1 CFR Part 51

    EASA AD 2021-0198 specifies procedures for installing serviceable 
EEC software or EEC units having the serviceable software, limiting 
certain parts installation configurations, and prior or concurrent 
modification of EEC software. 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 11 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
21 work-hours x $85 per hour = $1,785........................              $0           $1,785          $19,635
----------------------------------------------------------------------------------------------------------------

    The FAA has received no definitive data on which to base the cost 
estimates for the software update specified in this AD.
    According to the manufacturer, some or all of the costs of this AD 
may be covered under warranty, thereby reducing the cost impact on 
affected individuals. The FAA does not control warranty coverage for 
affected individuals. As a result, the FAA has included all known costs 
in the cost estimate.

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:

2022-18-12 Airbus SAS: Amendment 39-22163; Docket No. FAA-2022-0391; 
Project Identifier MCAI-2021-00980-T.

(a) Effective Date

    This airworthiness directive (AD) is effective October 20, 2022.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Airbus SAS Model A330-841 and -941 
airplanes, certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 73, Engine Fuel 
& Control.

(e) Unsafe Condition

    This AD was prompted by a report of erroneous electronic 
centralized airplane monitoring (ECAM) warnings for low engine oil 
pressure, which can lead to a commanded shutdown of an engine. The 
FAA is issuing this AD to address erroneous ECAM engine oil pressure 
warnings, which could lead to dual engine in-flight shutdown and 
result in reduced 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) AD 
2021-0198, dated August 27, 2021 (EASA AD 2021-0198).

(h) Exceptions to EASA AD 2021-0198

    (1) Where EASA AD 2021-0198 refers to its effective date or ``10 
September 2021,'' this AD requires using the effective date of this 
AD.
    (2) Where paragraphs (5) and (6) of EASA AD 2021-0198 refers to 
``From 10 September 2021 . . . until 09 September 2023,'' this AD 
requires using ``from the effective date of this AD up to 24 months 
after the effective date of this AD.''
    (3) Where paragraph (7) of EASA AD 2021-0198 refers to ``10 
September 2023,'' this AD requires using 24 months after the 
effective date of this AD.
    (4) This AD does not mandate compliance with the ``Remarks'' 
section of EASA AD 2021-0198.

(i) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Large Aircraft Section, 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 Large Aircraft

[[Page 56563]]

Section, International Validation Branch, send it to the attention 
of the person 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, Large Aircraft 
Section, International Validation Branch, FAA; or EASA; or Airbus 
SAS's EASA Design Organization Approval (DOA). If approved by the 
DOA, the approval must include the DOA-authorized signature.
    (3) Required for Compliance (RC): Except as required by 
paragraph (i)(2) of this AD, if any service information contains 
procedures or tests that are identified as RC, those procedures and 
tests must be done to comply with this AD; any procedures or tests 
that are not identified as RC are recommended. Those procedures and 
tests that are not identified as RC may be deviated from using 
accepted methods in accordance with the operator's maintenance or 
inspection program without obtaining approval of an AMOC, provided 
the procedures and tests identified as RC can be done and the 
airplane can be put back in an airworthy condition. Any 
substitutions or changes to procedures or tests identified as RC 
require approval of an AMOC.

(j) Related Information

    For more information about this AD, contact Vladimir Ulyanov, 
Aerospace Engineer, Large Aircraft Section, FAA, International 
Validation Branch, 2200 South 216th St., Des Moines, WA 98198; 
telephone and fax 206-231-3229; email [email protected].

(k) 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 this AD specifies otherwise.
    (i) European Union Aviation Safety Agency (EASA) AD 2021-0198, 
dated August 27, 2021.
    (ii) [Reserved]
    (3) For EASA AD 2021-0198, contact EASA, Konrad-Adenauer-Ufer 3, 
50668 Cologne, Germany; telephone +49 221 8999 000; email 
[email protected]; internet easa.europa.eu. You may find this EASA 
AD on the EASA website at ad.easa.europa.eu.
    (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 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: archives.gov/federal-register/cfr/ibr-locations.html.

    Issued on August 23, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2022-19808 Filed 9-14-22; 8:45 am]
BILLING CODE 4910-13-P
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