Airworthiness Directives; Airbus SAS Airplanes, 60001-60003 [2019-24269]

Download as PDF Federal Register / Vol. 84, No. 216 / Thursday, November 7, 2019 / Proposed Rules The requirements in Chapter 2, Sections V.A.4 through V.G also apply to a credit union that serves a rural district. 3. Amend Chapter 2 of Appendix B to part 701 by adding Section V.A.8 to read as follows: ■ V.A.8 Community Selection Requirements and Review The NCUA will not approve an application for a community charter consisting of all or a portion of a CSA or a CBSA, including an initial application, amendment, or expansion, unless the applicant demonstrates in its business and marketing plan that (1) the credit union will serve a community that is contiguous and (2) the credit union will provide financial services to low- and moderate-income and underserved people, and that the credit union has not selected its service area in order to exclude low- and moderate-income and underserved people. Upon receipt of this material, the NCUA will evaluate the business and marketing plan to ensure that low- and moderate-income and underserved people will be served and that the credit union has not selected the service area in order to exclude such people. This requirement is in addition to the requirement to document in the business and marketing plan the realistic assumptions that support the credit union’s viability and its plan to serve its entire FOM. The NCUA may conduct such further inquiry or evaluation as it deems appropriate, as authorized by 12 U.S.C. 1754 and consistent with the principles of this Manual, other federal laws, and public policy. If the NCUA determines that the credit union’s submission is inaccurate or unsupported, it may deny that application on those grounds, regardless of whether the application satisfies the other criteria for initial chartering, amendment, or expansion. 4. Section V.B of Chapter 2 of Appendix B to part 701 is revised to read as follows: ■ 17:23 Nov 06, 2019 Jkt 250001 [FR Doc. 2019–23680 Filed 11–6–19; 8:45 am] BILLING CODE 7535–01–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2019–0863; Product Identifier 2019–NM–157–AD] be incorporated by reference. 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 December 23, 2019. 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 https://www.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. For the material identified in this proposed AD that will be incorporated by reference (IBR), contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 89990 1000; email ADs@easa.europa.eu; internet www.easa.europa.eu. You may find this IBR material on the EASA website at https://ad.easa.europa.eu. You may view this IBR material at the FAA, Transport Standards 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 on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2019– 0863. RIN 2120–AA64 V.B Field of Membership Amendments A community credit union may amend its field of membership by adding additional affinities or removing exclusionary clauses. This can be accomplished with a housekeeping amendment. A community credit union also may expand its geographic boundaries. Persons who live, work, worship, or attend school within the proposed well-defined local community, neighborhood or rural district must have common interests and/or interact. The credit union must follow the requirements of Section V.A.4 and Section V.A.8 of this chapter. A community credit union that is based on a Single Political Jurisdiction, a Statistical Area (e.g., Core Based Statistical Area or Combined Statistical Area) or a rural district may expand its geographic boundaries to add a bordering area, provided the area is well defined and the credit union demonstrates that persons who live, work, worship, or attend school within the proposed expanded community (i.e., on both sides of the boundary separating the existing community and the bordering area) have common VerDate Sep<11>2014 interests and/or interact. Such a credit union applying to expand its geographic boundaries to add a bordering area must follow a streamlined version of the business plan requirements of Section V.A.4 of this chapter and the expanded community would be subject to the corresponding population limit—2.5 million in the case of a Single Political Jurisdiction, or a Statistical Area and 1 million in the case of a rural district. The streamlined business plan requirements for adding a bordering area are: • Anticipated marginal financial impact on the credit union of adding the proposed bordering area, including the need for additional employees and fixed assets, and the associated costs; • A description of the current and, if applicable, proposed office/branch structure specific to serving the proposed bordering area; • A marketing plan addressing how the new community will be served for the 24month period after the proposed expansion of a community charter, including detailing how the credit union will address the unique needs of any demographic groups in the proposed bordering community not presently served by the credit union and how the credit union will market to any new groups; and • Details, terms and conditions of any new financial products, programs, and services to be introduced as part of this expansion. 60001 Examining the AD Docket You may examine the AD docket on Airworthiness Directives; Airbus SAS the internet at https:// Airplanes www.regulations.gov by searching for and locating Docket No. FAA–2019– AGENCY: Federal Aviation 0863; or in person at Docket Operations Administration (FAA), DOT. between 9 a.m. and 5 p.m., Monday ACTION: Notice of proposed rulemaking through Friday, except Federal holidays. (NPRM). The AD docket contains this NPRM, the SUMMARY: The FAA proposes to adopt a regulatory evaluation, any comments new airworthiness directive (AD) for received, and other information. The street address for Docket Operations is certain Airbus SAS Model A318–112, A319–111, A319–112, A319–113, A319– listed above. Comments will be available in the AD docket shortly after 114, A319–115, A319–131, A319–132, A319–133, A320–211, A320–212, A320– receipt. 214, A320–216, A320–231, A320–232, FOR FURTHER INFORMATION CONTACT: A320–233, A320–251N, and A320–271N Sanjay Ralhan, Aerospace Engineer, airplanes. This proposed AD was International Section, Transport prompted by a report of marginal Standards Branch, FAA, 2200 South clearance between certain fuel sensor 216th St., Des Moines, WA 98198; covers on both left-hand (LH) and right- telephone and fax 206–231–3223. hand (RH) wings. This proposed AD SUPPLEMENTARY INFORMATION: would require the replacement of Comments Invited certain fuel level sensor brackets, as specified in a European Union Aviation The FAA invites you to send any Safety Agency (EASA) AD, which will written relevant data, views, or PO 00000 Frm 00032 Fmt 4702 Sfmt 4702 E:\FR\FM\07NOP1.SGM 07NOP1 60002 Federal Register / Vol. 84, No. 216 / Thursday, November 7, 2019 / Proposed Rules possible motion between the stringer and the shield, can make the gap more susceptible to sparking in case of lightning strike. The FAA is proposing this AD to address this condition, which could create a source of ignition in a fuel tank vapor space, possibly resulting in a fire or explosion and consequent loss of the airplane. See the MCAI for additional background information. arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2019–0863; Product Identifier 2019–NM–157–AD’’ at the beginning of your comments. The FAA specifically invites comments on the overall regulatory, economic, environmental, and energy aspects of this NPRM. The FAA will consider all comments received by the closing date and may amend this NPRM based on those comments. The FAA will post all comments received, without change, to https:// www.regulations.gov, including any personal information you provide. The FAA will also post a report summarizing each substantive verbal contact received about this NPRM. Related IBR Material Under 1 CFR Part 51 EASA AD 2019–0197 describes procedures for the replacement of certain fuel level sensor brackets. 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. Discussion The EASA, which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2019–0197, dated August 14, 2019 (‘‘EASA AD 2019–0197’’) (also referred to as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for certain Airbus SAS Model A318– 112, A319–111, A319–112, A319–113, A319–114, A319–115, A319–131, A319– 132, A319–133, A320–211, A320–212, A320–214, A320–215, A320–216, A320– 231, A320–232, A320–233, A320–251N, and A320–271N airplanes. Model A320–215 airplanes are not on the U.S. Register; this AD therefore does not include those airplanes in the applicability. This proposed AD was prompted by a report of marginal clearance between certain fuel sensor covers on rib 24 and the crown of stringer 15 on both LH and RH wings. A possible contact between the shield and the stringer, and/or FAA’s Determination and Requirements of This Proposed AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to a bilateral agreement with the State of Design Authority, the FAA has been notified of the unsafe condition described in the MCAI referenced above. The FAA is proposing this AD because the agency evaluated all the relevant information and determined the unsafe condition described previously is likely to exist or develop in other products of the same type design. Proposed AD Requirements This proposed AD would require accomplishing the actions specified in EASA AD 2019–0197 described previously, as incorporated by reference, except for any differences identified as exceptions in the regulatory text of this AD. Explanation of Required Compliance Information In the FAA’s ongoing efforts to improve the efficiency of the AD process, the FAA initially worked with Airbus and EASA to develop a process to use certain EASA ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. The FAA has since coordinated with other manufacturers and civil aviation authorities (CAAs) to use this process. As a result, EASA AD 2019–0197 will be incorporated by reference in the FAA final rule. This proposed AD would, therefore, require compliance with EASA AD 2019–0197 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 the EASA AD 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 the EASA AD. Service information specified in EASA AD 2019–0197 that is required for compliance with EASA AD 2019–0197 will be available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2019–0863 after the FAA final rule is published. Costs of Compliance The FAA estimates that this proposed AD affects 776 airplanes of U.S. registry. The FAA estimates the following costs to comply with this proposed AD: ESTIMATED COSTS FOR REQUIRED ACTIONS Labor cost Parts cost Cost per product Up to 7 work-hour × $85 per hour = Up to $595 ............................................... Up to $609 ............. Up to $1,204 .......... 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 VerDate Sep<11>2014 17:23 Nov 06, 2019 Jkt 250001 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. PO 00000 Frm 00033 Fmt 4702 Sfmt 4702 Cost on U.S. operators Up to $934,304. This proposed AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes and associated E:\FR\FM\07NOP1.SGM 07NOP1 Federal Register / Vol. 84, No. 216 / Thursday, November 7, 2019 / Proposed Rules appliances to the Director of the System Oversight Division. 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) 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 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 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 (AD): ■ Airbus SAS: Docket No. FAA–2019–0863; Product Identifier 2019–NM–157–AD. (a) Comments Due Date The FAA must receive comments by December 23, 2019. (b) Affected ADs None. (c) Applicability This AD applies to Airbus SAS Model A318–112, A319–111, A319–112, A319–113, A319–114, A319–115, A319–131, A319–132, A319–133, A320–211, A320–212, A320–214, A320–216, A320–231, A320–232, A320–233, A320–251N, and A320–271N airplanes, certificated in any category, as identified in European Union Aviation Safety Agency (EASA) AD 2019–0197, dated August 14, 2019 (‘‘EASA AD 2019–0197’’). (d) Subject Air Transport Association (ATA) of America Code 28, Fuel. VerDate Sep<11>2014 17:23 Nov 06, 2019 Jkt 250001 (e) Reason This AD was prompted by a report of marginal clearance between certain fuel sensor covers on rib 24 and the crown of stringer 15 on both left-hand (LH) and righthand (RH) wings. A possible contact between the shield and the stringer, and/or possible motion between the stringer and the shield, can make the gap more susceptible to sparking in case of lightning strike. The FAA is issuing this AD to address this condition, which could create a source of ignition in a fuel tank vapor space, possibly resulting in a fire or explosion and consequent loss 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, EASA AD 2019–0197. (h) Exceptions to EASA AD 2019–0197 (1) Where EASA AD 2019–0197 refers to its effective date, this AD requires using the effective date of this AD. (2) The ‘‘Remarks’’ section of EASA AD 2019–0197 does not apply to this AD. (i) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Section, Transport Standards 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 local Flight Standards District Office, as appropriate. If sending information directly to the International Section, send it to the attention of the person identified in paragraph (j)(2) of this AD. Information may be emailed to: 9-ANM-116-AMOCREQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district 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 Section, Transport Standards Branch, FAA; or EASA; or Airbus SAS’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOAauthorized signature. (3) Required for Compliance (RC): For any service information referenced in EASA AD 2019–0197 that contains RC procedures and tests: Except as required by paragraph (i)(2) of this AD, RC 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 PO 00000 Frm 00034 Fmt 4702 Sfmt 4702 60003 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 (1) For information about EASA AD 2019– 0197, contact the EASA, Konrad-AdenauerUfer 3, 50668 Cologne, Germany; telephone +49 221 89990 6017; email ADs@ easa.europa.eu; internet www.easa.europa.eu. You may find this EASA AD on the EASA website at https:// ad.easa.europa.eu. You may view this material at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. This material may be found in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2019–0863. (2) For more information about this AD, contact Sanjay Ralhan, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206– 231–3223. Issued in Des Moines, Washington, on November 1, 2019. Dionne Palermo, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2019–24269 Filed 11–6–19; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2019–0016; Product Identifier 2018–NM–168–AD] RIN 2120–AA64 Airworthiness Directives; Airbus SAS Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Supplemental notice of proposed rulemaking (SNPRM); reopening of comment period. AGENCY: The FAA is revising an earlier proposal for all Airbus SAS Model A350–941 and –1041 airplanes. This action revises the notice of proposed rulemaking (NPRM) by including additional part numbers that are affected by the unsafe condition. The FAA is proposing this airworthiness directive (AD) to address the unsafe condition on these products. Since these actions would impose an additional burden over those in the NPRM, the SUMMARY: E:\FR\FM\07NOP1.SGM 07NOP1

Agencies

[Federal Register Volume 84, Number 216 (Thursday, November 7, 2019)]
[Proposed Rules]
[Pages 60001-60003]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2019-24269]


=======================================================================
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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0863; Product Identifier 2019-NM-157-AD]
RIN 2120-AA64


Airworthiness Directives; Airbus SAS Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Airbus SAS Model A318-112, A319-111, A319-112, A319-113, 
A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, A320-212, 
A320-214, A320-216, A320-231, A320-232, A320-233, A320-251N, and A320-
271N airplanes. This proposed AD was prompted by a report of marginal 
clearance between certain fuel sensor covers on both left-hand (LH) and 
right-hand (RH) wings. This proposed AD would require the replacement 
of certain fuel level sensor brackets, as specified in a European Union 
Aviation Safety Agency (EASA) AD, which will be incorporated by 
reference. 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 December 
23, 2019.

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 https://www.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.
    For the material identified in this proposed AD that will be 
incorporated by reference (IBR), contact the EASA, Konrad-Adenauer-Ufer 
3, 50668 Cologne, Germany; telephone +49 221 89990 1000; email 
[email protected]; internet www.easa.europa.eu. You may find this IBR 
material on the EASA website at https://ad.easa.europa.eu. You may view 
this IBR material at the FAA, Transport Standards 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 on the internet at https://www.regulations.gov by searching for 
and locating Docket No. FAA-2019-0863.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
0863; 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 regulatory evaluation, any comments received, and other 
information. The street address for Docket Operations is listed above. 
Comments will be available in the AD docket shortly after receipt.

FOR FURTHER INFORMATION CONTACT: Sanjay Ralhan, Aerospace Engineer, 
International Section, Transport Standards Branch, FAA, 2200 South 
216th St., Des Moines, WA 98198; telephone and fax 206-231-3223.

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or

[[Page 60002]]

arguments about this proposal. Send your comments to an address listed 
under the ADDRESSES section. Include ``Docket No. FAA-2019-0863; 
Product Identifier 2019-NM-157-AD'' at the beginning of your comments. 
The FAA specifically invites comments on the overall regulatory, 
economic, environmental, and energy aspects of this NPRM. The FAA will 
consider all comments received by the closing date and may amend this 
NPRM based on those comments.
    The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide. 
The FAA will also post a report summarizing each substantive verbal 
contact received about this NPRM.

Discussion

    The EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2019-0197, dated August 14, 2019 
(``EASA AD 2019-0197'') (also referred to as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for certain Airbus SAS Model A318-112, A319-111, A319-112, 
A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, A320-211, 
A320-212, A320-214, A320-215, A320-216, A320-231, A320-232, A320-233, 
A320-251N, and A320-271N airplanes. Model A320-215 airplanes are not on 
the U.S. Register; this AD therefore does not include those airplanes 
in the applicability.
    This proposed AD was prompted by a report of marginal clearance 
between certain fuel sensor covers on rib 24 and the crown of stringer 
15 on both LH and RH wings. A possible contact between the shield and 
the stringer, and/or possible motion between the stringer and the 
shield, can make the gap more susceptible to sparking in case of 
lightning strike. The FAA is proposing this AD to address this 
condition, which could create a source of ignition in a fuel tank vapor 
space, possibly resulting in a fire or explosion and consequent loss of 
the airplane. See the MCAI for additional background information.

Related IBR Material Under 1 CFR Part 51

    EASA AD 2019-0197 describes procedures for the replacement of 
certain fuel level sensor brackets. 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.

FAA's Determination and Requirements of This Proposed AD

    This product has been approved by the aviation authority of another 
country, and is approved for operation in the United States. Pursuant 
to a bilateral agreement with the State of Design Authority, the FAA 
has been notified of the unsafe condition described in the MCAI 
referenced above. The FAA is proposing this AD because the agency 
evaluated all the relevant information and determined the unsafe 
condition described previously is likely to exist or develop in other 
products of the same type design.

Proposed AD Requirements

    This proposed AD would require accomplishing the actions specified 
in EASA AD 2019-0197 described previously, as incorporated by 
reference, except for any differences identified as exceptions in the 
regulatory text of this AD.

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD 
process, the FAA initially worked with Airbus and EASA to develop a 
process to use certain EASA ADs as the primary source of information 
for compliance with requirements for corresponding FAA ADs. The FAA has 
since coordinated with other manufacturers and civil aviation 
authorities (CAAs) to use this process. As a result, EASA AD 2019-0197 
will be incorporated by reference in the FAA final rule. This proposed 
AD would, therefore, require compliance with EASA AD 2019-0197 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 the EASA AD 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 the EASA AD. Service information specified 
in EASA AD 2019-0197 that is required for compliance with EASA AD 2019-
0197 will be available on the internet at https://www.regulations.gov 
by searching for and locating Docket No. FAA-2019-0863 after the FAA 
final rule is published.

Costs of Compliance

    The FAA estimates that this proposed AD affects 776 airplanes of 
U.S. registry. The FAA estimates the following costs to comply with 
this proposed AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
          Labor cost                    Parts cost               Cost per product        Cost on U.S. operators
----------------------------------------------------------------------------------------------------------------
Up to 7 work-hour x $85 per     Up to $609................  Up to $1,204.............  Up to $934,304.
 hour = Up to $595.
----------------------------------------------------------------------------------------------------------------

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.
    This proposed AD is issued in accordance with authority delegated 
by the Executive Director, Aircraft Certification Service, as 
authorized by FAA Order 8000.51C. In accordance with that order, 
issuance of ADs is normally a function of the Compliance and 
Airworthiness Division, but during this transition period, the 
Executive Director has delegated the authority to issue ADs applicable 
to transport category airplanes and associated

[[Page 60003]]

appliances to the Director of the System Oversight Division.

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) 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 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 (AD):

Airbus SAS: Docket No. FAA-2019-0863; Product Identifier 2019-NM-
157-AD.

(a) Comments Due Date

    The FAA must receive comments by December 23, 2019.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Airbus SAS Model A318-112, A319-111, A319-
112, A319-113, A319-114, A319-115, A319-131, A319-132, A319-133, 
A320-211, A320-212, A320-214, A320-216, A320-231, A320-232, A320-
233, A320-251N, and A320-271N airplanes, certificated in any 
category, as identified in European Union Aviation Safety Agency 
(EASA) AD 2019-0197, dated August 14, 2019 (``EASA AD 2019-0197'').

(d) Subject

    Air Transport Association (ATA) of America Code 28, Fuel.

(e) Reason

    This AD was prompted by a report of marginal clearance between 
certain fuel sensor covers on rib 24 and the crown of stringer 15 on 
both left-hand (LH) and right-hand (RH) wings. A possible contact 
between the shield and the stringer, and/or possible motion between 
the stringer and the shield, can make the gap more susceptible to 
sparking in case of lightning strike. The FAA is issuing this AD to 
address this condition, which could create a source of ignition in a 
fuel tank vapor space, possibly resulting in a fire or explosion and 
consequent loss 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, EASA AD 2019-0197.

(h) Exceptions to EASA AD 2019-0197

    (1) Where EASA AD 2019-0197 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) The ``Remarks'' section of EASA AD 2019-0197 does not apply 
to this AD.

(i) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Section, Transport Standards 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 local Flight 
Standards District Office, as appropriate. If sending information 
directly to the International Section, send it to the attention of 
the person identified in paragraph (j)(2) 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 local flight 
standards district office/certificate holding district 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 
Section, Transport Standards 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): For any service information 
referenced in EASA AD 2019-0197 that contains RC procedures and 
tests: Except as required by paragraph (i)(2) of this AD, RC 
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

    (1) For information about EASA AD 2019-0197, contact the EASA, 
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; telephone +49 221 
89990 6017; email [email protected]; internet www.easa.europa.eu. 
You may find this EASA AD on the EASA website at https://ad.easa.europa.eu. You may view this material at the FAA, Transport 
Standards Branch, 2200 South 216th St., Des Moines, WA. For 
information on the availability of this material at the FAA, call 
206-231-3195. This material may be found in the AD docket on the 
internet at https://www.regulations.gov by searching for and 
locating Docket No. FAA-2019-0863.
    (2) For more information about this AD, contact Sanjay Ralhan, 
Aerospace Engineer, International Section, Transport Standards 
Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone 
and fax 206-231-3223.

    Issued in Des Moines, Washington, on November 1, 2019.
Dionne Palermo,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2019-24269 Filed 11-6-19; 8:45 am]
 BILLING CODE 4910-13-P
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