83 FR 63598 - Airworthiness Directives; Airbus SAS Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 237 (December 11, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 237 (December 11, 2018)
| Page Range | 63598-63601 | |
| FR Document | 2018-26624 |
[Federal Register Volume 83, Number 237 (Tuesday, December 11, 2018)] [Proposed Rules] [Pages 63598-63601] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-26624] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-1007; Product Identifier 2018-NM-141-AD] RIN 2120-AA64 Airworthiness Directives; Airbus SAS Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). ----------------------------------------------------------------------- SUMMARY: We propose to adopt a new airworthiness directive (AD) for certain Airbus SAS Model A318 and A319 series airplanes, Model A320- 211, -212, -214, -216, -231, -232, and -233 airplanes, and Model A321- 111, -112, -131, -211, -212, -213, -231, and -232 airplanes. This proposed AD was prompted by a report that taperloks used in a certain wing-to-fuselage junction were found to be non-compliant with the applicable specification, resulting in a loss of pre-tension in the fasteners. This proposed AD would require repetitive special detailed inspections of the center and outer wing box lower stiffeners and panels at a certain junction on the left- and right-hand sides for any cracking, and repair if necessary. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by January 25, 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 http://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 incorporation by reference (IBR) material described in the ``Related IBR material under 1 CFR part 51'' section in SUPPLEMENTARY INFORMATION, contact 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 http://www.regulations.gov. Examining the AD Docket You may examine the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 1007; or in person at the Docket Management Facility 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 the Docket Operations office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Sanjay Ralhan, Aerospace Engineer, [[Page 63599]] International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3223. SUPPLEMENTARY INFORMATION: Comments Invited We invite you to send any written relevant data, views, or arguments about this proposal. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2018-1007; Product Identifier 2018-NM-141-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this NPRM. We will consider all comments received by the closing date and may amend this NPRM based on those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this NPRM. Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2018-0218, dated October 11, 2018; corrected October 26, 2018 (``EASA AD 2018-0218'') (also referred to as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Airbus SAS Model A318 and A319 series airplanes, Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes, and Model A321-111, -112, -131, -211, -212, -213, -231, and -232 airplanes. The MCAI states: Taperloks used in the wing-to-fuselage junction at Rib 1 were found to be non-compliant with the applicable specification, resulting in a loss of pre-tension in the fasteners. This condition, if not detected and corrected, could affect the structural integrity of the aeroplane. To address this potential unsafe condition, Airbus issued SB A320-57-1129 and SB A320-57-1130, later revised twice, providing instructions for repetitive internal inspections of the lower stiffeners and for repetitive external inspections of the lower panels of the center and outer wing box at the level of Rib 1 junction. Consequently, EASA issued AD 2007-0067, later revised [which corresponds to FAA AD 2008-02-15, Amendment 39- 15345 (73 FR 4063, January 24, 2008) (``AD 2008-02-15'')], to require accomplishment of these inspections. Since EASA AD 2007-0067R1 was issued, new events and the results of studies identified an aging effect on these parts. Prompted by these findings, Airbus revised SB A320-57-1129 (now at Revision 05) and A320-57-1130 (now at Revision 04), expanding the applicability, modifying the area to be inspected and updating the inspection intervals. For the reasons stated above, this [EASA] AD retains the requirements of EASA AD 2007-0067R1, which is superseded, expands the Applicability, modifies the areas to be inspected and revises the inspection thresholds and intervals. This [EASA] AD is republished to correct typographical errors in paragraph (2) and in Tables 1 and 3. Relationship Between Proposed AD and AD 2008-02-15 This NPRM would not supersede AD 2008-02-15. Rather, we have determined that a stand-alone AD would be more appropriate to address the changes in the MCAI. This NPRM would require repetitive special detailed inspections of the center and outer wing box lower stiffeners and panels at the level of rib 1 junction on the left- and right-hand sides for any cracking, and repair if necessary. Accomplishment of the proposed actions would then terminate all of the requirements of AD 2008-02-15. Related IBR Material Under 1 CFR Part 51 EASA AD 2018-0218 describes procedures for repetitive special detailed inspections of the center and outer wing box lower stiffeners and panels at the level of rib 1 junction on the left- and right-hand sides for any cracking, and repair if necessary. EASA AD 2018-0218 also provides procedures for an optional modification, which would terminate the repetitive inspections. 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 and it is publicly available through the EASA website. 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 our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI referenced above. We are proposing this AD because we evaluated all pertinent information and determined an unsafe condition exists and is likely to exist or develop on other products of the same type design. Explanation of Required Compliance Information In the FAA's ongoing efforts to improve the efficiency of the AD process, the FAA worked with Airbus and the EASA to develop a process to use certain EASA ADs as the primary source of information for compliance with requirements for corresponding FAA ADs. As a result, EASA AD 2018-0218 will be incorporated by reference in the FAA final rule. This proposed AD would, therefore, require compliance with the provisions specified in EASA AD 2018-0218, except for any differences identified as exceptions in the regulatory text of this proposed AD. Service information specified in EASA AD 2018-0218 that is required for compliance with EASA AD 2018-0218 will be available at http://www.regulations.gov under Docket No. FAA-2018-1007 after the FAA final rule is published. Explanation of ``RC'' (Required for Compliance) EASA AD 2018-0218, dated October 11, 2018; corrected October 26, 2018; might refer to service information that contains procedures or tests that are identified as RC. 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 alternative method of compliance (AMOC), provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Costs of Compliance We estimate that this proposed AD affects 516 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: Estimated Costs for Required Actions ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- 51 work-hours x $85 per hour = $4,335........................ $0 $4,335 $2,236,860 ---------------------------------------------------------------------------------------------------------------- [[Page 63600]] We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this proposed AD. Estimated Costs for Optional Actions ---------------------------------------------------------------------------------------------------------------- Cost per Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- 244 work-hours x $85 per hour = $20,740....................................... $5,120 $25,860 ---------------------------------------------------------------------------------------------------------------- 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. We are 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 to the Director of the System Oversight Division. Regulatory Findings We 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. Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); 3. Will not affect intrastate aviation in Alaska; and 4. 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-2018-1007; Product Identifier 2018-NM- 141-AD. (a) Comments Due Date We must receive comments by January 25, 2019. (b) Affected ADs This AD affects AD 2008-02-15, Amendment 39-15345 (73 FR 4063, January 24, 2008) (``AD 2008-02-15''). (c) Applicability This AD applies to Airbus SAS Model A318-111, -112, -121, and - 122 airplanes, Model A319-111, -112, -113, -114, -115, -131, -132, and -133 airplanes, Model A320-211, -212, -214, -216, -231, -232, and -233 airplanes, and Model A321-111, -112, -131, -211, -212, - 213, -231, and -232 airplanes, certificated in any category, as identified in the European Aviation Safety Agency (EASA) AD 2018- 0218, dated October 11, 2018; corrected October 26, 2018 (``EASA AD 2018-0218''). (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Reason This AD was prompted by a report that taperloks used in the wing-to-fuselage junction at rib 1 were found to be non-compliant with the applicable specification, resulting in a loss of pre- tension in the fasteners. We are issuing this AD to address the loss of pre-tension in the fasteners, which could affect the structural integrity of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Requirements Except as specified in paragraph (h) of this AD: Comply with all required actions and compliance times specified in, and in accordance with, EASA AD 2018-0218. (h) Exceptions to EASA AD 2018-0218 (1) For purposes of determining compliance with the requirements of this AD: Where EASA AD 2018-0218 refers to its effective date, this AD requires using the effective date of this AD. (2) The ``Remarks'' section of EASA AD 2018-0218 does not apply. (3) Where EASA AD 2018-0218 refers to instructions provided by Airbus, for this AD, the instructions must be approved 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. (i) Terminating Action for AD 2008-02-15 Accomplishing the actions required by this AD terminates all requirements of AD 2008-02-15. (j) 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 (k)(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 [[Page 63601]] 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): Except as required by paragraph (j)(2) of this AD: Any RC procedures and tests identified in the service information referenced in EASA AD 2018-0218 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. (k) Related Information (1) For information about EASA AD 2018-0218, contact 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 EASA AD 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. EASA AD 2018-0218 may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-1007. (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 29, 2018. James Cashdollar, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-26624 Filed 12-10-18; 8:45 am] BILLING CODE 4910-13-P
![63598 Federal Register / Vol. 83, No. 237 / Tuesday, December 11, 2018 / Proposed Rules
(g) Replacement by the Manager, International Section, compliant with the applicable
Within 36 months after the effective date Transport Standards Branch, FAA; or the specification, resulting in a loss of pre-
of this AD, remove the upper front relay box, Civil Aviation Authority of Israel (CAAI); or tension in the fasteners. This proposed
Israel Aerospace Industries (IAI) part number the CAAI’s authorized Designee. If approved
AD would require repetitive special
(P/N) 25G8130301–510/–512/–514/–516, and by the CAAI Designee, the approval must
include the Designee’s authorized signature. detailed inspections of the center and
replace with IAI P/N 25G8130301–516, outer wing box lower stiffeners and
upgraded to MOD A, and remove the lower (k) Related Information
front relay box, IAI P/N 25G8130300–512/–
panels at a certain junction on the left-
516/–518/–520, and replace with an (1) Refer to Mandatory Continuing and right-hand sides for any cracking,
improved lower front relay box, IAI P/N Airworthiness Information (MCAI) Israeli and repair if necessary. We are
25G8130300–520, upgraded to MOD A, in Airworthiness Directive ISR–I–24–2018–09– proposing this AD to address the unsafe
7, dated October 1, 2018, for related
accordance with the Accomplishment condition on these products.
Instructions of Gulfstream Service Bulletin information. This MCAI may be found in the
AD docket on the internet at http:// DATES: We must receive comments on
150–24–193, dated March 30, 2018. this proposed AD by January 25, 2019.
www.regulations.gov by searching for and
(h) Parts Installation Prohibition locating Docket No. FAA–2018–1006. ADDRESSES: You may send comments,
As of the applicable compliance time (2) For more information about this AD, using the procedures found in 14 CFR
specified in paragraph (h)(1) or (h)(2) of this contact Tom Rodriguez, Aerospace Engineer, 11.43 and 11.45, by any of the following
AD, do not install relay box IAI P/N International Section, Transport Standards
Branch, FAA, 2200 South 216th St., Des methods:
25G8130301–510/–512/–514/–516 or IAI P/N
Moines, WA 98198; telephone and fax 206– • Federal eRulemaking Portal: Go to
25G8130300–512/–516/–518/–520 on any http://www.regulations.gov. Follow the
airplane, except relay box IAI P/N 231–3226.
25G8130301–516 or IAI P/N 25G8130300– (3) For service information identified in instructions for submitting comments.
520 that has been upgraded to MOD A as this AD, contact Gulfstream Aerospace • Fax: 202–493–2251.
specified in paragraph (g) of this AD may be Corporation, P.O. Box 2206, Mail Station D– • Mail: U.S. Department of
installed. 25, Savannah, GA 31402–2206; telephone Transportation, Docket Operations, M–
(1) For airplanes that have IAI P/N 800–810–4853; fax 912–965–3520; email 30, West Building Ground Floor, Room
25G8130301–510/–512/–514/–516 or IAI P/N pubs@gulfstream.com; internet http:// W12–140, 1200 New Jersey Avenue SE,
25G8130300–512/–516/–518/–520 installed www.gulfstream.com/product_support/
Washington, DC 20590.
technical_pubs/pubs/index.htm. You may
as of the effective date of this AD: After
view this service information at the FAA, • Hand Delivery: Deliver to Mail
modification of the airplane as required by address above between 9 a.m. and 5
this AD. Transport Standards Branch, 2200 South
216th St., Des Moines, WA. For information p.m., Monday through Friday, except
(2) For airplanes that do not have IAI P/
N 25G8130301–510/–512/–514/–516 or IAI on the availability of this material at the Federal holidays.
P/N 25G8130300–512/–516/–518/–520 FAA, call 206–231–3195. For the incorporation by reference
installed as of the effective date of this AD: Issued in Des Moines, Washington, on (IBR) material described in the ‘‘Related
As of the effective date of this AD. November 29, 2018. IBR material under 1 CFR part 51’’
James Cashdollar, section in SUPPLEMENTARY INFORMATION,
(i) No Parts Return or Reporting
Requirement Acting Director, System Oversight Division,
contact EASA, Konrad-Adenauer-Ufer 3,
Aircraft Certification Service. 50668 Cologne, Germany; telephone +49
(1) Although Gulfstream Service Bulletin 221 89990 1000; email ADs@
150–24–193, dated March 30, 2018, specifies [FR Doc. 2018–26623 Filed 12–10–18; 8:45 am]
returning parts to the manufacturer, this AD
easa.europa.eu; internet
BILLING CODE 4910–13–P
does not include that requirement. www.easa.europa.eu. You may find this
(2) Although Gulfstream Service Bulletin IBR material on the EASA website at
150–24–193, dated March 30, 2018, specifies DEPARTMENT OF TRANSPORTATION https://ad.easa.europa.eu. You may
to submit certain information to the view this IBR material at the FAA,
manufacturer, this AD does not include that Federal Aviation Administration Transport Standards Branch, 2200
requirement. South 216th St., Des Moines, WA. For
(j) Other FAA AD Provisions 14 CFR Part 39 information on the availability of this
The following provisions also apply to this
material at the FAA, call 206–231–3195.
[Docket No. FAA–2018–1007; Product It is also available in the AD docket on
AD: Identifier 2018–NM–141–AD]
(1) Alternative Methods of Compliance the internet at http://
(AMOCs): The Manager, International RIN 2120–AA64 www.regulations.gov.
Section, Transport Standards Branch, FAA,
has the authority to approve AMOCs for this Airworthiness Directives; Airbus SAS Examining the AD Docket
AD, if requested using the procedures found Airplanes You may examine the AD docket on
in 14 CFR 39.19. In accordance with 14 CFR the internet at http://
39.19, send your request to your principal AGENCY: Federal Aviation
Administration (FAA), DOT. www.regulations.gov by searching for
inspector or local Flight Standards District and locating Docket No. FAA–2018–
Office, as appropriate. If sending information ACTION: Notice of proposed rulemaking
1007; or in person at the Docket
directly to the International Section, send it (NPRM).
to the attention of the person identified in Management Facility between 9 a.m.
paragraph (k)(2) of this AD. Information may SUMMARY: We propose to adopt a new and 5 p.m., Monday through Friday,
be emailed to: 9-ANM-116-AMOC- airworthiness directive (AD) for certain except Federal holidays. The AD docket
REQUESTS@faa.gov. Before using any Airbus SAS Model A318 and A319 contains this NPRM, the regulatory
amozie on DSK3GDR082PROD with PROPOSALS1
approved AMOC, notify your appropriate series airplanes, Model A320–211, –212, evaluation, any comments received, and
principal inspector, or lacking a principal –214, –216, –231, –232, and –233 other information. The street address for
inspector, the manager of the local flight the Docket Operations office (telephone
airplanes, and Model A321–111, –112,
standards district office/certificate holding 800–647–5527) is in the ADDRESSES
district office. –131, –211, –212, –213, –231, and –232
airplanes. This proposed AD was section. Comments will be available in
(2) Contacting the Manufacturer: For any
requirement in this AD to obtain corrective prompted by a report that taperloks the AD docket shortly after receipt.
actions from a manufacturer, the action must used in a certain wing-to-fuselage FOR FURTHER INFORMATION CONTACT:
be accomplished using a method approved junction were found to be non- Sanjay Ralhan, Aerospace Engineer,
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![Federal Register / Vol. 83, No. 237 / Tuesday, December 11, 2018 / Proposed Rules 63599
International Section, Transport 2008–02–15, Amendment 39–15345 (73 FR country, and is approved for operation
Standards Branch, FAA, 2200 South 4063, January 24, 2008) (‘‘AD 2008–02–15’’)], in the United States. Pursuant to our
216th St., Des Moines, WA 98198; to require accomplishment of these bilateral agreement with the State of
inspections.
telephone and fax 206–231–3223. Design Authority, we have been notified
Since EASA AD 2007–0067R1 was issued,
SUPPLEMENTARY INFORMATION: new events and the results of studies of the unsafe condition described in the
identified an aging effect on these parts. MCAI referenced above. We are
Comments Invited
Prompted by these findings, Airbus revised proposing this AD because we evaluated
We invite you to send any written SB A320–57–1129 (now at Revision 05) and all pertinent information and
relevant data, views, or arguments about A320–57–1130 (now at Revision 04), determined an unsafe condition exists
this proposal. Send your comments to expanding the applicability, modifying the and is likely to exist or develop on other
an address listed under the ADDRESSES area to be inspected and updating the
inspection intervals.
products of the same type design.
section. Include ‘‘Docket No. FAA–
For the reasons stated above, this [EASA] Explanation of Required Compliance
2018–1007; Product Identifier 2018– AD retains the requirements of EASA AD
NM–141–AD’’ at the beginning of your Information
2007–0067R1, which is superseded, expands
comments. We specifically invite the Applicability, modifies the areas to be In the FAA’s ongoing efforts to
comments on the overall regulatory, inspected and revises the inspection
thresholds and intervals.
improve the efficiency of the AD
economic, environmental, and energy
This [EASA] AD is republished to correct process, the FAA worked with Airbus
aspects of this NPRM. We will consider
typographical errors in paragraph (2) and in and the EASA to develop a process to
all comments received by the closing
Tables 1 and 3. use certain EASA ADs as the primary
date and may amend this NPRM based
source of information for compliance
on those comments. Relationship Between Proposed AD and
We will post all comments we with requirements for corresponding
AD 2008–02–15 FAA ADs. As a result, EASA AD 2018–
receive, without change, to http://
www.regulations.gov, including any This NPRM would not supersede AD 0218 will be incorporated by reference
personal information you provide. We 2008–02–15. Rather, we have in the FAA final rule. This proposed AD
will also post a report summarizing each determined that a stand-alone AD would, therefore, require compliance
substantive verbal contact we receive would be more appropriate to address with the provisions specified in EASA
about this NPRM. the changes in the MCAI. This NPRM AD 2018–0218, except for any
would require repetitive special detailed differences identified as exceptions in
Discussion inspections of the center and outer wing the regulatory text of this proposed AD.
The European Aviation Safety Agency box lower stiffeners and panels at the Service information specified in EASA
(EASA), which is the Technical Agent level of rib 1 junction on the left- and AD 2018–0218 that is required for
for the Member States of the European right-hand sides for any cracking, and compliance with EASA AD 2018–0218
Union, has issued EASA AD 2018–0218, repair if necessary. Accomplishment of will be available at http://
dated October 11, 2018; corrected the proposed actions would then www.regulations.gov under Docket No.
October 26, 2018 (‘‘EASA AD 2018– terminate all of the requirements of AD FAA–2018–1007 after the FAA final
0218’’) (also referred to as the 2008–02–15. rule is published.
Mandatory Continuing Airworthiness Related IBR Material Under 1 CFR Part Explanation of ‘‘RC’’ (Required for
Information, or ‘‘the MCAI’’), to correct 51 Compliance)
an unsafe condition for certain Airbus
SAS Model A318 and A319 series EASA AD 2018–0218 describes EASA AD 2018–0218, dated October
airplanes, Model A320–211, –212, –214, procedures for repetitive special 11, 2018; corrected October 26, 2018;
–216, –231, –232, and –233 airplanes, detailed inspections of the center and might refer to service information that
and Model A321–111, –112, –131, –211, outer wing box lower stiffeners and contains procedures or tests that are
–212, –213, –231, and –232 airplanes. panels at the level of rib 1 junction on identified as RC. Those procedures and
The MCAI states: the left- and right-hand sides for any tests that are not identified as RC may
cracking, and repair if necessary. EASA
Taperloks used in the wing-to-fuselage be deviated from using accepted
AD 2018–0218 also provides procedures
junction at Rib 1 were found to be non- methods in accordance with the
for an optional modification, which
compliant with the applicable specification, operator’s maintenance or inspection
resulting in a loss of pre-tension in the would terminate the repetitive
program without obtaining approval of
fasteners. inspections. This material is reasonably
an alternative method of compliance
This condition, if not detected and available because the interested parties
(AMOC), provided the procedures and
corrected, could affect the structural integrity have access to it through their normal
of the aeroplane. To address this potential tests identified as RC can be done and
course of business or by the means
unsafe condition, Airbus issued SB A320– the airplane can be put back in an
identified in the ADDRESSES section and
57–1129 and SB A320–57–1130, later revised airworthy condition.
it is publicly available through the
twice, providing instructions for repetitive
internal inspections of the lower stiffeners
EASA website. Costs of Compliance
and for repetitive external inspections of the FAA’s Determination and Requirements
lower panels of the center and outer wing We estimate that this proposed AD
of This Proposed AD affects 516 airplanes of U.S. registry. We
box at the level of Rib 1 junction.
Consequently, EASA issued AD 2007–0067, This product has been approved by estimate the following costs to comply
amozie on DSK3GDR082PROD with PROPOSALS1
later revised [which corresponds to FAA AD the aviation authority of another with this proposed AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Cost per Cost on
Labor cost Parts cost product U.S. operators
51 work-hours × $85 per hour = $4,335 ..................................................................................... $0 $4,335 $2,236,860
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![63600 Federal Register / Vol. 83, No. 237 / Tuesday, December 11, 2018 / Proposed Rules
We have received no definitive data estimates for the on-condition actions
that would enable us to provide cost specified in this proposed AD.
ESTIMATED COSTS FOR OPTIONAL ACTIONS
Cost per
Labor cost Parts cost product
244 work-hours × $85 per hour = $20,740 ............................................................................................................. $5,120 $25,860
Authority for This Rulemaking 4. Will not have a significant compliant with the applicable specification,
economic impact, positive or negative, resulting in a loss of pre-tension in the
Title 49 of the United States Code fasteners. We are issuing this AD to address
specifies the FAA’s authority to issue on a substantial number of small entities
the loss of pre-tension in the fasteners, which
rules on aviation safety. Subtitle I, under the criteria of the Regulatory
could affect the structural integrity of the
section 106, describes the authority of Flexibility Act. airplane.
the FAA Administrator. Subtitle VII: List of Subjects in 14 CFR Part 39 (f) Compliance
Aviation Programs, describes in more
Air transportation, Aircraft, Aviation Comply with this AD within the
detail the scope of the Agency’s
safety, Incorporation by reference, compliance times specified, unless already
authority. done.
We are issuing this rulemaking under Safety.
the authority described in Subtitle VII, The Proposed Amendment (g) Requirements
Part A, Subpart III, Section 44701: Accordingly, under the authority Except as specified in paragraph (h) of this
‘‘General requirements.’’ Under that delegated to me by the Administrator,
AD: Comply with all required actions and
section, Congress charges the FAA with compliance times specified in, and in
the FAA proposes to amend 14 CFR part accordance with, EASA AD 2018–0218.
promoting safe flight of civil aircraft in 39 as follows:
air commerce by prescribing regulations (h) Exceptions to EASA AD 2018–0218
for practices, methods, and procedures PART 39—AIRWORTHINESS (1) For purposes of determining
the Administrator finds necessary for DIRECTIVES compliance with the requirements of this AD:
safety in air commerce. This regulation Where EASA AD 2018–0218 refers to its
is within the scope of that authority ■ 1. The authority citation for part 39 effective date, this AD requires using the
because it addresses an unsafe condition continues to read as follows: effective date of this AD.
that is likely to exist or develop on (2) The ‘‘Remarks’’ section of EASA AD
Authority: 49 U.S.C. 106(g), 40113, 44701.
products identified in this rulemaking 2018–0218 does not apply.
§ 39.13 [Amended] (3) Where EASA AD 2018–0218 refers to
action. instructions provided by Airbus, for this AD,
This proposed AD is issued in ■ 2. The FAA amends § 39.13 by adding the instructions must be approved using a
accordance with authority delegated by the following new airworthiness method approved by the Manager,
the Executive Director, Aircraft directive (AD): International Section, Transport Standards
Certification Service, as authorized by Airbus SAS: Docket No. FAA–2018–1007; Branch, FAA; or EASA; or Airbus SAS’s
FAA Order 8000.51C. In accordance Product Identifier 2018–NM–141–AD. EASA Design Organization Approval (DOA).
with that order, issuance of ADs is If approved by the DOA, the approval must
normally a function of the Compliance (a) Comments Due Date include the DOA-authorized signature.
and Airworthiness Division, but during We must receive comments by January 25, (i) Terminating Action for AD 2008–02–15
this transition period, the Executive 2019.
Accomplishing the actions required by this
Director has delegated the authority to (b) Affected ADs AD terminates all requirements of AD 2008–
issue ADs applicable to transport This AD affects AD 2008–02–15, 02–15.
category airplanes to the Director of the Amendment 39–15345 (73 FR 4063, January (j) Other FAA AD Provisions
System Oversight Division. 24, 2008) (‘‘AD 2008–02–15’’).
The following provisions also apply to this
Regulatory Findings (c) Applicability AD:
We determined that this proposed AD This AD applies to Airbus SAS Model (1) Alternative Methods of Compliance
A318–111, –112, –121, and –122 airplanes, (AMOCs): The Manager, International
would not have federalism implications
Model A319–111, –112, –113, –114, –115, Section, Transport Standards Branch, FAA,
under Executive Order 13132. This has the authority to approve AMOCs for this
proposed AD would not have a –131, –132, and –133 airplanes, Model
A320–211, –212, –214, –216, –231, –232, and AD, if requested using the procedures found
substantial direct effect on the States, on –233 airplanes, and Model A321–111, –112, in 14 CFR 39.19. In accordance with 14 CFR
the relationship between the national –131, –211, –212, –213, –231, and –232 39.19, send your request to your principal
Government and the States, or on the airplanes, certificated in any category, as inspector or local Flight Standards District
distribution of power and identified in the European Aviation Safety Office, as appropriate. If sending information
responsibilities among the various Agency (EASA) AD 2018–0218, dated directly to the International Section, send it
levels of government. October 11, 2018; corrected October 26, 2018 to the attention of the person identified in
For the reasons discussed above, I (‘‘EASA AD 2018–0218’’). paragraph (k)(2) of this AD. Information may
amozie on DSK3GDR082PROD with PROPOSALS1
be emailed to: 9-ANM-116-AMOC-
certify this proposed regulation: (d) Subject REQUESTS@faa.gov. Before using any
1. Is not a ‘‘significant regulatory
Air Transport Association (ATA) of approved AMOC, notify your appropriate
action’’ under Executive Order 12866; principal inspector, or lacking a principal
America Code 57, Wings.
2. Is not a ‘‘significant rule’’ under the inspector, the manager of the local flight
DOT Regulatory Policies and Procedures (e) Reason standards district office/certificate holding
(44 FR 11034, February 26, 1979); This AD was prompted by a report that district office.
3. Will not affect intrastate aviation in taperloks used in the wing-to-fuselage (2) Contacting the Manufacturer: For any
Alaska; and junction at rib 1 were found to be non- requirement in this AD to obtain instructions
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![Federal Register / Vol. 83, No. 237 / Tuesday, December 11, 2018 / Proposed Rules 63601
from a manufacturer, the instructions must Notice of proposed rulemaking
ACTION: Subtitle VII, Aviation Programs,
be accomplished using a method approved (NPRM). describes in more detail the scope of the
by the Manager, International Section, agency’s authority. This rulemaking is
Transport Standards Branch, FAA; or EASA; SUMMARY: This action proposes to promulgated under the authority
or Airbus SAS’s EASA Design Organization amend VHF Omnidirectional Range
Approval (DOA). If approved by the DOA,
described in Subtitle VII, Part A,
(VOR) Federal airways V–128 and V– Subpart I, Section 40103. Under that
the approval must include the DOA- 144 in the vicinity of Kankakee, IL. The
authorized signature. section, the FAA is charged with
(3) Required for Compliance (RC): Except
modifications are necessary due to the prescribing regulations to assign the use
as required by paragraph (j)(2) of this AD: planned decommissioning of the of the airspace necessary to ensure the
Any RC procedures and tests identified in the Kankakee, IL (IKK), VOR navigation aid safety of aircraft and the efficient use of
service information referenced in EASA AD (NAVAID), which provides navigation airspace. This regulation is within the
2018–0218 must be done to comply with this guidance for portions of the affected air scope of that authority as it would
AD; any procedures or tests that are not traffic service (ATS) routes. The modify the National Airspace System as
identified as RC are recommended. Those Kankakee VOR is being necessary to preserve the safe and
procedures and tests that are not identified decommissioned as part of the FAA’s
as RC may be deviated from using accepted
efficient flow of air traffic.
VOR Minimum Operational Network
methods in accordance with the operator’s Comments Invited
maintenance or inspection program without
(MON) program.
obtaining approval of an AMOC, provided DATES: Comments must be received on Interested parties are invited to
the procedures and tests identified as RC can or before January 25, 2019. participate in this proposed rulemaking
be done and the airplane can be put back in ADDRESSES: Send comments on this
by submitting such written data, views,
an airworthy condition. Any substitutions or proposal to the U.S. Department of or arguments as they may desire.
changes to procedures or tests identified as
Transportation, Docket Operations, 1200 Comments that provide the factual basis
RC require approval of an AMOC. supporting the views and suggestions
New Jersey Avenue SE, West Building
(k) Related Information Ground Floor, Room W12–140, presented are particularly helpful in
Washington, DC 20590; telephone: developing reasoned regulatory
(1) For information about EASA AD 2018–
0218, contact EASA, Konrad-Adenauer-Ufer 1(800) 647–5527, or (202) 366–9826. decisions on the proposal. Comments
3, 50668 Cologne, Germany; telephone +49 You must identify FAA Docket No. are specifically invited on the overall
221 89990 6017; email ADs@easa.europa.eu; FAA–2018–0990; Airspace Docket No. regulatory, aeronautical, economic,
Internet www.easa.europa.eu. You may find 18–AGL–13 at the beginning of your environmental, and energy-related
this EASA AD on the EASA website at
comments. You may also submit aspects of the proposal.
https://ad.easa.europa.eu. You may view this Communications should identify both
EASA AD at the FAA, Transport Standards comments through the internet at http://
docket numbers (FAA Docket No. FAA–
Branch, 2200 South 216th St., Des Moines, www.regulations.gov.
2018–0990; Airspace Docket No.
WA. For information on the availability of FAA Order 7400.11C, Airspace
18–AGL–13) and be submitted in
this material at the FAA, call 206–231–3195. Designations and Reporting Points, and
triplicate to the Docket Management
EASA AD 2018–0218 may be found in the subsequent amendments can be viewed
AD docket on the internet at http:// Facility (see ADDRESSES section for
online at http://www.faa.gov/air_traffic/
www.regulations.gov by searching for and publications/. For further information, address and phone number). You may
locating Docket No. FAA–2018–1007. you can contact the Airspace Policy also submit comments through the
(2) For more information about this AD,
Group, Federal Aviation internet at http://www.regulations.gov.
contact Sanjay Ralhan, Aerospace Engineer, Commenters wishing the FAA to
International Section, Transport Standards Administration, 800 Independence
acknowledge receipt of their comments
Branch, FAA, 2200 South 216th St., Des Avenue SW, Washington, DC 20591;
on this action must submit with those
Moines, WA 98198; telephone and fax 206– telephone: (202) 267–8783. The Order is
comments a self-addressed, stamped
231–3223. also available for inspection at the
postcard on which the following
Issued in Des Moines, Washington, on National Archives and Records
statement is made: ‘‘Comments to FAA
November 29, 2018. Administration (NARA). For
Docket No. FAA–2018–0990; Airspace
James Cashdollar, information on the availability of FAA
Docket No. 18–AGL–13.’’ The postcard
Order 7400.11C at NARA, call (202)
Acting Director, System Oversight Division, will be date/time stamped and returned
Aircraft Certification Service. 741–6030, or go to https://
to the commenter.
www.archives.gov/federal-register/cfr/ All communications received on or
[FR Doc. 2018–26624 Filed 12–10–18; 8:45 am]
ibr-locations.html. before the specified comment closing
BILLING CODE 4910–13–P
FAA Order 7400.11, Airspace date will be considered before taking
Designations and Reporting Points, is action on the proposed rule. The
published yearly and effective on proposal contained in this action may
DEPARTMENT OF TRANSPORTATION
September 15. be changed in light of comments
Federal Aviation Administration FOR FURTHER INFORMATION CONTACT: received. All comments submitted will
Colby Abbott, Airspace Policy Group, be available for examination in the
14 CFR Part 71 Office of Airspace Services, Federal public docket both before and after the
Aviation Administration, 800 comment closing date. A report
[Docket No. FAA–2018–0990; Airspace Independence Avenue SW, Washington, summarizing each substantive public
Docket No. 18–AGL–13] DC 20591; telephone: (202) 267–8783. contact with FAA personnel concerned
amozie on DSK3GDR082PROD with PROPOSALS1
SUPPLEMENTARY INFORMATION: with this rulemaking will be filed in the
RIN 2120–AA66
Authority for This Rulemaking docket.
Proposed Amendment of VOR Federal Availability of NPRMs
Airways V–128 and V–144 in the The FAA’s authority to issue rules
Vicinity of Kankakee, IL regarding aviation safety is found in An electronic copy of this document
Title 49 of the United States Code. may be downloaded through the
AGENCY:Federal Aviation Subtitle I, Section 106 describes the internet at http://www.regulations.gov.
Administration (FAA), DOT. authority of the FAA Administrator. Recently published rulemaking
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Document Created: 2018-12-11 01:06:27
Document Modified: 2018-12-11 01:06:27
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Proposed Rules | |
| Action | Notice of proposed rulemaking (NPRM). | |
| Dates | We must receive comments on this proposed AD by January 25, 2019. | |
| 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. | |
| FR Citation | 83 FR 63598 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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