83 FR 2894 - Airworthiness Directives; Airbus Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 14 (January 22, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 14 (January 22, 2018)
| Page Range | 2894-2896 | |
| FR Document | 2018-00949 |
[Federal Register Volume 83, Number 14 (Monday, January 22, 2018)] [Rules and Regulations] [Pages 2894-2896] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-00949] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0023; Product Identifier 2017-NM-084-AD; Amendment 39-19164; AD 2018-02-11] RIN 2120-AA64 Airworthiness Directives; Airbus Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Airbus Model A330-301, -321, -322 and -342 airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition on these products, and doing the actions specified in those instructions. This AD was prompted by a report of cracking in the top skin of the horizontal stabilizer (HS) center box (CB) of an airplane in pre-modification 41330 configuration. We are issuing this AD to address the unsafe condition on these products. DATES: This AD becomes effective February 6, 2018. We must receive comments on this AD by March 8, 2018. 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: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. 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- 0023; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, 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: Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone: 425-227-1138; fax: 425- 227-1149. SUPPLEMENTARY INFORMATION: Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2017-0078, dated May 3, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Airbus Model A330-301, -321, -322 and -342 airplanes. The MCAI states: Cracks were found in the horizontal stabilizer (HS) centre box (CB) top skin of an aeroplane in pre-modification 41330 configuration. The cracks were initiated at the upper flange corner at Rib 3 rear spar area on left hand side of the CB. This condition, if not detected and corrected, could lead to reduced structural integrity of the HS CB of the aeroplane. To address this unsafe condition, Airbus published Service Bulletin (SB) A330-55-3046 to provide inspection instructions for the affected area. For the reason described above, this [EASA] AD requires a one- time special detailed inspection (SDI) of the HS CB top [[Page 2895]] skin integral flange area and, depending on findings, accomplishment of applicable corrective action(s). This [EASA] AD also requires reporting of the inspection results, including no findings, to Airbus. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0023. FAA's Determination and Requirements of This 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. We are issuing this AD because we evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of the same type design. FAA's Determination of the Effective Date Since there are currently no domestic operators of this product, we find good cause that notice and opportunity for prior public comment are unnecessary. In addition, for the reasons stated above, we find that good cause exists for making this amendment effective in less than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and opportunity for public comment. We invite you to send any written relevant data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA-2018-0023; Product Identifier 2017-NM-084-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD 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 AD. Costs of Compliance Currently, there are no affected U.S.-registered airplanes. This AD requires contacting the FAA to obtain instructions for addressing the unsafe condition, and doing the actions specified in those instructions. Based on the actions specified in the MCAI AD, we are providing the following cost estimates for an affected airplane that is placed on the U.S. Register in the future: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- High frequency eddy current inspection..... 1 work-hour x $85 per hour = $85... $0 $85 Reporting.................................. 1 work-hour x $85 per hour = $85... 0 85 ---------------------------------------------------------------------------------------------------------------- We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this AD. Paperwork Reduction Act A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB control number. The control number for the collection of information required by this AD is 2120- 0056. The paperwork cost associated with this AD has been detailed in the Costs of Compliance section of this document and includes time for reviewing instructions, as well as completing and reviewing the collection of information. Therefore, all reporting associated with this AD is mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at 800 Independence Ave. SW, Washington, DC 20591, ATTN: Information Collection Clearance Officer, AES-200. 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 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 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. 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. [[Page 2896]] Adoption of 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 (AD): 2018-02-11 Airbus: Amendment 39-19164; Docket No. FAA-2018-0023; Product Identifier 2017-NM-084-AD. (a) Effective Date This AD becomes effective February 6, 2018. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Model A330-301, -321, -322 and A330- 342 airplanes, certificated in any category, manufacturer serial numbers 0012, 0017, 0030, 0037, 0045, 0050, 0060, 0062, 0064, 0065, 0071, 0082, 0083, 0098, 0099, 0102, 0106, 0109, 0112, 0132 and 0177. (d) Subject Air Transport Association (ATA) of America Code 55, Stabilizers. (e) Reason This AD was prompted by a report of cracking in the top skin of the horizontal stabilizer (HS) center box (CB) of an airplane in pre-modification 41330 configuration. We are issuing this AD to detect and correct cracking in the HS CB, which could lead to reduced structural integrity of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Required Action(s) Within 30 days after the effective date of this AD, request instructions from the Manager, International Section, Transport Standards Branch, FAA, to address the unsafe condition specified in paragraph (e) of this AD; and accomplish the actions at the times specified in, and in accordance with, those instructions. Guidance can be found in Mandatory Continuing Airworthiness Information (MCAI) European Aviation Safety Agency (EASA) AD 2017-0078, dated May 3, 2017. (h) 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. (i) Paperwork Reduction Act Burden Statement A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to a penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB Control Number. The OMB Control Number for this information collection is 2120-0056. Public reporting for this collection of information is estimated to be approximately 1 hour per response, including the time for reviewing instructions, completing and reviewing the collection of information. All responses to this collection of information are mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at: 800 Independence Ave. SW, Washington, DC 20591, Attn: Information Collection Clearance Officer, AES-200. (j) Related Information (1) Refer to MCAI EASA AD 2017-0078, dated May 3, 2017, for related information. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0023. (2) For more information about this AD, contact Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone: 425-227-1138; fax: 425-227-1149. (k) Material Incorporated by Reference None. Issued in Renton, Washington, on January 10, 2018. John P. Piccola, Jr., Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-00949 Filed 1-19-18; 8:45 am] BILLING CODE 4910-13-P
![2894 Federal Register / Vol. 83, No. 14 / Monday, January 22, 2018 / Rules and Regulations
PART 690—PROTECTION OF HUMAN pursuant to § 11.101(i), or for which a • Federal eRulemaking Portal: Go to
SUBJECTS determination was made that the http://www.regulations.gov. Follow the
research was exempt before July 19, instructions for submitting comments.
■ 1. The authority citation for 690 2018, shall comply with the pre-2018 • Fax: 202–493–2251.
continues to read as follows: Requirements, except that an institution • Mail: U.S. Department of
Authority: 5 U.S.C. 301; 42 U.S.C. 300v– engaged in such research on or after July Transportation, Docket Operations,
1(b). 19, 2018 may instead comply with the M–30, West Building Ground Floor,
■ 2. Amend § 690.101 by revising 2018 Requirements if the institution Room W12–140, 1200 New Jersey
paragraphs (l)(3) and (4) to read as determines that such ongoing research Avenue SE, Washington, DC 20590.
follows: will comply with the 2018 • Hand Delivery: U.S. Department of
Requirements and an IRB documents Transportation, Docket Operations,
§ 690.101 To what does this policy apply? M–30, West Building Ground Floor,
such determination.
* * * * * (4) Research initially approved by an Room W12–140, 1200 New Jersey
(l) * * * IRB, for which such review was waived Avenue SE, Washington, DC, between 9
(3) Research initially approved by an pursuant to § 11.101(i), or for which a a.m. and 5 p.m., Monday through
IRB, for which such review was waived determination was made that the Friday, except Federal holidays.
pursuant to § 690.101(i), or for which a research was exempt on or after July 19,
determination was made that the Examining the AD Docket
2018, shall comply with the 2018
research was exempt before July 19, Requirements. You may examine the AD docket on
2018, shall comply with the pre-2018 the internet at http://
Requirements, except that an institution * * * * * www.regulations.gov by searching for
Elaine L. Chao,
engaged in such research on or after July Secretary of Transportation.
and locating Docket No. FAA–2018–
19, 2018 may instead comply with the 0023; or in person at the Docket
[FR Doc. 2018–00997 Filed 1–17–18; 4:15 pm]
2018 Requirements if the institution Operations office between 9 a.m. and 5
BILLING CODE 4150–36–P p.m., Monday through Friday, except
determines that such ongoing research
will comply with the 2018 Federal holidays. The AD docket
Requirements and an IRB documents contains this AD, the regulatory
such determination. DEPARTMENT OF TRANSPORTATION evaluation, any comments received, and
(4) Research initially approved by an other information. The street address for
IRB, for which such review was waived Federal Aviation Administration the Docket Operations office (telephone:
pursuant to § 690.101(i), or for which a 800–647–5527) is in the ADDRESSES
determination was made that the 14 CFR Part 39 section. Comments will be available in
research was exempt on or after July 19, the AD docket shortly after receipt.
[Docket No. FAA–2018–0023; Product
2018, shall comply with the 2018 Identifier 2017–NM–084–AD; Amendment FOR FURTHER INFORMATION CONTACT:
Requirements. 39–19164; AD 2018–02–11] Vladimir Ulyanov, Aerospace Engineer,
* * * * * International Section, Transport
Lawrence Rudolph, RIN 2120–AA64 Standards Branch, FAA, 1601 Lind
General Counsel. Avenue SW, Renton, WA 98057–3356;
Airworthiness Directives; Airbus telephone: 425–227–1138; fax: 425–
DEPARTMENT OF TRANSPORTATION Airplanes 227–1149.
49 CFR Part 11 AGENCY: Federal Aviation SUPPLEMENTARY INFORMATION:
Administration (FAA), DOT. Discussion
List of Subjects in 49 CFR Part 11
ACTION: Final rule; request for
Human research subjects, Reporting The European Aviation Safety Agency
comments.
and record-keeping requirements, (EASA), which is the Technical Agent
Research. SUMMARY: We are adopting a new for the Member States of the European
For the reasons stated in the airworthiness directive (AD) for certain Union, has issued EASA AD 2017–0078,
preamble, the Department of Airbus Model A330–301, –321, –322 dated May 3, 2017 (referred to after this
Transportation further amends 49 CFR and –342 airplanes. This AD requires as the Mandatory Continuing
part 11 as published in the Federal contacting the FAA to obtain Airworthiness Information, or ‘‘the
Register on January 19, 2017 (82 FR instructions for addressing the unsafe MCAI’’), to correct an unsafe condition
7149) as follows: condition on these products, and doing for certain Airbus Model A330–301,
the actions specified in those –321, –322 and –342 airplanes. The
PART 11—PROTECTION OF HUMAN instructions. This AD was prompted by MCAI states:
SUBJECTS a report of cracking in the top skin of Cracks were found in the horizontal
■ 1. The authority citation for 11 the horizontal stabilizer (HS) center box stabilizer (HS) centre box (CB) top skin of an
(CB) of an airplane in pre-modification aeroplane in pre-modification 41330
continues to read as follows: configuration. The cracks were initiated at
41330 configuration. We are issuing this
Authority: 5 U.S.C. 301; 42 U.S.C. 300v– AD to address the unsafe condition on the upper flange corner at Rib 3 rear spar area
1(b). on left hand side of the CB.
these products. This condition, if not detected and
■ 2. Amend § 11.101 by revising
DATES: This AD becomes effective corrected, could lead to reduced structural
paragraphs (l)(3) and (4) to read as
February 6, 2018. integrity of the HS CB of the aeroplane.
ethrower on DSK3G9T082PROD with RULES
follows: To address this unsafe condition, Airbus
We must receive comments on this
§ 11.101 To what does this policy apply? AD by March 8, 2018. published Service Bulletin (SB) A330–55–
3046 to provide inspection instructions for
* * * * * ADDRESSES: You may send comments, the affected area.
(l) * * * using the procedures found in 14 CFR For the reason described above, this
(3) Research initially approved by an 11.43 and 11.45, by any of the following [EASA] AD requires a one-time special
IRB, for which such review was waived methods: detailed inspection (SDI) of the HS CB top
VerDate Sep<11>2014 15:52 Jan 19, 2018 Jkt 244001 PO 00000 Frm 00010 Fmt 4700 Sfmt 4700 E:\FR\FM\22JAR1.SGM 22JAR1](https://thefederalregister.org/doc/83_FR_2908/page/1.svg)
![Federal Register / Vol. 83, No. 14 / Monday, January 22, 2018 / Rules and Regulations 2895
skin integral flange area and, depending on FAA’s Determination of the Effective environmental, and energy aspects of
findings, accomplishment of applicable Date this AD. We will consider all comments
corrective action(s). This [EASA] AD also received by the closing date and may
requires reporting of the inspection results, Since there are currently no domestic
including no findings, to Airbus. operators of this product, we find good amend this AD based on those
cause that notice and opportunity for comments.
You may examine the MCAI on the prior public comment are unnecessary. We will post all comments we
internet at http://www.regulations.gov In addition, for the reasons stated above, receive, without change, to http://
by searching for and locating Docket No. we find that good cause exists for www.regulations.gov, including any
FAA–2018–0023. making this amendment effective in less personal information you provide. We
FAA’s Determination and Requirements than 30 days. will also post a report summarizing each
of This AD Comments Invited substantive verbal contact we receive
This product has been approved by about this AD.
This AD is a final rule that involves
the aviation authority of another requirements affecting flight safety, and Costs of Compliance
country, and is approved for operation we did not precede it by notice and
in the United States. Pursuant to our opportunity for public comment. We Currently, there are no affected U.S.-
bilateral agreement with the State of invite you to send any written relevant registered airplanes. This AD requires
Design Authority, we have been notified data, views, or arguments about this AD. contacting the FAA to obtain
of the unsafe condition described in the Send your comments to an address instructions for addressing the unsafe
MCAI. We are issuing this AD because listed under the ADDRESSES section. condition, and doing the actions
we evaluated all pertinent information Include ‘‘Docket No. FAA–2018–0023; specified in those instructions. Based on
and determined the unsafe condition Product Identifier 2017–NM–084–AD’’ the actions specified in the MCAI AD,
exists and is likely to exist or develop at the beginning of your comments. We we are providing the following cost
on other products of the same type specifically invite comments on the estimates for an affected airplane that is
design. overall regulatory, economic, placed on the U.S. Register in the future:
ESTIMATED COSTS
Cost per
Action Labor cost Parts cost product
High frequency eddy current inspection ....................... 1 work-hour × $85 per hour = $85 ............................... $0 $85
Reporting ...................................................................... 1 work-hour × $85 per hour = $85 ............................... 0 85
We have received no definitive data Authority for This Rulemaking delegated the authority to issue ADs
that would enable us to provide cost applicable to transport category
Title 49 of the United States Code
estimates for the on-condition actions airplanes to the Director of the System
specifies the FAA’s authority to issue
specified in this AD. Oversight Division.
rules on aviation safety. Subtitle I,
Paperwork Reduction Act section 106, describes the authority of Regulatory Findings
the FAA Administrator. ‘‘Subtitle VII: We determined that this AD will not
A federal agency may not conduct or Aviation Programs,’’ describes in more have federalism implications under
sponsor, and a person is not required to detail the scope of the Agency’s Executive Order 13132. This AD will
respond to, nor shall a person be subject authority. not have a substantial direct effect on
to penalty for failure to comply with a We are issuing this rulemaking under the States, on the relationship between
collection of information subject to the the authority described in ‘‘Subtitle VII, the national government and the States,
requirements of the Paperwork Part A, Subpart III, Section 44701: or on the distribution of power and
Reduction Act unless that collection of General requirements.’’ Under that responsibilities among the various
information displays a current valid section, Congress charges the FAA with levels of government.
OMB control number. The control promoting safe flight of civil aircraft in For the reasons discussed above, I
number for the collection of information air commerce by prescribing regulations certify that this AD:
required by this AD is 2120–0056. The for practices, methods, and procedures 1. Is not a ‘‘significant regulatory
paperwork cost associated with this AD the Administrator finds necessary for action’’ under Executive Order 12866;
has been detailed in the Costs of safety in air commerce. This regulation 2. Is not a ‘‘significant rule’’ under the
Compliance section of this document is within the scope of that authority DOT Regulatory Policies and Procedures
and includes time for reviewing because it addresses an unsafe condition (44 FR 11034, February 26, 1979);
instructions, as well as completing and that is likely to exist or develop on 3. Will not affect intrastate aviation in
reviewing the collection of information. products identified in this rulemaking Alaska; and
Therefore, all reporting associated with action. 4. Will not have a significant
this AD is mandatory. Comments This AD is issued in accordance with economic impact, positive or negative,
concerning the accuracy of this burden authority delegated by the Executive on a substantial number of small entities
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and suggestions for reducing the burden Director, Aircraft Certification Service, under the criteria of the Regulatory
should be directed to the FAA at 800 as authorized by FAA Order 8000.51C. Flexibility Act.
In accordance with that order, issuance
Independence Ave. SW, Washington, List of Subjects in 14 CFR Part 39
of ADs is normally a function of the
DC 20591, ATTN: Information
Compliance and Airworthiness Air transportation, Aircraft, Aviation
Collection Clearance Officer, AES–200. Division, but during this transition safety, Incorporation by reference,
period, the Executive Director has Safety.
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![2896 Federal Register / Vol. 83, No. 14 / Monday, January 22, 2018 / Rules and Regulations
Adoption of the Amendment requested using the procedures found in 14 DEPARTMENT OF TRANSPORTATION
CFR 39.19. In accordance with 14 CFR 39.19,
Accordingly, under the authority
send your request to your principal inspector Federal Aviation Administration
delegated to me by the Administrator, or local Flight Standards District Office, as
the FAA amends 14 CFR part 39 as appropriate. If sending information directly 14 CFR Part 39
follows: to the International Section, send it to the
[Docket No. FAA–2017–0719; Product
attention of the person identified in
PART 39—AIRWORTHINESS Identifier 2017–NE–22–AD; Amendment 39–
paragraph (j)(2) of this AD. Information may
DIRECTIVES 19163; AD 2018–02–10]
be emailed to: 9-ANM-116-AMOC-
REQUESTS@faa.gov. Before using any RIN 2120–AA64
■ 1. The authority citation for part 39
continues to read as follows: approved AMOC, notify your appropriate
principal inspector, or lacking a principal Airworthiness Directives; Pratt &
Authority: 49 U.S.C. 106(g), 40113, 44701. inspector, the manager of the local flight Whitney Division Turbofan Engines
§ 39.13 [Amended] standards district office/certificate holding AGENCY: Federal Aviation
district office. Administration (FAA), DOT.
■ 2. The FAA amends § 39.13 by adding
the following new airworthiness (i) Paperwork Reduction Act Burden ACTION: Final rule.
directive (AD): Statement
A federal agency may not conduct or
SUMMARY: We are adopting a new
2018–02–11 Airbus: Amendment 39–19164; airworthiness directive (AD) for all Pratt
Docket No. FAA–2018–0023; Product sponsor, and a person is not required to
respond to, nor shall a person be subject to & Whitney Division (PW) PW4074,
Identifier 2017–NM–084–AD.
a penalty for failure to comply with a PW4074D, PW4077, PW4077D,
(a) Effective Date PW4084D, PW4090, and PW4090–3
collection of information subject to the
This AD becomes effective February 6, requirements of the Paperwork Reduction turbofan engines. This AD was
2018. Act unless that collection of information prompted by the discovery of multiple
(b) Affected ADs displays a current valid OMB Control cracked outer diffuser cases. This AD
Number. The OMB Control Number for this requires initial and repetitive
None. inspections to detect cracks in the outer
information collection is 2120–0056. Public
(c) Applicability reporting for this collection of information is diffuser case and removal from service
This AD applies to Airbus Model A330– estimated to be approximately 1 hour per of cases that fail inspection. We are
301, –321, –322 and A330–342 airplanes, response, including the time for reviewing issuing this AD to address the unsafe
certificated in any category, manufacturer instructions, completing and reviewing the condition on these products.
serial numbers 0012, 0017, 0030, 0037, 0045, collection of information. All responses to DATES: This AD is effective February 26,
0050, 0060, 0062, 0064, 0065, 0071, 0082, this collection of information are mandatory. 2018.
0083, 0098, 0099, 0102, 0106, 0109, 0112,
Comments concerning the accuracy of this The Director of the Federal Register
0132 and 0177.
burden and suggestions for reducing the approved the incorporation by reference
(d) Subject burden should be directed to the FAA at: 800 of a certain publication listed in this AD
Air Transport Association (ATA) of Independence Ave. SW, Washington, DC as of February 26, 2018.
America Code 55, Stabilizers. 20591, Attn: Information Collection ADDRESSES: For service information
Clearance Officer, AES–200. identified in this final rule, contact Pratt
(e) Reason
This AD was prompted by a report of (j) Related Information & Whitney Division, 400 Main St., East
cracking in the top skin of the horizontal (1) Refer to MCAI EASA AD 2017–0078, Hartford, CT 06118; phone: 800–565–
stabilizer (HS) center box (CB) of an airplane dated May 3, 2017, for related information. 0140; fax: 860–565–5442. You may view
in pre-modification 41330 configuration. We You may examine the MCAI on the internet this service information at the FAA,
are issuing this AD to detect and correct Engine and Propeller Standards Branch,
at http://www.regulations.gov by searching
cracking in the HS CB, which could lead to 1200 District Avenue, Burlington, MA.
for and locating Docket No. FAA–2018–0023.
reduced structural integrity of the airplane. For information on the availability of
(2) For more information about this AD,
(f) Compliance contact Vladimir Ulyanov, Aerospace this material at the FAA, call 781–238–
Comply with this AD within the Engineer, International Section, Transport 7759. It is also available on the internet
compliance times specified, unless already Standards Branch, FAA, 1601 Lind Avenue at http://www.regulations.gov by
done. SW, Renton, WA 98057–3356; telephone: searching for and locating Docket No.
425–227–1138; fax: 425–227–1149. FAA–2017–0719.
(g) Required Action(s)
Within 30 days after the effective date of (k) Material Incorporated by Reference Examining the AD Docket
this AD, request instructions from the None. You may examine the AD docket on
Manager, International Section, Transport the internet at http://
Standards Branch, FAA, to address the Issued in Renton, Washington, on January
unsafe condition specified in paragraph (e) of 10, 2018. www.regulations.gov by searching for
this AD; and accomplish the actions at the and locating Docket No. FAA–2017–
John P. Piccola, Jr.,
times specified in, and in accordance with, 0719; or in person at Docket Operations
those instructions. Guidance can be found in Acting Director, System Oversight Division, between 9 a.m. and 5 p.m., Monday
Mandatory Continuing Airworthiness Aircraft Certification Service. through Friday, except Federal holidays.
Information (MCAI) European Aviation [FR Doc. 2018–00949 Filed 1–19–18; 8:45 am] The AD docket contains this final rule,
Safety Agency (EASA) AD 2017–0078, dated the regulatory evaluation, any
ethrower on DSK3G9T082PROD with RULES
BILLING CODE 4910–13–P
May 3, 2017. comments received, and other
(h) Alternative Methods of Compliance information. The address for Docket
(AMOCs) Operations (phone: 800–647–5527) is
The Manager, International Section, Document Operations, U.S. Department
Transport Standards Branch, FAA, has the of Transportation, Docket Operations,
authority to approve AMOCs for this AD, if M–30, West Building Ground Floor,
VerDate Sep<11>2014 15:52 Jan 19, 2018 Jkt 244001 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\22JAR1.SGM 22JAR1](https://thefederalregister.org/doc/83_FR_2908/page/3.svg)
Document Created: 2018-01-23 21:35:44
Document Modified: 2018-01-23 21:35:44
| 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 | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD becomes effective February 6, 2018. | |
| Contact | Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone: 425-227-1138; fax: 425- 227-1149. | |
| FR Citation | 83 FR 2894 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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