Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes, 24236-24240 [2018-11142]

Download as PDF 24236 Federal Register / Vol. 83, No. 102 / Friday, May 25, 2018 / Proposed Rules directly to the International Section, send it to the attention of the person identified in paragraph (l)(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 corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or Fokker Services B.V.’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (3) Reporting Requirements: 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. amozie on DSK3GDR082PROD with PROPOSALS1 (l) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2017–0163, dated September 4, 2017; corrected September 5, 2017; for related information. This MCAI may be found in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2018–0448. (2) For more information about this AD, contact Tom Rodriquez, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206– 231–3226. (3) For service information identified in this AD, contact Fokker Services B.V., Technical Services Dept., P.O. Box 1357, 2130 EL Hoofddorp, the Netherlands; telephone: +31 (0)88–6280–350; fax: +31 (0)88–6280–111; email: technicalservices@ fokker.com; internet: https:// www.myfokkerfleet.com. You may view this service information 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. VerDate Sep<11>2014 17:49 May 24, 2018 Jkt 244001 Issued in Des Moines, Washington, on May 15, 2018. Dionne Palermo, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018–11135 Filed 5–24–18; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2018–0416; Product Identifier 2017–NM–164–AD] RIN 2120–AA64 Airworthiness Directives; Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.) Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: SUMMARY: We propose to adopt a new airworthiness directive (AD) for all Airbus Defense and Space S.A. Model CN–235, CN–235–100, CN–235–200, and CN–235–300 airplanes; and certain Model C–295 airplanes. This proposed AD was prompted by a report that cracks were found on the stabilizer-tofuselage rear attachment fitting. This proposed AD would require a detailed inspection of the upper and lower lugs of each horizontal stabilizer-to-fuselage rear attachment fitting, repair if necessary, and a report of findings. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by July 9, 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 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 service information identified in this NPRM, contact Airbus Defense and Space Services/Engineering Support, ´ Avenida de Aragon 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax PO 00000 Frm 00004 Fmt 4702 Sfmt 4702 +34 91 585 31 27; email MTA.TechnicalService@airbus.com. You may view this service information 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. 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–2018– 0416; 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: Shahram Daneshmandi, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3220. 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– 2018–0416; Product Identifier 2017– NM–164–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 https:// 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 2017–0218, dated November 8, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all Airbus Defense and Space S.A. Model CN–235, CN–235–100, CN–235– 200, and CN–235–300 airplanes; and E:\FR\FM\25MYP1.SGM 25MYP1 24237 Federal Register / Vol. 83, No. 102 / Friday, May 25, 2018 / Proposed Rules certain Model C–295 airplanes. The MCAI states: Cracks were reportedly found on the stabilizer-to-fuselage rear attachment fitting of a CN–235 aeroplane. Subsequent investigation determined that the affected horizontal attachment fitting was a reworked part. This condition, if not detected and corrected, could lead to reduced structural integrity of lugs of the stabilizer-to-fuselage rear attachment fittings and consequent lug or fitting failure, possibly resulting in reduced control of the aeroplane. To address this potentially unsafe condition, Airbus Defence and Space (D&S) issued Alert Operators Transmission (AOT) AOT–C295–55–0005 and AOT–CN235–55– 0004 to provide inspection instructions. For the reasons described above, this [EASA] AD requires a one-time detailed inspection (DET) of the upper and lower lugs of the horizontal stabilizer-to-fuselage rear attachment fittings on the left hand (LH) and right hand (RH) sides and, depending on findings, accomplishment of applicable corrective action(s) [repairs]. This [EASA] AD also requires reporting of all findings, including none. You may examine the MCAI in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2018– 0416. Related Service Information Under 1 CFR Part 51 Airbus Defense and Space S.A. has issued Alert Operators Transmission (AOT) AOT–CN235–55–0004, Revision 1, dated October 24, 2016; and AOT AOT–C295–55–0005, Revision 1, dated October 24, 2016. This service information describes a detailed inspection of the upper and lower lugs of each horizontal stabilizer-to-fuselage rear attachment fitting (left- and righthand sides), repair if necessary, and sending inspection results to the manufacturer. These documents are distinct since they apply to different airplane models. This service information 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 our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information 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 these same type designs. Costs of Compliance We estimate that this proposed AD affects 14 airplanes of U.S. registry. We estimate the following costs to comply with this proposed AD: ESTIMATED COSTS Action Labor cost Inspection ........................................................ Reporting ......................................................... 8 work-hours × $85 per hour = $680 ............. 1 work-hour × $85 per hour = $85 ................. We estimate the following costs to do any necessary repair that would be Cost per product Parts cost required based on the results of the proposed inspection. We have no way of $0 0 Cost on U.S. operators $680 85 $9,520 1,190 determining the number of aircraft that might need this repair: ON-CONDITION COSTS Action Labor cost Repair ........................................................................... 15 work-hours × $85 per hour = $1,275 ...................... amozie on DSK3GDR082PROD with PROPOSALS1 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 NPRM is 2120–0056. The paperwork cost associated with this NPRM 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 NPRM is mandatory. Comments concerning the accuracy of this burden VerDate Sep<11>2014 17:49 May 24, 2018 Jkt 244001 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 PO 00000 Frm 00005 Fmt 4702 Sfmt 4702 Cost per product Parts cost $0 $1,275 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. E:\FR\FM\25MYP1.SGM 25MYP1 24238 Federal Register / Vol. 83, No. 102 / Friday, May 25, 2018 / Proposed Rules 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 amozie on DSK3GDR082PROD with PROPOSALS1 Accordingly, under the authority delegated to me by the Administrator, VerDate Sep<11>2014 17:49 May 24, 2018 Jkt 244001 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. [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): ■ Airbus Defense and Space S.A. (Formerly Known as Construcciones Aeronauticas, S.A.): Docket No. FAA–2018–0416; Product Identifier 2017–NM–164–AD. (a) Comments Due Date We must receive comments by July 9, 2018. (b) Affected ADs None. (c) Applicability This AD applies to Airbus Defense and Space S.A. Model airplanes, certificated in any category, specified in paragraphs (c)(1) and (c)(2) of this AD. (1) Model CN–235, CN–235–100, CN–235– 200, and CN–235–300 airplanes, all manufacturer serial numbers (MSN). (2) Model C–295 airplanes, MSN 001 through 148 inclusive. PO 00000 Frm 00006 Fmt 4702 Sfmt 4725 Air Transport Association (ATA) of America Code 55, Horizontal stabilizer. (e) Reason ■ § 39.13 (d) Subject This AD was prompted by a report that cracks were found on the stabilizer-tofuselage rear attachment fitting. We are issuing this AD to address such cracking, which could lead to reduced structural integrity of the lugs on the stabilizer-tofuselage rear attachment fittings and consequent lug or fitting failure, and could result in reduced controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Inspection Within the compliance times specified in figure 1 or figure 2 to paragraph (g) of this AD, as applicable, accomplish a detailed inspection for cracks or rework of the upper and lower lugs of each horizontal stabilizerto-fuselage rear attachment fitting (left- and right-hand sides), in accordance with the instructions of Airbus Defence and Space Alert Operators Transmission (AOT) AOT– CN235–55–0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT–C295–55–0005, Revision 1, dated October 24, 2016; as applicable. E:\FR\FM\25MYP1.SGM 25MYP1 EP25MY18.001</GPH> Regulatory Findings Federal Register / Vol. 83, No. 102 / Friday, May 25, 2018 / Proposed Rules (i) Reporting Requirement Submit a one-time report of the findings (both positive and negative) of the inspection required by paragraph (g) of this AD to Airbus Defense and Space S.A., in accordance with Airbus Defence and Space AOT AOT–CN235–55–0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT–C295–55–0005, Revision 1, dated October 24, 2016; as applicable; at the applicable time specified in paragraph (i)(1) or (i)(2) of this AD. (1) If the inspection was done on or after the effective date of this AD: Submit the report within 60 days after the inspection. (2) If the inspection was done before the effective date of this AD: Submit the report within 60 days after the effective date of this AD. (j) Parts Installation Limitations As of the effective date of this AD, no person may install, on any airplane, a horizontal stabilizer-to-fuselage rear attachment fitting, unless the part is new or it has been inspected in accordance with VerDate Sep<11>2014 17:49 May 24, 2018 Jkt 244001 instructions of Airbus Defence and Space AOT AOT–CN235–55–0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT–C295–55–0005, Revision 1, dated October 24, 2016; as applicable; and no discrepancy was found. Before installation of the horizontal stabilizer-to-fuselage rear attachment fitting, contact the Manager, International Section, Transport Standards Branch, FAA; or the EASA; or Airbus Defense and Space S.A.’s EASA DOA, for approved instructions and do those instructions accordingly. If approved by the DOA, the approval must include the DOA-authorized signature. (k) Credit for Previous Actions This paragraph provides credit for actions required by paragraphs (g), (h), and (i) of this AD, if those actions were performed before the effective date of this AD using Airbus Defence and Space AOT AOT–CN235–55– 0004, dated December 22, 2015; or Airbus Defence and Space AOT AOT–C295–55– 0005, December 22, 2015; as applicable. (l) 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 (m)(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. PO 00000 Frm 00007 Fmt 4702 Sfmt 4702 (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or the EASA; or Airbus Defense and Space S.A.’s DOA. If approved by the DOA, the approval must include the DOA-authorized signature. (3) 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. (m) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2017–0218, dated November 8, 2017, for related information. This MCAI may be found in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2018–0416. (2) For more information about this AD, contact Shahram Daneshmandi, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3220. E:\FR\FM\25MYP1.SGM 25MYP1 EP25MY18.002</GPH> amozie on DSK3GDR082PROD with PROPOSALS1 (h) Corrective Action If, during the detailed inspection required by paragraph (g) of this AD, any discrepancy (i.e., cracking or rework) is detected, as specified in Airbus Defence and Space AOT AOT–CN235–55–0004, Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT AOT–C295–55–0005, Revision 1, dated October 24, 2016; as applicable: Before further flight, contact the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or Airbus Defense and Space S.A.’s EASA Design Organization Approval (DOA), for approved repair instructions. If approved by the DOA, the approval must include the DOA-authorized signature. Accomplish the repair accordingly within the compliance time specified in those instructions, including any repetitive post-repair inspections, if applicable. 24239 24240 Federal Register / Vol. 83, No. 102 / Friday, May 25, 2018 / Proposed Rules (3) For service information identified in this AD, contact Airbus Defense and Space Services/Engineering Support, Avenida de ´ Aragon 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax +34 91 585 31 27; email MTA.TechnicalService@airbus.com. You may view this service information 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. Issued in Des Moines, Washington, on May 11, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018–11142 Filed 5–24–18; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2018–0414; Product Identifier 2017–NM–159–AD] RIN 2120–AA64 Airworthiness Directives; Airbus Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed rulemaking (NPRM). AGENCY: We propose to adopt a new airworthiness directive (AD) for all Airbus Model A300 series airplanes. This proposed AD was prompted by a revision of a certain airworthiness limitations item (ALI) document, which specifies new or more restrictive instructions and airworthiness limitations. This proposed AD would require revising the maintenance or inspection program, as applicable, to incorporate new or revised structural inspection requirements. We are proposing this AD to address the unsafe condition on these products. DATES: We must receive comments on this proposed AD by July 9, 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 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 amozie on DSK3GDR082PROD with PROPOSALS1 SUMMARY: VerDate Sep<11>2014 17:49 May 24, 2018 Jkt 244001 p.m., Monday through Friday, except Federal holidays. For service information identified in this NPRM, contact Airbus SAS, Airworthiness Office—EAW, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email account.airworth-eas@airbus.com; internet https://www.airbus.com. You may view this service information 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. 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–2018– 0414; 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: Dan Rodina, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3225. 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– 2018–0414; Product Identifier 2017– NM–159–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 https:// 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 2017–0207, dated October 12, 2017 (referred to after PO 00000 Frm 00008 Fmt 4702 Sfmt 4702 this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all Airbus Model A300 series airplanes. The MCAI states: The airworthiness limitations for the Airbus A300 aeroplanes, which are approved by EASA, are currently defined and published in the Airbus A300 Airworthiness Limitations Section (ALS) documents. The Damage Tolerant Airworthiness Limitation Items are specified in the A300 ALS Part 2. These instructions have been identified as mandatory for continuing airworthiness. Failure to accomplish these instructions could result in an unsafe condition. EASA previously issued [EASA] AD 2015– 0115 [which corresponds to FAA AD 2017– 04–05, Amendment 39–18800 (82 FR 11134, February 21, 2017) (‘‘AD 2017–04–05’’)] to require compliance with the maintenance requirements and associated airworthiness limitations defined in Airbus A300 ALS Part 2 Revision 02. Since that [EASA] AD was issued, new or more restrictive maintenance requirements and airworthiness limitations were approved by EASA. Consequently, Airbus published Revision 03 of the A300 ALS Part 2, compiling all ALS Part 2 changes approved since previous Revision 02. For the reason described above, this [EASA] AD retains the requirements of EASA AD 2015–0115, which is superseded, and requires accomplishment of the actions specified in Airbus A300 ALS Part 2 Revision 03. You may examine the MCAI in the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2018– 0414. Relationship Between Proposed AD and AD 2017–04–05 This NPRM would not supersede AD 2017–04–05. Rather, we have determined that a stand-alone AD would be more appropriate to address the changes in the MCAI. This NPRM would require revising the maintenance or inspection program, as applicable, to incorporate new or revised structural inspection requirements. Accomplishment of the proposed actions would then terminate all of the requirements of AD 2017–04–05. Related Service Information Under 1 CFR Part 51 Airbus has issued A300 Airworthiness Limitations Section (ALS), Part 2—Damage Tolerant Airworthiness Limitation Items (DT– ALI), Revision 03, dated August 28, 2017. The service information describes airworthiness limitations applicable to the DT–ALI. This service information is reasonably available because the interested parties have access to it through their normal course of business E:\FR\FM\25MYP1.SGM 25MYP1

Agencies

[Federal Register Volume 83, Number 102 (Friday, May 25, 2018)]
[Proposed Rules]
[Pages 24236-24240]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-11142]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0416; Product Identifier 2017-NM-164-AD]
RIN 2120-AA64


Airworthiness Directives; Airbus Defense and Space S.A. (Formerly 
Known as Construcciones Aeronauticas, S.A.) Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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

SUMMARY: We propose to adopt a new airworthiness directive (AD) for all 
Airbus Defense and Space S.A. Model CN-235, CN-235-100, CN-235-200, and 
CN-235-300 airplanes; and certain Model C-295 airplanes. This proposed 
AD was prompted by a report that cracks were found on the stabilizer-
to-fuselage rear attachment fitting. This proposed AD would require a 
detailed inspection of the upper and lower lugs of each horizontal 
stabilizer-to-fuselage rear attachment fitting, repair if necessary, 
and a report of findings. We are proposing this AD to address the 
unsafe condition on these products.

DATES: We must receive comments on this proposed AD by July 9, 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 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 service information identified in this NPRM, contact Airbus 
Defense and Space Services/Engineering Support, Avenida de 
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; fax 
+34 91 585 31 27; email [email protected]. You may view 
this service information 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.

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-2018-
0416; 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: Shahram Daneshmandi, Aerospace 
Engineer, International Section, Transport Standards Branch, FAA, 2200 
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3220.

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-2018-0416; 
Product Identifier 2017-NM-164-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 https://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 
2017-0218, dated November 8, 2017 (referred to after this as the 
Mandatory Continuing Airworthiness Information, or ``the MCAI''), to 
correct an unsafe condition for all Airbus Defense and Space S.A. Model 
CN-235, CN-235-100, CN-235-200, and CN-235-300 airplanes; and

[[Page 24237]]

certain Model C-295 airplanes. The MCAI states:

    Cracks were reportedly found on the stabilizer-to-fuselage rear 
attachment fitting of a CN-235 aeroplane. Subsequent investigation 
determined that the affected horizontal attachment fitting was a 
reworked part.
    This condition, if not detected and corrected, could lead to 
reduced structural integrity of lugs of the stabilizer-to-fuselage 
rear attachment fittings and consequent lug or fitting failure, 
possibly resulting in reduced control of the aeroplane.
    To address this potentially unsafe condition, Airbus Defence and 
Space (D&S) issued Alert Operators Transmission (AOT) AOT-C295-55-
0005 and AOT-CN235-55-0004 to provide inspection instructions.
    For the reasons described above, this [EASA] AD requires a one-
time detailed inspection (DET) of the upper and lower lugs of the 
horizontal stabilizer-to-fuselage rear attachment fittings on the 
left hand (LH) and right hand (RH) sides and, depending on findings, 
accomplishment of applicable corrective action(s) [repairs]. This 
[EASA] AD also requires reporting of all findings, including none.

    You may examine the MCAI in the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0416.

Related Service Information Under 1 CFR Part 51

    Airbus Defense and Space S.A. has issued Alert Operators 
Transmission (AOT) AOT-CN235-55-0004, Revision 1, dated October 24, 
2016; and AOT AOT-C295-55-0005, Revision 1, dated October 24, 2016. 
This service information describes a detailed inspection of the upper 
and lower lugs of each horizontal stabilizer-to-fuselage rear 
attachment fitting (left- and right-hand sides), repair if necessary, 
and sending inspection results to the manufacturer. These documents are 
distinct since they apply to different airplane models. This service 
information 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 our bilateral agreement with the State of Design Authority, we have 
been notified of the unsafe condition described in the MCAI and service 
information 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 these 
same type designs.

Costs of Compliance

    We estimate that this proposed AD affects 14 airplanes of U.S. 
registry.
    We estimate the following costs to comply with this proposed AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                     Cost per      Cost on U.S.
                Action                         Labor cost           Parts cost        product        operators
----------------------------------------------------------------------------------------------------------------
Inspection............................  8 work-hours x $85 per                $0            $680          $9,520
                                         hour = $680.
Reporting.............................  1 work-hour x $85 per                  0              85           1,190
                                         hour = $85.
----------------------------------------------------------------------------------------------------------------

    We estimate the following costs to do any necessary repair that 
would be required based on the results of the proposed inspection. We 
have no way of determining the number of aircraft that might need this 
repair:

                                               On-Condition Costs
----------------------------------------------------------------------------------------------------------------
                                                                                                     Cost per
                   Action                                 Labor cost                Parts cost        product
----------------------------------------------------------------------------------------------------------------
Repair.....................................  15 work-hours x $85 per hour =                   $0          $1,275
                                              $1,275.
----------------------------------------------------------------------------------------------------------------

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 NPRM is 2120-
0056. The paperwork cost associated with this NPRM 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 NPRM 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 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.

[[Page 24238]]

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 Defense and Space S.A. (Formerly Known as Construcciones 
Aeronauticas, S.A.): Docket No. FAA-2018-0416; Product Identifier 
2017-NM-164-AD.

(a) Comments Due Date

    We must receive comments by July 9, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Airbus Defense and Space S.A. Model 
airplanes, certificated in any category, specified in paragraphs 
(c)(1) and (c)(2) of this AD.
    (1) Model CN-235, CN-235-100, CN-235-200, and CN-235-300 
airplanes, all manufacturer serial numbers (MSN).
    (2) Model C-295 airplanes, MSN 001 through 148 inclusive.

(d) Subject

    Air Transport Association (ATA) of America Code 55, Horizontal 
stabilizer.

(e) Reason

    This AD was prompted by a report that cracks were found on the 
stabilizer-to-fuselage rear attachment fitting. We are issuing this 
AD to address such cracking, which could lead to reduced structural 
integrity of the lugs on the stabilizer-to-fuselage rear attachment 
fittings and consequent lug or fitting failure, and could result in 
reduced controllability of the airplane.

(f) Compliance

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

(g) Inspection

    Within the compliance times specified in figure 1 or figure 2 to 
paragraph (g) of this AD, as applicable, accomplish a detailed 
inspection for cracks or rework of the upper and lower lugs of each 
horizontal stabilizer-to-fuselage rear attachment fitting (left- and 
right-hand sides), in accordance with the instructions of Airbus 
Defence and Space Alert Operators Transmission (AOT) AOT-CN235-55-
0004, Revision 1, dated October 24, 2016; or Airbus Defence and 
Space AOT AOT-C295-55-0005, Revision 1, dated October 24, 2016; as 
applicable.
[GRAPHIC] [TIFF OMITTED] TP25MY18.001


[[Page 24239]]


[GRAPHIC] [TIFF OMITTED] TP25MY18.002

(h) Corrective Action

    If, during the detailed inspection required by paragraph (g) of 
this AD, any discrepancy (i.e., cracking or rework) is detected, as 
specified in Airbus Defence and Space AOT AOT-CN235-55-0004, 
Revision 1, dated October 24, 2016; or Airbus Defence and Space AOT 
AOT-C295-55-0005, Revision 1, dated October 24, 2016; as applicable: 
Before further flight, contact the Manager, International Section, 
Transport Standards Branch, FAA; or the European Aviation Safety 
Agency (EASA); or Airbus Defense and Space S.A.'s EASA Design 
Organization Approval (DOA), for approved repair instructions. If 
approved by the DOA, the approval must include the DOA-authorized 
signature. Accomplish the repair accordingly within the compliance 
time specified in those instructions, including any repetitive post-
repair inspections, if applicable.

(i) Reporting Requirement

    Submit a one-time report of the findings (both positive and 
negative) of the inspection required by paragraph (g) of this AD to 
Airbus Defense and Space S.A., in accordance with Airbus Defence and 
Space AOT AOT-CN235-55-0004, Revision 1, dated October 24, 2016; or 
Airbus Defence and Space AOT AOT-C295-55-0005, Revision 1, dated 
October 24, 2016; as applicable; at the applicable time specified in 
paragraph (i)(1) or (i)(2) of this AD.
    (1) If the inspection was done on or after the effective date of 
this AD: Submit the report within 60 days after the inspection.
    (2) If the inspection was done before the effective date of this 
AD: Submit the report within 60 days after the effective date of 
this AD.

(j) Parts Installation Limitations

    As of the effective date of this AD, no person may install, on 
any airplane, a horizontal stabilizer-to-fuselage rear attachment 
fitting, unless the part is new or it has been inspected in 
accordance with instructions of Airbus Defence and Space AOT AOT-
CN235-55-0004, Revision 1, dated October 24, 2016; or Airbus Defence 
and Space AOT AOT-C295-55-0005, Revision 1, dated October 24, 2016; 
as applicable; and no discrepancy was found. Before installation of 
the horizontal stabilizer-to-fuselage rear attachment fitting, 
contact the Manager, International Section, Transport Standards 
Branch, FAA; or the EASA; or Airbus Defense and Space S.A.'s EASA 
DOA, for approved instructions and do those instructions 
accordingly. If approved by the DOA, the approval must include the 
DOA-authorized signature.

(k) Credit for Previous Actions

    This paragraph provides credit for actions required by 
paragraphs (g), (h), and (i) of this AD, if those actions were 
performed before the effective date of this AD using Airbus Defence 
and Space AOT AOT-CN235-55-0004, dated December 22, 2015; or Airbus 
Defence and Space AOT AOT-C295-55-0005, December 22, 2015; as 
applicable.

(l) 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 (m)(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 corrective actions from a manufacturer, the action must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, FAA; or the EASA; or Airbus 
Defense and Space S.A.'s DOA. If approved by the DOA, the approval 
must include the DOA-authorized signature.
    (3) 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.

(m) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA AD 2017-0218, dated November 8, 2017, for related 
information. This MCAI may be found in the AD docket on the internet 
at https://www.regulations.gov by searching for and locating Docket 
No. FAA-2018-0416.
    (2) For more information about this AD, contact Shahram 
Daneshmandi, Aerospace Engineer, International Section, Transport 
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; 
telephone and fax 206-231-3220.

[[Page 24240]]

    (3) For service information identified in this AD, contact 
Airbus Defense and Space Services/Engineering Support, Avenida de 
Arag[oacute]n 404, 28022 Madrid, Spain; telephone +34 91 585 55 84; 
fax +34 91 585 31 27; email [email protected]. You may 
view this service information 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.

    Issued in Des Moines, Washington, on May 11, 2018.
Michael Kaszycki,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-11142 Filed 5-24-18; 8:45 am]
 BILLING CODE 4910-13-P
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