83 FR 45539 - Airworthiness Directives; Airbus SAS Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 175 (September 10, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 175 (September 10, 2018)
| Page Range | 45539-45545 | |
| FR Document | 2018-18907 |
[Federal Register Volume 83, Number 175 (Monday, September 10, 2018)] [Rules and Regulations] [Pages 45539-45545] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-18907] ======================================================================= ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0454; Product Identifier 2017-NM-056-AD; Amendment 39-19387; AD 2018-18-08] RIN 2120-AA64 Airworthiness Directives; Airbus SAS Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for all Airbus SAS Model A330-200 Freighter series airplanes, Model A330-200 and -300 series airplanes, and Model A340-200 and -300 series airplanes. This AD was prompted by reports of cracked slat tracks at the location of the front stop attachment to the track. This AD requires a detailed inspection, repetitive special detailed inspections, and corrective actions if necessary. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective October 15, 2018. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of October 15, 2018. ADDRESSES: For service information identified in this final rule, contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; phone: +33 5 61 93 36 96; fax: +33 5 61 93 45 80; email: [email protected]; internet: http://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. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0454. 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- 0454; or in person at Docket Operations between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this final rule, the regulatory evaluation, any comments received, and other [[Page 45540]] information. The address for Docket Operations (phone: 800-647-5527) is in the ADDRESSES section. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3229. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to all Airbus SAS Model A330- 200 Freighter series airplanes, Model A330-200 and -300 series airplanes, and Model A340-200 and -300 series airplanes. The NPRM published in the Federal Register on May 29, 2018 (83 FR 24427). The NPRM was prompted by reports of cracked slat tracks at the location of the front stop attachment to the track. The NPRM proposed to require a detailed inspection, repetitive special detailed inspections, and corrective actions if necessary. We are issuing this AD to address cracked slat tracks which could affect the structural integrity of the slat surface, possibly leading to detachment of an outer or inner slat surface, and resulting in reduced control of the airplane. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2017-0060, dated April 7, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for all Airbus SAS Model A330-200 Freighter series airplanes; Model A330-200 and -300 series airplanes; and Model A340-200 and -300 series airplanes. The MCAI states: Several cases of cracked slat tracks at the location of front stop attachment to track have been reported by operators. Analysis of the affected slat tracks (Airbus pre-modification (mod) 45967 design) revealed that induced torque loads during normal installation of the front stop, in combination with an incorrect shaft length of the attachment bolts and geometry of the front stop, are the root cause. This condition, if not detected and corrected, would affect the structural integrity of the slat surface, which could lead to detachment of an outer or inner slat surface, possibly resulting in reduced control of the aeroplane and/or injury to persons on the ground. To address this potential unsafe condition, Airbus issued Service Bulletin (SB) A330-57-3123 and SB A340-57-4130, to provide inspection instructions. For the reasons described above, this [EASA] AD requires a one- time detailed inspection (DET) of the front stop lateral and aft surfaces [for marks (dents or scratches),] and repetitive special detailed inspections (SDI) of the front stop attachment areas, of slat tracks number (No.) 5 to No. 16 inclusive, both left hand (LH) and right hand (RH) wings [for cracks], and, depending on findings, accomplishment of applicable corrective action(s) [corrective actions include rework, repair, and slat rigging]. This [EASA] AD also includes reference to an optional modification (Airbus mod 205378) of the affected slat tracks, for which the associated SBs (SB A330-57-3126 and SB A340-57-4133, as applicable) are expected to become available in July 2017, which constitutes terminating action for the repetitive inspections required by this [EASA] AD. You may examine the MCAI in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0454. Comments We gave the public the opportunity to participate in developing this final rule. We received no comments on the NPRM or on the determination of the cost to the public. Conclusion We reviewed the relevant data and determined that air safety and the public interest require adopting this final rule as proposed, except for minor editorial changes. We have determined that these minor changes:Are consistent with the intent that was proposed in the NPRM for addressing the unsafe condition; and Do not add any additional burden upon the public than was already proposed in the NPRM. Related Service Information Under 1 CFR Part 51 Airbus has issued Service Bulletin A330-57-3123, Revision 01, dated September 27, 2017; and Service Bulletin A340-57-4130, Revision 01, dated September 27, 2017. This service information describes procedures for a detailed inspection of the front stop lateral and aft surfaces for marks (dents or scratches), repetitive special detailed inspections of the front stop attachment areas, of slat track numbers 5 to 16 inclusive, both LH and RH wings for cracks, and corrective actions. These documents are distinct since they apply to different airplane models. Airbus has also issued Service Bulletin A330-57-3126, dated December 21, 2017; and Service Bulletin A340-57-4133, dated December 21, 2017. This service information describes procedures for modification of all affected slat tracks on an airplane. 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. Costs of Compliance We estimate that this AD affects 101 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost on U.S. Action Labor cost Parts cost Cost per product operators ---------------------------------------------------------------------------------------------------------------- Detailed Inspection............ 25 work-hours x $85 per $0 $2,125............ $214,625. hour = $2,125. Special Detailed Inspection.... 25 work-hours x $85 per 0 $2,125 per $214,625 per hour = $2,125 per inspection cycle. inspection cycle. inspection cycle. Reporting...................... 1 work-hour x $85 per 0 $85 per inspection $8,585 per hour = $85 per cycle. inspection cycle. inspection cycle. Modification................... 49 work-hours x $85 per 8,150 $12,315........... $1,243,815. hour = $4,165. ---------------------------------------------------------------------------------------------------------------- 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 [[Page 45541]] 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 and associated appliances to the Director of the System Oversight Division. Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) 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. 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): 2018-18-08 Airbus SAS: Amendment 39-19387; Docket No. FAA-2018-0454; Product Identifier 2017-NM-056-AD. (a) Effective Date This AD is effective October 15, 2018. (b) Affected ADs None. (c) Applicability This AD applies to the airplanes identified in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), and (c)(5) of this AD, certificated in any category, all manufacturer serial numbers. (1) Airbus SAS Model A330-223F and -243F airplanes. (2) Airbus SAS Model A330-201, -202, -203, -223, and -243 airplanes. (3) Airbus SAS Model A330-301, -302, -303, -321, -322, -323, - 341, -342, and -343 airplanes. (4) Airbus SAS Model A340-211, -212, -213 airplanes. (5) Airbus SAS Model A340-311, -312, and -313 airplanes. (d) Subject Air Transport Association (ATA) of America Code 57, Wings. (e) Reason This AD was prompted by reports of cracked slat tracks at the location of the front stop attachment to the track. We are issuing this AD to detect and correct cracked slat tracks which could affect the structural integrity of the slat surface, possibly leading to detachment of an outer or inner slat surface, and resulting in reduced control of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Definitions (1) For the purpose of this AD, ``affected slat track'' is defined as a pre-modification 45967 slat track, located at the wing positions as indicated in figure 1 to paragraph (g) of this AD, and having a part number specified in figure 2 to paragraph (g) of this AD. In case the part number identification (ID) plate is missing or cannot be read, the slat track can be identified by the ink marking. If the operator cannot determine the part number, then that airplane is in Group 1. (2) For the purpose of this AD: Group 1 airplanes are those that, on the effective date of this AD, have an affected slat track installed. Group 2 airplanes are those that, on the effective date of this AD, do not have any affected slat track installed. BILLINGCODE 4910-13-P [[Page 45542]] [GRAPHIC] [TIFF OMITTED] TR10SE18.000 [[Page 45543]] [GRAPHIC] [TIFF OMITTED] TR10SE18.001 [[Page 45544]] (h) One-Time Detailed Inspection and Repetitive Special Detailed Inspections For Group 1 airplanes: At the applicable times specified in figure 3 to paragraph (h) of this AD, do a detailed inspection of the front stop lateral and aft surfaces, and do a special detailed inspection of the front stop attachment areas of each affected slat track, both right hand (RH) and left hand (LH) wings, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-57-3123, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; or Airbus Service Bulletin A340-57-4130, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; as applicable. Thereafter, repeat the special detailed inspection for the front stop attachment areas of each affected slat track, both RH and LH wings, at intervals not to exceed the applicable compliance times specified in figure 4 to paragraph (h) of this AD. [GRAPHIC] [TIFF OMITTED] TR10SE18.002 [GRAPHIC] [TIFF OMITTED] TR10SE18.003 BILLINGCODE 4910-13-C (i) Corrective Actions (1) If, during any special detailed inspection required by paragraph (h) of this AD, any crack is detected at the front stop attachment area of an affected slat track: Before further flight, obtain corrective action instructions approved by the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or Airbus SAS's EASA Design Organization Approval (DOA), and accomplish them within the compliance time specified therein. If approved by the DOA, the approval must include the DOA-authorized signature. (2) If, during any inspection required by paragraph (h) of this AD, marks (dents or scratches) are found on the front stop lateral or aft surfaces of an affected slat track; provided that no crack is detected; before further flight, rework the affected lateral front stop surface of that slat track, and accomplish slat rigging, as applicable, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-57-3123, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; or Airbus Service Bulletin A340-57-4130, Revision 01, including Appendixes 02 and 03, dated September 27, 2017. Accomplishment of rework or slat rigging on an airplane, as required by this paragraph, does not constitute terminating action for the repetitive special detailed inspection required by paragraph (h) of this AD. (3) If, during any inspection required by paragraph (h) of this AD, marks (dents or scratches) are found on the front stop lateral or aft surfaces of an affected slat track, and any crack is detected at the front stop attachment area of that slat track: Before further flight, obtain corrective action instructions approved by the Manager, International Section, Transport Standards Branch, FAA; or EASA; or Airbus SAS's EASA DOA, and accomplish them within the compliance time specified therein. If approved by the DOA, the approval must include the DOA-authorized signature. (j) Reporting At the applicable time specified in paragraph (j)(1) or (j)(2) of this AD: Report the results of the inspections required by paragraph (h) of this AD to Airbus Service Bulletin Reporting Online Application on Airbus World (https://w3.airbus.com/), or submit the results to Airbus in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-57-3123, Revision 01, including Appendixes 02 and 03, dated September 27, 2017, or Airbus Service Bulletin A340-57-4130, Revision 01, including Appendixes 02 and 03, dated September 27, 2017. The report must include the inspection results (including no findings), a description of any discrepancies found, the airplane serial number, and the number of landings and flight hours on the airplane. (1) If the inspection was done on or after the effective date of this AD: Submit the report within 60 days after each inspection required by paragraph (h) of this AD. (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. (k) Optional Terminating Actions (1) Replacement of an affected slat track at any position with a post-modification 45967 slat track, if accomplished as part of the corrective actions specified in paragraph (i)(1) or (i)(3) of this AD, terminates the repetitive inspections required by paragraph (h) of this AD, for that slat track position. [[Page 45545]] (2) Modification of all affected slat tracks on an airplane in accordance with the Accomplishment Instructions of Airbus Service Bulletin A330-57-3126, including Appendixes 02 and 03, dated December 21, 2017; or Airbus Service Bulletin A340-57-4133, including Appendixes 02 and 03, dated December 21, 2017; as applicable, terminates the repetitive inspections required by paragraph (h) of this AD for that airplane, provided that, prior to modification, the affected slat tracks pass an inspection (crack free) in accordance with the instructions of Airbus Service Bulletin A330-57-3123, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; or Airbus Service Bulletin A340-57-4130, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; as applicable. (l) Parts Installation Limitations (1) Except as specified in paragraph (l)(2) of this AD: For Group 1 airplanes, after the effective date of this AD, an affected slat track may be installed, provided the installation is accomplished using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or EASA; or Airbus SAS's EASA DOA. If approved by the DOA, the approval must include the DOA- authorized signature. (2) After modification of a Group 1 airplane as specified in paragraph (k)(2) of this AD, no person may install an affected slat track on that airplane. (3) For Group 2 airplanes: As of the effective date of this AD, no person may install an affected slat track on any Group 2 airplane. (m) Credit for Previous Actions This paragraph provides credit for actions required by paragraphs (h), (i), and (j) of this AD, if those actions were performed before the effective date of this AD using Airbus Service Bulletin A330-57-3123, dated June 14, 2016; or Airbus Service Bulletin A340-57-4130, dated June 14, 2016, provided that within 12 months after the effective date of this AD, the additional work identified in Airbus Service Bulletin A330-57-3123, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; or Airbus Service Bulletin A340-57-4130, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; as applicable, has been completed in accordance with Airbus Service Bulletin A330-57-3123, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; or Airbus Service Bulletin A340-57-4130, Revision 01, including Appendixes 02 and 03, dated September 27, 2017; as applicable. (n) 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 Branch, send it to the attention of the person identified in paragraph (o)(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 EASA; or Airbus SAS's EASA 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 work-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. (4) Required for Compliance (RC): Except as required by paragraph (i) of this AD: If any service information contains procedures or tests that are identified as RC, those procedures and tests must be done to comply with this AD; any procedures or tests that are not identified as RC are recommended. Those procedures and tests that are not identified as RC may be deviated from using accepted methods in accordance with the operator's maintenance or inspection program without obtaining approval of an AMOC, provided the procedures and tests identified as RC can be done and the airplane can be put back in an airworthy condition. Any substitutions or changes to procedures or tests identified as RC require approval of an AMOC. (o) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2017-0060, dated April 7, 2017, for related information. This MCAI may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0454. (2) For more information about this AD, contact Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax 206 231 3229. (3) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (p)(3) and (p)(4) of this AD. (p) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Airbus Service Bulletin A330-57-3123, Revision 01, dated September 27, 2017. (ii) Airbus Service Bulletin A330-57-3126, dated December 21, 2017. (iii) Airbus Service Bulletin A340-57-4130, Revision 01, dated September 27, 2017. (iv) Airbus Service Bulletin A340-57-4133, dated December 21, 2017. (3) For service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile Dewoitine No: 2, 31700Blagnac Cedex, France; phone: +33 5 61 93 36 96; fax: +33 5 61 93 45 80; email: [email protected]; internet http://www.airbus.com. (4) 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. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Des Moines, Washington, on August 22, 2018. James Cashdollar, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-18907 Filed 9-7-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 175 / Monday, September 10, 2018 / Rules and Regulations 45539
contract at any time during the crop corporate resolution due to an insured DEPARTMENT OF TRANSPORTATION
year; and peril will be converted to pounds of raw
* * * * * sugar by multiplying the tons of such Federal Aviation Administration
(b) * * * damaged production by 2,000 and by
(2) The Board of Directors or officers the average percent of raw sugar 14 CFR Part 39
of the processor must have adopted and contained in such production. [Docket No. FAA–2018–0454; Product
executed a corporate resolution that (1) If individual tests of raw sugar Identifier 2017–NM–056–AD; Amendment
contains essentially the same terms as a content are not made at the time of 39–19387; AD 2018–18–08]
processor contract. Such corporate delivery, the average percent of raw RIN 2120–AA64
resolution will be considered a
sugar may be based on the results of
processor contract under the terms of Airworthiness Directives; Airbus SAS
previous tests performed by the
the sugar beet crop insurance policy; Airplanes
processor during the crop year if it is
* * * * * determined that such results are
9. Insurance Period AGENCY: Federal Aviation
representative of the total production. Administration (FAA), Department of
In accordance with section 11 of the
Basic Provisions, the dates for the end (2) If not representative, the average Transportation (DOT).
of insurance period are contained in the percent of raw sugar will equal the raw ACTION: Final rule.
actuarial documents. sugar content percent shown in the
Special Provisions. SUMMARY: We are adopting a new
* * * * * airworthiness directive (AD) for all
11. Replanting Payments (f) Production lost due to harvest prior Airbus SAS Model A330–200 Freighter
* * * * * to full maturity. If the percentage of series airplanes, Model A330–200 and
(b) The dollar amount of the replant insured acreage in the unit harvested –300 series airplanes, and Model A340–
payment is specified in the Special prior to full maturity exceeds the 200 and –300 series airplanes. This AD
Provisions. threshold specified in the actuarial was prompted by reports of cracked slat
* * * * * documents, production to count from tracks at the location of the front stop
12. Duties in the Event of Damage or such acreage will be determined by attachment to the track. This AD
Loss increasing the amount of harvested requires a detailed inspection, repetitive
* * * * * production by 1 percent per day for special detailed inspections, and
(b) You must provide a copy of your each day the sugar beets were harvested corrective actions if necessary. We are
processor contract, or corporate prior to the date the sugar beets would issuing this AD to address the unsafe
resolution if you are the processor. have reached full maturity. condition on these products.
13. Settlement of Claim (1) The date the sugar beets would DATES: This AD is effective October 15,
* * * * * have reached full maturity will be 2018.
(d) Harvested production or considered to be 45 days prior to the The Director of the Federal Register
unharvested production that is calendar date for the end of the approved the incorporation by reference
appraised after the earliest delivery date insurance period, unless otherwise of certain publications listed in this AD
that the processor accepts harvested specified in the Special Provisions. as of October 15, 2018.
production and that meets the minimum ADDRESSES: For service information
acceptable standards contained in the (2) This adjustment will not be made
identified in this final rule, contact
processor contract or corporate if the sugar beets are damaged by an Airbus SAS, Airworthiness Office—
resolution will be converted to pounds insurable cause of loss and leaving the EAL, Rond-Point Emile Dewoitine No:
of raw sugar by multiplying the tons of crop in the field would reduce 2, 31700 Blagnac Cedex, France; phone:
such production by 2,000 and by the production. +33 5 61 93 36 96; fax: +33 5 61 93 45
average percentage of raw sugar to (3) The adjustment cannot result in 80; email: airworthiness.A330-A340@
determine the production to count. The production to count in excess of the airbus.com; internet: http://
average percentage of raw sugar will be insured’s actual production history; www.airbus.com. You may view this
determined from tests performed by the service information at the FAA,
* * * * *
processor at the time of delivery. Transport Standards Branch, 2200
(1) If individual tests of raw sugar 15. Prevented Planting South 216th St., Des Moines, WA. For
content are not made at the time of Your prevented planting coverage will information on the availability of this
delivery, the average percent of raw be a percentage specified in the material at the FAA, call 206–231–3195.
sugar may be based on the results of actuarial documents of your production It is also available on the internet at
previous tests performed by the guarantee for timely planted acreage. If http://www.regulations.gov by searching
processor during the crop year if it is you have additional levels of coverage for and locating Docket No. FAA–2018–
determined that such results are and pay an additional premium, you 0454.
representative of the total production. may increase your prevented planting
(2) If not representative, the average Examining the AD Docket
coverage if such additional coverage is
percent of raw sugar will equal the raw specified in the actuarial documents. You may examine the AD docket on
sugar content percent shown in the the internet at http://
Special Provisions. Martin R. Barbre, www.regulations.gov by searching for
(e) Harvested production or and locating Docket No. FAA–2018–
daltland on DSKBBV9HB2PROD with RULES
Manager, Federal Crop Insurance
unharvested production that is Corporation. 0454; or in person at Docket Operations
appraised after the earliest delivery date [FR Doc. 2018–19152 Filed 9–7–18; 8:45 am] between 9 a.m. and 5 p.m., Monday
that the processor accepts harvested BILLING CODE 3410–08–P
through Friday, except Federal holidays.
production and that does not meet the The AD docket contains this final rule,
minimum acceptable standards the regulatory evaluation, any
contained in the processor contract or comments received, and other
VerDate Sep<11>2014 16:01 Sep 07, 2018 Jkt 244001 PO 00000 Frm 00005 Fmt 4700 Sfmt 4700 E:\FR\FM\10SER1.SGM 10SER1](https://thefederalregister.org/doc/83_FR_45714/page/1.svg)
![45540 Federal Register / Vol. 83, No. 175 / Monday, September 10, 2018 / Rules and Regulations
information. The address for Docket the affected slat tracks (Airbus pre- public interest require adopting this
Operations (phone: 800–647–5527) is in modification (mod) 45967 design) revealed final rule as proposed, except for minor
the ADDRESSES section. that induced torque loads during normal editorial changes. We have determined
installation of the front stop, in combination
FOR FURTHER INFORMATION CONTACT: with an incorrect shaft length of the that these minor changes:
Vladimir Ulyanov, Aerospace Engineer, attachment bolts and geometry of the front • Are consistent with the intent that
International Section, Transport stop, are the root cause. was proposed in the NPRM for
Standards Branch, FAA, 2200 South This condition, if not detected and addressing the unsafe condition; and
216th St., Des Moines, WA 98198; corrected, would affect the structural
phone and fax: 206–231–3229. integrity of the slat surface, which could lead • Do not add any additional burden
to detachment of an outer or inner slat upon the public than was already
SUPPLEMENTARY INFORMATION:
surface, possibly resulting in reduced control proposed in the NPRM.
Discussion of the aeroplane and/or injury to persons on
the ground. Related Service Information Under 1
We issued a notice of proposed To address this potential unsafe condition, CFR Part 51
rulemaking (NPRM) to amend 14 CFR Airbus issued Service Bulletin (SB) A330–
part 39 by adding an AD that would 57–3123 and SB A340–57–4130, to provide Airbus has issued Service Bulletin
apply to all Airbus SAS Model A330– inspection instructions. A330–57–3123, Revision 01, dated
200 Freighter series airplanes, Model For the reasons described above, this September 27, 2017; and Service
A330–200 and –300 series airplanes, [EASA] AD requires a one-time detailed Bulletin A340–57–4130, Revision 01,
and Model A340–200 and –300 series inspection (DET) of the front stop lateral and
aft surfaces [for marks (dents or scratches),]
dated September 27, 2017. This service
airplanes. The NPRM published in the information describes procedures for a
and repetitive special detailed inspections
Federal Register on May 29, 2018 (83 (SDI) of the front stop attachment areas, of detailed inspection of the front stop
FR 24427). The NPRM was prompted by slat tracks number (No.) 5 to No. 16 lateral and aft surfaces for marks (dents
reports of cracked slat tracks at the inclusive, both left hand (LH) and right hand or scratches), repetitive special detailed
location of the front stop attachment to (RH) wings [for cracks], and, depending on inspections of the front stop attachment
the track. The NPRM proposed to findings, accomplishment of applicable areas, of slat track numbers 5 to 16
require a detailed inspection, repetitive corrective action(s) [corrective actions
inclusive, both LH and RH wings for
special detailed inspections, and include rework, repair, and slat rigging].
This [EASA] AD also includes reference to cracks, and corrective actions. These
corrective actions if necessary. documents are distinct since they apply
We are issuing this AD to address an optional modification (Airbus mod
205378) of the affected slat tracks, for which to different airplane models.
cracked slat tracks which could affect the associated SBs (SB A330–57–3126 and
the structural integrity of the slat Airbus has also issued Service
SB A340–57–4133, as applicable) are
surface, possibly leading to detachment Bulletin A330–57–3126, dated
expected to become available in July 2017,
of an outer or inner slat surface, and which constitutes terminating action for the December 21, 2017; and Service Bulletin
resulting in reduced control of the repetitive inspections required by this A340–57–4133, dated December 21,
airplane. [EASA] AD. 2017. This service information describes
The European Aviation Safety Agency You may examine the MCAI in the procedures for modification of all
(EASA), which is the Technical Agent AD docket on the internet at http:// affected slat tracks on an airplane. These
for the Member States of the European www.regulations.gov by searching for documents are distinct since they apply
Union, has issued EASA AD 2017–0060, and locating Docket No. FAA–2018– to different airplane models.
dated April 7, 2017 (referred to after this 0454. This service information is reasonably
as the Mandatory Continuing available because the interested parties
Airworthiness Information, or ‘‘the Comments
have access to it through their normal
MCAI’’), to correct an unsafe condition We gave the public the opportunity to course of business or by the means
for all Airbus SAS Model A330–200 participate in developing this final rule. identified in the ADDRESSES section.
Freighter series airplanes; Model A330– We received no comments on the NPRM
200 and –300 series airplanes; and or on the determination of the cost to Costs of Compliance
Model A340–200 and –300 series the public.
airplanes. The MCAI states: We estimate that this AD affects 101
Conclusion airplanes of U.S. registry.
Several cases of cracked slat tracks at the
location of front stop attachment to track We reviewed the relevant data and We estimate the following costs to
have been reported by operators. Analysis of determined that air safety and the comply with this AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Detailed Inspection ........ 25 work-hours × $85 per hour = $2,125 ............ $0 $2,125 .......................... $214,625.
Special Detailed Inspec- 25 work-hours × $85 per hour = $2,125 per in- 0 $2,125 per inspection $214,625 per inspection
tion. spection cycle. cycle. cycle.
Reporting ....................... 1 work-hour × $85 per hour = $85 per inspec- 0 $85 per inspection $8,585 per inspection
tion cycle. cycle. cycle.
Modification ................... 49 work-hours × $85 per hour = $4,165 ............ 8,150 $12,315 ........................ $1,243,815.
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We have received no definitive data Paperwork Reduction Act to penalty for failure to comply with a
that would enable us to provide cost collection of information subject to the
A federal agency may not conduct or
estimates for the on-condition actions requirements of the Paperwork
sponsor, and a person is not required to
specified in this AD. Reduction Act unless that collection of
respond to, nor shall a person be subject
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![Federal Register / Vol. 83, No. 175 / Monday, September 10, 2018 / Rules and Regulations 45541
information displays a current valid the Director of the System Oversight (b) Affected ADs
OMB control number. The control Division. None.
number for the collection of information
Regulatory Findings (c) Applicability
required by this AD is 2120–0056. The
paperwork cost associated with this AD This AD will not have federalism This AD applies to the airplanes identified
has been detailed in the Costs of implications under Executive Order in paragraphs (c)(1), (c)(2), (c)(3), (c)(4), and
Compliance section of this document 13132. This AD will not have a (c)(5) of this AD, certificated in any category,
and includes time for reviewing substantial direct effect on the States, on all manufacturer serial numbers.
the relationship between the national (1) Airbus SAS Model A330–223F and
instructions, as well as completing and
government and the States, or on the –243F airplanes.
reviewing the collection of information.
distribution of power and (2) Airbus SAS Model A330–201, –202,
Therefore, all reporting associated with –203, –223, and –243 airplanes.
this AD is mandatory. Comments responsibilities among the various
levels of government. (3) Airbus SAS Model A330–301, –302,
concerning the accuracy of this burden –303, –321, –322, –323, –341, –342, and –343
and suggestions for reducing the burden For the reasons discussed above, I
certify that this AD: airplanes.
should be directed to the FAA at 800 (4) Airbus SAS Model A340–211, –212,
(1) Is not a ‘‘significant regulatory
Independence Ave. SW, Washington, –213 airplanes.
action’’ under Executive Order 12866,
DC 20591, ATTN: Information (2) Is not a ‘‘significant rule’’ under (5) Airbus SAS Model A340–311, –312,
Collection Clearance Officer, AES–200. the DOT Regulatory Policies and
and –313 airplanes.
Authority for This Rulemaking Procedures (44 FR 11034, February 26, (d) Subject
1979), Air Transport Association (ATA) of
Title 49 of the United States Code (3) Will not affect intrastate aviation
specifies the FAA’s authority to issue America Code 57, Wings.
in Alaska, and
rules on aviation safety. Subtitle I, (4) Will not have a significant (e) Reason
section 106, describes the authority of economic impact, positive or negative, This AD was prompted by reports of
the FAA Administrator. Subtitle VII: on a substantial number of small entities cracked slat tracks at the location of the front
Aviation Programs, describes in more under the criteria of the Regulatory stop attachment to the track. We are issuing
detail the scope of the Agency’s Flexibility Act. this AD to detect and correct cracked slat
authority. tracks which could affect the structural
We are issuing this rulemaking under List of Subjects in 14 CFR Part 39 integrity of the slat surface, possibly leading
the authority described in Subtitle VII, Air transportation, Aircraft, Aviation to detachment of an outer or inner slat
Part A, Subpart III, Section 44701: safety, Incorporation by reference, surface, and resulting in reduced control of
‘‘General requirements.’’ Under that Safety. the airplane.
section, Congress charges the FAA with (f) Compliance
Adoption of the Amendment
promoting safe flight of civil aircraft in
Accordingly, under the authority Comply with this AD within the
air commerce by prescribing regulations
delegated to me by the Administrator, compliance times specified, unless already
for practices, methods, and procedures done.
the Administrator finds necessary for the FAA amends 14 CFR part 39 as
safety in air commerce. This regulation follows: (g) Definitions
is within the scope of that authority (1) For the purpose of this AD, ‘‘affected
because it addresses an unsafe condition PART 39—AIRWORTHINESS slat track’’ is defined as a pre-modification
that is likely to exist or develop on DIRECTIVES 45967 slat track, located at the wing positions
products identified in this rulemaking ■ 1. The authority citation for part 39 as indicated in figure 1 to paragraph (g) of
action. this AD, and having a part number specified
continues to read as follows:
This AD is issued in accordance with in figure 2 to paragraph (g) of this AD. In case
Authority: 49 U.S.C. 106(g), 40113, 44701. the part number identification (ID) plate is
authority delegated by the Executive
Director, Aircraft Certification Service, missing or cannot be read, the slat track can
§ 39.13 [Amended]
be identified by the ink marking. If the
as authorized by FAA Order 8000.51C. ■ 2. The FAA amends § 39.13 by adding operator cannot determine the part number,
In accordance with that order, issuance the following new airworthiness then that airplane is in Group 1.
of ADs is normally a function of the directive (AD): (2) For the purpose of this AD: Group 1
Compliance and Airworthiness airplanes are those that, on the effective date
Division, but during this transition 2018–18–08 Airbus SAS: Amendment 39–
19387; Docket No. FAA–2018–0454; of this AD, have an affected slat track
period, the Executive Director has Product Identifier 2017–NM–056–AD. installed. Group 2 airplanes are those that, on
delegated the authority to issue ADs the effective date of this AD, do not have any
applicable to transport category (a) Effective Date affected slat track installed.
airplanes and associated appliances to This AD is effective October 15, 2018. BILLINGCODE 4910–13–P
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![Federal Register / Vol. 83, No. 175 / Monday, September 10, 2018 / Rules and Regulations 45545
(2) Modification of all affected slat tracks to the attention of the person identified in (p) Material Incorporated by Reference
on an airplane in accordance with the paragraph (o)(2) of this AD. Information may (1) The Director of the Federal Register
Accomplishment Instructions of Airbus be emailed to: 9-ANM-116-AMOC- approved the incorporation by reference
Service Bulletin A330–57–3126, including REQUESTS@faa.gov. Before using any (IBR) of the service information listed in this
Appendixes 02 and 03, dated December 21, approved AMOC, notify your appropriate paragraph under 5 U.S.C. 552(a) and 1 CFR
2017; or Airbus Service Bulletin A340–57– principal inspector, or lacking a principal part 51.
4133, including Appendixes 02 and 03, dated inspector, the manager of the local flight (2) You must use this service information
December 21, 2017; as applicable, terminates standards district office/certificate holding as applicable to do the actions required by
the repetitive inspections required by district office. this AD, unless this AD specifies otherwise.
paragraph (h) of this AD for that airplane, (2) Contacting the Manufacturer: For any (i) Airbus Service Bulletin A330–57–3123,
provided that, prior to modification, the requirement in this AD to obtain corrective Revision 01, dated September 27, 2017.
affected slat tracks pass an inspection (crack actions from a manufacturer, the action must (ii) Airbus Service Bulletin A330–57–3126,
free) in accordance with the instructions of be accomplished using a method approved dated December 21, 2017.
Airbus Service Bulletin A330–57–3123, by the Manager, International Section,
(iii) Airbus Service Bulletin A340–57–
Revision 01, including Appendixes 02 and Transport Standards Branch, FAA; or EASA;
4130, Revision 01, dated September 27, 2017.
03, dated September 27, 2017; or Airbus or Airbus SAS’s EASA DOA. If approved by
(iv) Airbus Service Bulletin A340–57–
Service Bulletin A340–57–4130, Revision 01, the DOA, the approval must include the
4133, dated December 21, 2017.
including Appendixes 02 and 03, dated DOA-authorized signature.
(3) For service information identified in
September 27, 2017; as applicable. (3) Reporting Requirements: A federal
this AD, contact Airbus SAS, Airworthiness
agency may not conduct or sponsor, and a
(l) Parts Installation Limitations Office—EAL, Rond-Point Emile Dewoitine
person is not required to respond to, nor
No: 2, 31700Blagnac Cedex, France; phone:
(1) Except as specified in paragraph (l)(2) shall a person be subject to a penalty for
failure to comply with a collection of +33 5 61 93 36 96; fax: +33 5 61 93 45 80;
of this AD: For Group 1 airplanes, after the
information subject to the requirements of email: airworthiness.A330-A340@airbus.com;
effective date of this AD, an affected slat
the Paperwork Reduction Act unless that internet http://www.airbus.com.
track may be installed, provided the
collection of information displays a current (4) You may view this service information
installation is accomplished using a method
valid OMB Control Number. The OMB at the FAA, Transport Standards Branch,
approved by the Manager, International
Control Number for this information 2200 South 216th St., Des Moines, WA. For
Section, Transport Standards Branch, FAA;
collection is 2120–0056. Public reporting for information on the availability of this
or EASA; or Airbus SAS’s EASA DOA. If
this collection of information is estimated to material at the FAA, call 206–231–3195.
approved by the DOA, the approval must
be approximately 1 work-hour per response, (5) You may view this service information
include the DOA-authorized signature.
including the time for reviewing instructions, that is incorporated by reference at the
(2) After modification of a Group 1 airplane
completing and reviewing the collection of National Archives and Records
as specified in paragraph (k)(2) of this AD, no
information. All responses to this collection Administration (NARA). For information on
person may install an affected slat track on
of information are mandatory. Comments the availability of this material at NARA, call
that airplane.
concerning the accuracy of this burden and 202–741–6030, or go to: http://
(3) For Group 2 airplanes: As of the
suggestions for reducing the burden should www.archives.gov/federal-register/cfr/ibr-
effective date of this AD, no person may
be directed to the FAA at: 800 Independence locations.html.
install an affected slat track on any Group 2
airplane. Ave. SW, Washington, DC 20591, Attn: Issued in Des Moines, Washington, on
Information Collection Clearance Officer, August 22, 2018.
(m) Credit for Previous Actions AES–200. James Cashdollar,
This paragraph provides credit for actions (4) Required for Compliance (RC): Except
required by paragraphs (h), (i), and (j) of this as required by paragraph (i) of this AD: If any Acting Director, System Oversight Division,
AD, if those actions were performed before service information contains procedures or Aircraft Certification Service.
the effective date of this AD using Airbus tests that are identified as RC, those [FR Doc. 2018–18907 Filed 9–7–18; 8:45 am]
Service Bulletin A330–57–3123, dated June procedures and tests must be done to comply BILLING CODE 4910–13–P
14, 2016; or Airbus Service Bulletin A340– with this AD; any procedures or tests that are
57–4130, dated June 14, 2016, provided that not identified as RC are recommended. Those
within 12 months after the effective date of procedures and tests that are not identified DEPARTMENT OF TRANSPORTATION
this AD, the additional work identified in as RC may be deviated from using accepted
Airbus Service Bulletin A330–57–3123, methods in accordance with the operator’s Federal Aviation Administration
Revision 01, including Appendixes 02 and maintenance or inspection program without
03, dated September 27, 2017; or Airbus obtaining approval of an AMOC, provided
Service Bulletin A340–57–4130, Revision 01, the procedures and tests identified as RC can 14 CFR Part 39
including Appendixes 02 and 03, dated be done and the airplane can be put back in [Docket No. FAA–2018–0613; Product
September 27, 2017; as applicable, has been an airworthy condition. Any substitutions or Identifier 2018–SW–041–AD; Amendment
completed in accordance with Airbus Service changes to procedures or tests identified as 39–19391; AD 2018–18–12]
Bulletin A330–57–3123, Revision 01, RC require approval of an AMOC.
including Appendixes 02 and 03, dated RIN 2120–AA64
(o) Related Information
September 27, 2017; or Airbus Service
Bulletin A340–57–4130, Revision 01, (1) Refer to Mandatory Continuing Airworthiness Directives; Airbus
including Appendixes 02 and 03, dated Airworthiness Information (MCAI) EASA AD Helicopters
September 27, 2017; as applicable. 2017–0060, dated April 7, 2017, for related
information. This MCAI may be found in the AGENCY: Federal Aviation
(n) Other FAA AD Provisions AD docket on the internet at http:// Administration (FAA), DOT.
The following provisions also apply to this www.regulations.gov by searching for and ACTION: Final rule; request for
AD: locating Docket No. FAA–2018–0454. comments.
(1) Alternative Methods of Compliance (2) For more information about this AD,
(AMOCs): The Manager, International contact Vladimir Ulyanov, Aerospace SUMMARY: We are adopting a new
Section, Transport Standards Branch, FAA, Engineer, International Section, Transport airworthiness directive (AD) for Airbus
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has the authority to approve AMOCs for this Standards Branch, FAA, 2200 South 216th Helicopters Model AS350B, AS350B1,
AD, if requested using the procedures found St., Des Moines, WA 98198; phone and fax
in 14 CFR 39.19. In accordance with 14 CFR 206 231 3229. AS350B2, AS350B3, and AS350BA
39.19, send your request to your principal (3) Service information identified in this helicopters with a Pall Aerospace
inspector or local Flight Standards District AD that is not incorporated by reference is Corporation inlet barrier filter (IBF)
Office, as appropriate. If sending information available at the addresses specified in element. This AD requires revising the
directly to the International Branch, send it paragraphs (p)(3) and (p)(4) of this AD. Rotorcraft Flight Manual Supplement to
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Document Created: 2018-09-08 00:42:36
Document Modified: 2018-09-08 00:42:36
| 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. | |
| Dates | This AD is effective October 15, 2018. | |
| Contact | Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3229. | |
| FR Citation | 83 FR 45539 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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