83 FR 49265 - Airworthiness Directives; Airbus SAS Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 190 (October 1, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 190 (October 1, 2018)
| Page Range | 49265-49269 | |
| FR Document | 2018-21100 |
[Federal Register Volume 83, Number 190 (Monday, October 1, 2018)] [Rules and Regulations] [Pages 49265-49269] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-21100] ======================================================================== Rules and Regulations Federal Register ________________________________________________________________________ This section of the FEDERAL REGISTER contains regulatory documents having general applicability and legal effect, most of which are keyed to and codified in the Code of Federal Regulations, which is published under 50 titles pursuant to 44 U.S.C. 1510. The Code of Federal Regulations is sold by the Superintendent of Documents. ======================================================================== Federal Register / Vol. 83, No. 190 / Monday, October 1, 2018 / Rules and Regulations [[Page 49265]] DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0417; Product Identifier 2017-NM-132-AD; Amendment 39-19440; AD 2018-20-06] RIN 2120-AA64 Airworthiness Directives; Airbus SAS Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are superseding Airworthiness Directive (AD) 2016-25-03, which applied to certain Airbus Model A300 F4-600R series airplanes. AD 2016-25-03 required repetitive high frequency eddy current (HFEC) inspections of the aft lower deck cargo door (LDCD) frame forks; a one- time check of the LDCD clearances; and a one-time detailed visual inspection of hooks, eccentric bushes, and x-stops; and corrective actions if necessary. This AD requires repetitive HFEC inspections of the aft LDCD frame forks; a one-time check of the LDCD clearances; and a one-time detailed visual inspection of hooks, eccentric bushes, and x-stops; and corrective actions if necessary. This AD was prompted by a report of two adjacent frame forks that were found cracked on the aft LDCD of two airplanes during scheduled maintenance, and the introduction of frame fork reinforcement or repair procedures that, when done, allow an extension of repetitive inspection intervals. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 5, 2018. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of November 5, 2018. The Director of the Federal Register approved the incorporation by reference of a certain other publication listed in this AD as of January 26, 2017 (81 FR 93801, December 22, 2016). ADDRESSES: For service information identified in this final rule, contact Airbus SAS, Airworthiness Office--EAW, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email [email protected]; internet http://www.airbus.com. You may view this referenced 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-2018-0417. 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- 0417; 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 information. The address for Docket Operations (phone: 800-647- 5527) is U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. 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: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 to supersede AD 2016-25-03, Amendment 39-18729 (81 FR 93801, December 22, 2016) (``AD 2016-25-03''). AD 2016-25-03 applied to certain Airbus Model A300 F4-600R series airplanes. The NPRM published in the Federal Register on May 25, 2018 (83 FR 24244). The NPRM was prompted by a report of two adjacent frame forks that were found cracked on the aft LDCD of two airplanes during scheduled maintenance, and the introduction of frame fork reinforcement or repair procedures that, when done, allow an extension of repetitive inspection intervals. The NPRM proposed to continue to require repetitive HFEC inspections of the aft LDCD frame forks; a one-time check of the LDCD clearances; and a one-time detailed visual inspection of hooks, eccentric bushes, and x-stops; and corrective actions if necessary. The NPRM also proposed to require revised corrective actions and compliance times. We are issuing this AD to address cracked or ruptured aft LDCD frames, which could allow loads to be transferred to the remaining structural elements. This condition could lead to the rupture of one or more vertical aft LDCD frames, which could result in reduced structural integrity of the aft LDCD. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2015-0152R1, dated May 23, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Airbus SAS Model A300 F4-600R series airplanes. The MCAI states: During scheduled maintenance at frames (FR) 61 and FR61A on the aft lower deck cargo door (LDCD) of two A300-600F4 aeroplanes, two adjacent frame forks were found cracked. Subsequent analysis determined that, in case of cracked or ruptured aft cargo door frame(s), loads will be transferred to the remaining structural elements. However, these secondary load paths will be able to sustain the loads for a limited number of flight cycles only. This condition, if not detected and corrected, could lead to the rupture of one or more vertical aft cargo door frame(s), resulting in reduced structural integrity of the aft cargo door. To address this unsafe condition, Airbus issued Alert Operators Transmission (AOT) A52W011-15 to provide inspection instructions, and, consequently, EASA issued AD 2015-0152 [which corresponds to FAA AD 2016-25-03] to require repetitive inspections of the aft LDCD frame forks and, depending on findings, the accomplishment of applicable corrective action(s). Since that [EASA] AD was issued, Airbus published Service Bulletin (SB) SB A300-52-6085 which provides frame fork [[Page 49266]] reinforcement instruction and SB A300-52-6086 which provides instruction to inspect the cargo door for cracks as well as frame fork replacement instructions having the inspection interval extended from 600 flight cycles (FC) to 1,200 FC. For the reason described above, this [EASA] AD is revised to introduce frame forks replacement or repair [or reinforcement] as an allowance to extend the inspection interval. Required actions include repetitive HFEC inspections of the aft LDCD frame forks and repair, reinforcement, or replacement if necessary; a one-time check of the LDCD clearances and adjustment if necessary; and a one-time detailed visual inspection of hooks, eccentric bushes, and x-stops for wear, and corrective actions if necessary. Corrective actions include blend-out, adjustment, and replacement of hooks, bushes and x-stops. 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-2018-0417. Comments We gave the public the opportunity to participate in developing this final rule. The following presents the comment received on the NPRM and the FAA's response to the comment. Request To Incorporate Revised Service Bulletins FedEx Express requested that we revise the proposed AD to incorporate Airbus Service Bulletin A300-52-6085, Revision 01, dated May 2, 2018; and Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018. FedEx Express also requested that we update table 1 to paragraph (g) of the proposed AD with the revised compliance times specified in Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018. We partially agree with the commenter's requested changes. We agree to incorporate Airbus Service Bulletin A300-52-6085, Revision 01, dated May 2, 2018; and Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018; because the changes to the procedures in those documents are not significant. The changes include updating reference documents and figures and do not result in any additional work for airplanes modified using the previous issue. Therefore, we have revised this AD to refer to Airbus Service Bulletin A300-52-6085, Revision 01, dated May 2, 2018; and Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018, as the appropriate sources of service information for certain actions. We have also revised this AD to give credit for certain actions accomplished using Airbus Service Bulletin A300-52-6085, Revision 00, dated December 22, 2016; and Airbus Service Bulletin A300-52-6086, Revision 00, dated December 25, 2016. The updated compliance times in Airbus Service Bulletin A300-52- 6086, Revision 01, dated May 29, 2018, are substantively different from the compliance times specified in the proposed AD and would increase the scope of this AD without allowing for public notice and comment. Therefore, we have not changed this AD with regard to the compliance times specified in Airbus Service Bulletin A300-52-6086. However, under the provisions of paragraph (n)(1) of this AD, we will consider requests for approval of alternative compliance times if sufficient data are submitted to substantiate that the extension would provide an acceptable level of safety. Conclusion We reviewed the relevant data, considered the comment received, 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. We also determined that these changes will not increase the economic burden on any operator or increase the scope of this final rule. Related Service Information Under 1 CFR Part 51 Airbus has issued the following service information: Alert Operators Transmission A52W011-15, Revision 00, including Appendices 1, 2, 3, and 4, dated July 23, 2015, which describes procedures for a check of the aft LDCD clearances ``U'' and ``V'' between the latching hooks and the eccentric bush at frame FR60 through FR64A and an adjustment of the latching hook; a detailed inspection to detect signs of wear of the hooks, eccentric bushes, and x-stops and corrective actions; and an HFEC inspection to detect cracking at all frame fork stations of the aft LDCD and a replacement of the frame fork. Service Bulletin A300-52-6085, Revision 01, dated May 2, 2018, which describes procedures for reinforcing frame fork fastener holes, which include related investigative and corrective actions. The related investigative actions include a rotating probe inspection for cracking of the fastener holes and a check to determine the hole diameter. Corrective actions include repair and cold working the fastener holes. Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018, which describes procedures for a check of the aft LDCD clearances ``U'' and ``V'' between the latching hooks and the eccentric bush at FR60 through FR64A and an adjustment of the latching hook; and HFEC inspection to detect cracking at all frame fork stations of the aft LDCD and a repair of the frame fork. 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 58 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs for Required Actions ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- 17 work-hours x $85 per hour = $1,445........................ $0 $1,445 $83,810 ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary on-condition actions that would be required based on the results of any required actions. We have no way of determining the number of aircraft that might need these on-condition actions: [[Page 49267]] Estimated Costs of On-condition Actions ------------------------------------------------------------------------ Cost per Labor cost Parts cost product ------------------------------------------------------------------------ Up to 65 work-hours x $85 per hour = $10,000 $15,525 $5,525............................... ------------------------------------------------------------------------ Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes to the Director of the System Oversight Division. Regulatory Findings We determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: 1. Is not a ``significant regulatory action'' under Executive Order 12866; 2. Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); 3. Will not affect intrastate aviation in Alaska; and 4. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. 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 removing Airworthiness Directive (AD) 2016-25-03, Amendment 39-18729 (81 FR 93801, December 22, 2016), and adding the following new AD: 2018-20-06 Airbus SAS: Amendment 39-19440; Docket No. FAA-2018-0417; Product Identifier 2017-NM-132-AD. (a) Effective Date This AD is effective November 5, 2018. (b) Affected ADs This AD replaces AD 2016-25-03, Amendment 39-18729 (81 FR 93801, December 22, 2016) (``AD 2016-25-03''). (c) Applicability This AD applies to Airbus SAS Model A300 F4-605R and A300 F4- 622R airplanes, certificated in any category, on which Airbus SAS modification 12046 has been embodied in production. Modification 12046 has been embodied in production on manufacturer serial numbers (MSNs) 0805 and above, except MSNs 0836, 0837, and 0838. (d) Subject Air Transport Association (ATA) of America Code 52, Doors. (e) Reason This AD was prompted by a report of two adjacent frame forks that were found cracked on the aft lower deck cargo door (LDCD) of two airplanes during scheduled maintenance, and the introduction of frame fork reinforcement or repair procedures that, when done, allow an extension of repetitive inspection intervals. We are issuing this AD to address cracked or ruptured aft LDCD frames, which could allow loads to be transferred to the remaining structural elements. This condition could lead to the rupture of one or more vertical aft LDCD frames, which could result in reduced structural integrity of the aft LDCD. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Retained Inspection Requirements and On-Condition Actions, With Revised Compliance Times and New Service Information This paragraph restates the requirements of paragraph (g) of AD 2016-25-03, with revised compliance times and new service information. At the applicable time specified in paragraph (h) of this AD, or before exceeding the threshold defined in table 1 to paragraph (g) of this AD, whichever occurs later: Do the actions specified in paragraphs (g)(1), (g)(2), and (g)(3) of this AD. Repeat the high frequency eddy current (HFEC) inspection specified in paragraph (g)(3) of this AD thereafter at intervals not to exceed the applicable times specified in table 1 to paragraph (g) of this AD. (1) A one-time check of the aft LDCD clearances ``U'' and ``V'' between the latching hooks and the eccentric bush at FR60 through FR64A, in accordance with the instructions of Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015; or the Accomplishment Instructions of Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018. If any value outside tolerance is found, adjust the latching hook before further flight, in accordance with the instructions of Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015; or the Accomplishment Instructions of Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018. (2) A one-time detailed inspection to detect signs of wear of the hooks, eccentric bushes, and x-stops, in accordance with the instructions of Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015. If any wear is found, do all applicable corrective actions before further flight, in accordance with the instructions of Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015. (3) An HFEC inspection to detect cracking at all frame fork stations of the aft LDCD, in accordance with the instructions of Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015; or the Accomplishment Instructions of Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018, 2016. If any crack is found, before further flight, replace the cracked frame fork, in accordance with the instructions of Airbus Alert Operators Transmission A52W011-15, Revision 00, [[Page 49268]] dated July 23, 2015; repair the cracked frame fork, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018; or reinforce the cracked frame fork, including doing all applicable related investigative and corrective actions, in accordance with the Accomplishment Instructions of Airbus Service Bulletin A300-52-6085, Revision 01, dated May 2, 2018, except as required by paragraph (i) of this AD. [GRAPHIC] [TIFF OMITTED] TR01OC18.004 (h) Retained Compliance Times, With No Changes At the later of the times specified in paragraphs (h)(1) and (h)(2) of this AD, do the actions required by paragraph (g) of this AD. (1) Before the accumulation of 4,500 total flight cycles. (2) At the applicable time specified by paragraph (h)(2)(i) or (h)(2)(ii) of this AD. (i) For airplanes that have accumulated 8,000 or more total flight cycles as of January 26, 2017 (the effective date of AD 2016- 25-03): Within 100 flight cycles after January 26, 2017. (ii) For airplanes that have accumulated fewer than 8,000 total flight cycles as of January 26, 2017 (the effective date of AD 2016- 25-03): Within 400 flight cycles after January 26, 2017. (i) Service Information Exception Where Airbus Service Bulletin A300-52-6085, Revision 01, dated May 2, 2018, specifies to contact Airbus for appropriate action: Before further flight, accomplish corrective actions in accordance with the procedures specified in paragraph (n)(2) of this AD. (j) No Terminating Action Accomplishment of corrective actions on an airplane as required by paragraph (g)(1) or (g)(2) of this AD, or repair, reinforcement, or replacement of a frame fork as required by paragraph (g)(3) of this AD, on the aft LDCD of an airplane does not constitute terminating action for the repetitive HFEC inspections required by paragraph (g)(3) of this AD for that airplane. (k) Compliance Time Clarification After replacement, repair, or reinforcement of any frame fork on the aft LDCD of an airplane, as specified in paragraph (g)(3) of this AD, the next HFEC inspection as required by paragraph (g)(3) of this AD can be deferred for any frame fork that is replaced, repaired, or reinforced, but must be accomplished before exceeding 6,800 flight cycles after the replacement, repair, or reinforcement of that frame fork. (l) No Reporting Although the Accomplishment Instructions of Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015; and Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018; specify to submit certain information to the manufacturer, this AD does not include that requirement. (m) Credit for Previous Actions (1) This paragraph provides credit for actions required by paragraphs (g)(1) and (g)(3) of this AD, if those actions were performed before the effective date of this AD using Airbus Service Bulletin A300-52-6086, Revision 00, dated December 25, 2016. (2) This paragraph provides credit for actions required by paragraph (g)(3) of this AD, if those actions were performed before the effective date of this AD using Airbus Service Bulletin A300-52- 6085, Revision 00, dated December 22, 2016. (n) Other FAA AD Provisions (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 (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: As of the effective date of this AD, 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 Airbus SAS's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (3) Required for Compliance (RC): Except as required by paragraph (i) and paragraph (l) 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 2015-0152R1, dated May 23, 2017, for related information. This MCAI may be found in the AD docket on the iInternet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0417. (2) For more information about this AD, contact Dan Rodina, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des [[Page 49269]] Moines, WA 98198; telephone and fax 206-231-3225. (3) Service information identified in this AD that is not incorporated by reference is available at the addresses specified in paragraphs (p)(5) and (p)(6) 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. (3) The following service information was approved for IBR on November 5, 2018. (i) Airbus Service Bulletin A300-52-6085, Revision 01, dated May 2, 2018. (ii) Airbus Service Bulletin A300-52-6086, Revision 01, dated May 29, 2018. (4) The following service information was approved for IBR on January 26, 2017 (81 FR 93801, December 22, 2016). (i) Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015, including the following appendices: (A) Appendix 1--Flowchart, undated. (B) Appendix 2--Reporting Sheet, undated. (The pages of Appendix 2 are not numbered.) (C) Appendix 3--titled ``Technical Disposition,'' Ref. TD/K12/ L3/02978/2015, Issue B, dated July 21, 2015. (Appendix 3 is identified with an appendix number only on page 1 of Airbus Alert Operators Transmission A52W011-15, Revision 00, dated July 23, 2015.) (D) Appendix 4--Part number identification for frame forks and bushings, undated. (ii) Reserved. (5) For service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAW, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 44 51; email [email protected]; Internet http://www.airbus.com. (6) 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. (7) 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 September 21, 2018. John P. Piccola, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-21100 Filed 9-28-18; 8:45 am] BILLING CODE 4910-13-P
![49265
Rules and Regulations Federal Register
Vol. 83, No. 190
Monday, October 1, 2018
This section of the FEDERAL REGISTER of certain publications listed in this AD FR 24244). The NPRM was prompted by
contains regulatory documents having general as of November 5, 2018. a report of two adjacent frame forks that
applicability and legal effect, most of which The Director of the Federal Register were found cracked on the aft LDCD of
are keyed to and codified in the Code of approved the incorporation by reference two airplanes during scheduled
Federal Regulations, which is published under of a certain other publication listed in maintenance, and the introduction of
50 titles pursuant to 44 U.S.C. 1510.
this AD as of January 26, 2017 (81 FR frame fork reinforcement or repair
The Code of Federal Regulations is sold by 93801, December 22, 2016). procedures that, when done, allow an
the Superintendent of Documents. ADDRESSES: For service information extension of repetitive inspection
identified in this final rule, contact intervals. The NPRM proposed to
Airbus SAS, Airworthiness Office— continue to require repetitive HFEC
DEPARTMENT OF TRANSPORTATION EAW, Rond-Point Emile Dewoitine No: inspections of the aft LDCD frame forks;
2, 31700 Blagnac Cedex, France; a one-time check of the LDCD
Federal Aviation Administration clearances; and a one-time detailed
telephone +33 5 61 93 36 96; fax +33 5
61 93 44 51; email account.airworth- visual inspection of hooks, eccentric
14 CFR Part 39 bushes, and x-stops; and corrective
eas@airbus.com; internet http://
www.airbus.com. You may view this actions if necessary. The NPRM also
[Docket No. FAA–2018–0417; Product
Identifier 2017–NM–132–AD; Amendment referenced service information at the proposed to require revised corrective
39–19440; AD 2018–20–06] FAA, Transport Standards Branch, 2200 actions and compliance times. We are
South 216th St., Des Moines, WA. For issuing this AD to address cracked or
RIN 2120–AA64 information on the availability of this ruptured aft LDCD frames, which could
material at the FAA, call 206–231–3195. allow loads to be transferred to the
Airworthiness Directives; Airbus SAS It is also available on the internet at remaining structural elements. This
Airplanes http://www.regulations.gov by searching condition could lead to the rupture of
for and locating Docket No. FAA–2018– one or more vertical aft LDCD frames,
AGENCY: Federal Aviation 0417. which could result in reduced structural
Administration (FAA), Department of integrity of the aft LDCD.
Transportation (DOT). Examining the AD Docket The European Aviation Safety Agency
ACTION: Final rule. You may examine the AD docket on (EASA), which is the Technical Agent
the internet at http:// for the Member States of the European
SUMMARY: We are superseding www.regulations.gov by searching for Union, has issued EASA Airworthiness
Airworthiness Directive (AD) 2016–25– and locating Docket No. FAA–2018– Directive 2015–0152R1, dated May 23,
03, which applied to certain Airbus 0417; or in person at Docket Operations 2017 (referred to after this as the
Model A300 F4–600R series airplanes. between 9 a.m. and 5 p.m., Monday Mandatory Continuing Airworthiness
AD 2016–25–03 required repetitive high through Friday, except Federal holidays. Information, or ‘‘the MCAI’’), to correct
frequency eddy current (HFEC) The AD docket contains this final rule, an unsafe condition for certain Airbus
inspections of the aft lower deck cargo the regulatory evaluation, any SAS Model A300 F4–600R series
door (LDCD) frame forks; a one-time comments received, and other airplanes. The MCAI states:
check of the LDCD clearances; and a information. The address for Docket
one-time detailed visual inspection of During scheduled maintenance at frames
Operations (phone: 800–647–5527) is (FR) 61 and FR61A on the aft lower deck
hooks, eccentric bushes, and x-stops; U.S. Department of Transportation, cargo door (LDCD) of two A300–600F4
and corrective actions if necessary. This Docket Operations, M–30, West aeroplanes, two adjacent frame forks were
AD requires repetitive HFEC inspections Building Ground Floor, Room W12–140, found cracked. Subsequent analysis
of the aft LDCD frame forks; a one-time 1200 New Jersey Avenue SE, determined that, in case of cracked or
check of the LDCD clearances; and a ruptured aft cargo door frame(s), loads will
Washington, DC 20590.
one-time detailed visual inspection of be transferred to the remaining structural
FOR FURTHER INFORMATION CONTACT: Dan elements. However, these secondary load
hooks, eccentric bushes, and x-stops; Rodina, Aerospace Engineer, paths will be able to sustain the loads for a
and corrective actions if necessary. This International Section, Transport limited number of flight cycles only.
AD was prompted by a report of two Standards Branch, FAA, 2200 South This condition, if not detected and
adjacent frame forks that were found 216th St., Des Moines, WA 98198; corrected, could lead to the rupture of one or
cracked on the aft LDCD of two telephone and fax 206–231–3225. more vertical aft cargo door frame(s),
airplanes during scheduled resulting in reduced structural integrity of
SUPPLEMENTARY INFORMATION: the aft cargo door.
maintenance, and the introduction of
frame fork reinforcement or repair Discussion To address this unsafe condition, Airbus
issued Alert Operators Transmission (AOT)
procedures that, when done, allow an We issued a notice of proposed A52W011–15 to provide inspection
extension of repetitive inspection rulemaking (NPRM) to amend 14 CFR instructions, and, consequently, EASA issued
intervals. We are issuing this AD to part 39 to supersede AD 2016–25–03, AD 2015–0152 [which corresponds to FAA
amozie on DSK3GDR082PROD with RULES
address the unsafe condition on these Amendment 39–18729 (81 FR 93801, AD 2016–25–03] to require repetitive
products. December 22, 2016) (‘‘AD 2016–25– inspections of the aft LDCD frame forks and,
depending on findings, the accomplishment
DATES:This AD is effective November 5, 03’’). AD 2016–25–03 applied to certain of applicable corrective action(s).
2018. Airbus Model A300 F4–600R series Since that [EASA] AD was issued, Airbus
The Director of the Federal Register airplanes. The NPRM published in the published Service Bulletin (SB) SB A300–52–
approved the incorporation by reference Federal Register on May 25, 2018 (83 6085 which provides frame fork
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![49266 Federal Register / Vol. 83, No. 190 / Monday, October 1, 2018 / Rules and Regulations
reinforcement instruction and SB A300–52– changes to the procedures in those burden on any operator or increase the
6086 which provides instruction to inspect documents are not significant. The scope of this final rule.
the cargo door for cracks as well as frame fork changes include updating reference
replacement instructions having the Related Service Information Under 1
documents and figures and do not result
inspection interval extended from 600 flight CFR Part 51
cycles (FC) to 1,200 FC.
in any additional work for airplanes
For the reason described above, this modified using the previous issue. Airbus has issued the following
[EASA] AD is revised to introduce frame Therefore, we have revised this AD to service information:
forks replacement or repair [or refer to Airbus Service Bulletin A300– • Alert Operators Transmission
reinforcement] as an allowance to extend the 52–6085, Revision 01, dated May 2, A52W011–15, Revision 00, including
inspection interval. 2018; and Airbus Service Bulletin Appendices 1, 2, 3, and 4, dated July 23,
Required actions include repetitive A300–52–6086, Revision 01, dated May 2015, which describes procedures for a
HFEC inspections of the aft LDCD frame 29, 2018, as the appropriate sources of check of the aft LDCD clearances ‘‘U’’
forks and repair, reinforcement, or service information for certain actions. and ‘‘V’’ between the latching hooks and
replacement if necessary; a one-time We have also revised this AD to give the eccentric bush at frame FR60
check of the LDCD clearances and credit for certain actions accomplished through FR64A and an adjustment of
adjustment if necessary; and a one-time using Airbus Service Bulletin A300–52– the latching hook; a detailed inspection
detailed visual inspection of hooks, 6085, Revision 00, dated December 22, to detect signs of wear of the hooks,
eccentric bushes, and x-stops for wear, 2016; and Airbus Service Bulletin eccentric bushes, and x-stops and
and corrective actions if necessary. A300–52–6086, Revision 00, dated corrective actions; and an HFEC
Corrective actions include blend-out, December 25, 2016. inspection to detect cracking at all frame
adjustment, and replacement of hooks, The updated compliance times in fork stations of the aft LDCD and a
bushes and x-stops. You may examine Airbus Service Bulletin A300–52–6086, replacement of the frame fork.
the MCAI in the AD docket on the Revision 01, dated May 29, 2018, are • Service Bulletin A300–52–6085,
internet at http://www.regulations.gov substantively different from the Revision 01, dated May 2, 2018, which
by searching for and locating Docket No. compliance times specified in the describes procedures for reinforcing
FAA–2018–0417. proposed AD and would increase the frame fork fastener holes, which include
scope of this AD without allowing for related investigative and corrective
Comments public notice and comment. Therefore, actions. The related investigative
We gave the public the opportunity to we have not changed this AD with actions include a rotating probe
participate in developing this final rule. regard to the compliance times specified inspection for cracking of the fastener
The following presents the comment in Airbus Service Bulletin A300–52– holes and a check to determine the hole
received on the NPRM and the FAA’s 6086. However, under the provisions of diameter. Corrective actions include
response to the comment. paragraph (n)(1) of this AD, we will repair and cold working the fastener
consider requests for approval of holes.
Request To Incorporate Revised Service alternative compliance times if • Service Bulletin A300–52–6086,
Bulletins sufficient data are submitted to Revision 01, dated May 29, 2018, which
FedEx Express requested that we substantiate that the extension would describes procedures for a check of the
revise the proposed AD to incorporate provide an acceptable level of safety. aft LDCD clearances ‘‘U’’ and ‘‘V’’
Airbus Service Bulletin A300–52–6085, between the latching hooks and the
Conclusion
Revision 01, dated May 2, 2018; and eccentric bush at FR60 through FR64A
Airbus Service Bulletin A300–52–6086, We reviewed the relevant data, and an adjustment of the latching hook;
Revision 01, dated May 29, 2018. FedEx considered the comment received, and and HFEC inspection to detect cracking
Express also requested that we update determined that air safety and the at all frame fork stations of the aft LDCD
table 1 to paragraph (g) of the proposed public interest require adopting this and a repair of the frame fork.
AD with the revised compliance times final rule as proposed, except for minor This service information is reasonably
specified in Airbus Service Bulletin editorial changes. We have determined available because the interested parties
A300–52–6086, Revision 01, dated May that these minor changes: have access to it through their normal
29, 2018. • Are consistent with the intent that course of business or by the means
We partially agree with the was proposed in the NPRM for identified in the ADDRESSES section.
commenter’s requested changes. We addressing the unsafe condition; and
agree to incorporate Airbus Service • Do not add any additional burden Costs of Compliance
Bulletin A300–52–6085, Revision 01, upon the public than was already We estimate that this AD affects 58
dated May 2, 2018; and Airbus Service proposed in the NPRM. airplanes of U.S. registry. We estimate
Bulletin A300–52–6086, Revision 01, We also determined that these the following costs to comply with this
dated May 29, 2018; because the changes will not increase the economic AD:
ESTIMATED COSTS FOR REQUIRED ACTIONS
Cost per Cost on U.S.
Labor cost Parts cost product operators
17 work-hours × $85 per hour = $1,445 ..................................................................................... $0 $1,445 $83,810
amozie on DSK3GDR082PROD with RULES
We estimate the following costs to do of any required actions. We have no way that might need these on-condition
any necessary on-condition actions that of determining the number of aircraft actions:
would be required based on the results
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![Federal Register / Vol. 83, No. 190 / Monday, October 1, 2018 / Rules and Regulations 49267
ESTIMATED COSTS OF ON-CONDITION ACTIONS
Cost per
Labor cost Parts cost product
Up to 65 work-hours × $85 per hour = $5,525 ....................................................................................................... $10,000 $15,525
Authority for This Rulemaking under the criteria of the Regulatory elements. This condition could lead to the
Flexibility Act. rupture of one or more vertical aft LDCD
Title 49 of the United States Code frames, which could result in reduced
specifies the FAA’s authority to issue List of Subjects in 14 CFR Part 39 structural integrity of the aft LDCD.
rules on aviation safety. Subtitle I, Air transportation, Aircraft, Aviation (f) Compliance
section 106, describes the authority of safety, Incorporation by reference,
the FAA Administrator. Subtitle VII: Comply with this AD within the
Safety. compliance times specified, unless already
Aviation Programs, describes in more
Adoption of the Amendment done.
detail the scope of the Agency’s
authority. Accordingly, under the authority (g) Retained Inspection Requirements and
We are issuing this rulemaking under On-Condition Actions, With Revised
delegated to me by the Administrator,
the authority described in Subtitle VII, Compliance Times and New Service
the FAA amends 14 CFR part 39 as Information
Part A, Subpart III, Section 44701: follows:
‘‘General requirements.’’ Under that This paragraph restates the requirements of
section, Congress charges the FAA with PART 39—AIRWORTHINESS paragraph (g) of AD 2016–25–03, with
revised compliance times and new service
promoting safe flight of civil aircraft in DIRECTIVES
information. At the applicable time specified
air commerce by prescribing regulations in paragraph (h) of this AD, or before
for practices, methods, and procedures ■ 1. The authority citation for part 39
exceeding the threshold defined in table 1 to
the Administrator finds necessary for continues to read as follows: paragraph (g) of this AD, whichever occurs
safety in air commerce. This regulation Authority: 49 U.S.C. 106(g), 40113, 44701. later: Do the actions specified in paragraphs
is within the scope of that authority (g)(1), (g)(2), and (g)(3) of this AD. Repeat the
§ 39.13 [Amended] high frequency eddy current (HFEC)
because it addresses an unsafe condition
that is likely to exist or develop on ■ 2. The FAA amends § 39.13 by inspection specified in paragraph (g)(3) of
removing Airworthiness Directive (AD) this AD thereafter at intervals not to exceed
products identified in this rulemaking
the applicable times specified in table 1 to
action. 2016–25–03, Amendment 39–18729 (81 paragraph (g) of this AD.
This AD is issued in accordance with FR 93801, December 22, 2016), and (1) A one-time check of the aft LDCD
authority delegated by the Executive adding the following new AD: clearances ‘‘U’’ and ‘‘V’’ between the latching
Director, Aircraft Certification Service, 2018–20–06 Airbus SAS: Amendment 39– hooks and the eccentric bush at FR60
as authorized by FAA Order 8000.51C. 19440; Docket No. FAA–2018–0417; through FR64A, in accordance with the
In accordance with that order, issuance Product Identifier 2017–NM–132–AD. instructions of Airbus Alert Operators
of ADs is normally a function of the Transmission A52W011–15, Revision 00,
(a) Effective Date dated July 23, 2015; or the Accomplishment
Compliance and Airworthiness
This AD is effective November 5, 2018. Instructions of Airbus Service Bulletin A300–
Division, but during this transition 52–6086, Revision 01, dated May 29, 2018. If
period, the Executive Director has (b) Affected ADs any value outside tolerance is found, adjust
delegated the authority to issue ADs This AD replaces AD 2016–25–03, the latching hook before further flight, in
applicable to transport category Amendment 39–18729 (81 FR 93801, accordance with the instructions of Airbus
airplanes to the Director of the System December 22, 2016) (‘‘AD 2016–25–03’’). Alert Operators Transmission A52W011–15,
Oversight Division. Revision 00, dated July 23, 2015; or the
(c) Applicability Accomplishment Instructions of Airbus
Regulatory Findings This AD applies to Airbus SAS Model Service Bulletin A300–52–6086, Revision 01,
A300 F4–605R and A300 F4–622R airplanes, dated May 29, 2018.
We determined that this AD will not certificated in any category, on which Airbus (2) A one-time detailed inspection to detect
have federalism implications under SAS modification 12046 has been embodied signs of wear of the hooks, eccentric bushes,
Executive Order 13132. This AD will in production. Modification 12046 has been and x-stops, in accordance with the
not have a substantial direct effect on embodied in production on manufacturer instructions of Airbus Alert Operators
the States, on the relationship between serial numbers (MSNs) 0805 and above, Transmission A52W011–15, Revision 00,
the national government and the States, except MSNs 0836, 0837, and 0838. dated July 23, 2015. If any wear is found, do
or on the distribution of power and all applicable corrective actions before
(d) Subject further flight, in accordance with the
responsibilities among the various
Air Transport Association (ATA) of instructions of Airbus Alert Operators
levels of government. America Code 52, Doors. Transmission A52W011–15, Revision 00,
For the reasons discussed above, I dated July 23, 2015.
certify that this AD: (e) Reason (3) An HFEC inspection to detect cracking
1. Is not a ‘‘significant regulatory This AD was prompted by a report of two at all frame fork stations of the aft LDCD, in
action’’ under Executive Order 12866; adjacent frame forks that were found cracked accordance with the instructions of Airbus
2. Is not a ‘‘significant rule’’ under the on the aft lower deck cargo door (LDCD) of Alert Operators Transmission A52W011–15,
DOT Regulatory Policies and Procedures two airplanes during scheduled maintenance, Revision 00, dated July 23, 2015; or the
amozie on DSK3GDR082PROD with RULES
(44 FR 11034, February 26, 1979); and the introduction of frame fork Accomplishment Instructions of Airbus
reinforcement or repair procedures that, Service Bulletin A300–52–6086, Revision 01,
3. Will not affect intrastate aviation in when done, allow an extension of repetitive dated May 29, 2018, 2016. If any crack is
Alaska; and inspection intervals. We are issuing this AD found, before further flight, replace the
4. Will not have a significant to address cracked or ruptured aft LDCD cracked frame fork, in accordance with the
economic impact, positive or negative, frames, which could allow loads to be instructions of Airbus Alert Operators
on a substantial number of small entities transferred to the remaining structural Transmission A52W011–15, Revision 00,
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![Federal Register / Vol. 83, No. 190 / Monday, October 1, 2018 / Rules and Regulations 49269
Moines, WA 98198; telephone and fax 206– DEPARTMENT OF TRANSPORTATION www.regulations.gov by searching for
231–3225. and locating Docket No. FAA 2018–
(3) Service information identified in this Federal Aviation Administration 0395; or in person at Docket Operations
AD that is not incorporated by reference is between 9 a.m. and 5 p.m., Monday
available at the addresses specified in 14 CFR Part 39 through Friday, except Federal holidays.
paragraphs (p)(5) and (p)(6) of this AD. The AD docket contains this final rule,
[Docket No. FAA–2018–0395; Product
(p) Material Incorporated by Reference Identifier 2017–NM–136–AD; Amendment the regulatory evaluation, any
39–19430; AD 2018–19–29] comments received, and other
(1) The Director of the Federal Register
information. The address for Docket
approved the incorporation by reference RIN 2120–AA64
Operations (phone: 800–647–5527) is in
(IBR) of the service information listed in this
Airworthiness Directives; Airbus SAS the ADDRESSES section.
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51. Airplanes FOR FURTHER INFORMATION CONTACT:
(2) You must use this service information AGENCY: Federal Aviation Vladimir Ulyanov, Aerospace Engineer,
as applicable to do the actions required by Administration (FAA), Department of International Section, Transport
this AD, unless this AD specifies otherwise. Transportation (DOT). Standards Branch, FAA, 2200 South
(3) The following service information was 216th St., Des Moines, WA 98198–6547;
ACTION: Final rule.
approved for IBR on November 5, 2018. telephone and fax 206–231–3229.
(i) Airbus Service Bulletin A300–52–6085, SUMMARY: We are adopting a new SUPPLEMENTARY INFORMATION:
Revision 01, dated May 2, 2018. airworthiness directive (AD) for all
(ii) Airbus Service Bulletin A300–52–6086, Airbus SAS Model A330–200 Freighter, Discussion
Revision 01, dated May 29, 2018. –200, and –300 series airplanes; and
(4) The following service information was
We issued a notice of proposed
Airbus SAS Model A340–200, –300, rulemaking (NPRM) to amend 14 CFR
approved for IBR on January 26, 2017 (81 FR –500, and –600 series airplanes. This
93801, December 22, 2016). part 39 by adding an AD that would
AD was prompted by a report of apply to all Airbus Model A330–200
(i) Airbus Alert Operators Transmission deficient fatigue performance of high
A52W011–15, Revision 00, dated July 23, Freighter series airplanes, Model A330–
strength steel used in forgings. 200 series airplanes, Model A330–300
2015, including the following appendices: Components made from the affected
(A) Appendix 1—Flowchart, undated. series airplanes, Model A340–200 series
high strength steel are installed on the airplanes, Model A340–300 series
(B) Appendix 2—Reporting Sheet, undated. main landing gear (MLG), nose landing
(The pages of Appendix 2 are not numbered.) airplanes, Model A340–500 series
gear (NLG), and center landing gear airplanes, and Model A340–600 series
(C) Appendix 3—titled ‘‘Technical (CLG). This AD requires identifying the
Disposition,’’ Ref. TD/K12/L3/02978/2015, airplanes. The NPRM published in the
part number and serial number of
Issue B, dated July 21, 2015. (Appendix 3 is Federal Register on May 9, 2018 (83 FR
certain components installed on the
identified with an appendix number only on 21196). The NPRM was prompted by a
MLG, NLG, and CLG; replacing affected
page 1 of Airbus Alert Operators report of deficient fatigue performance
parts; identifying the airplane’s weight
Transmission A52W011–15, Revision 00, of high strength steel used in forgings.
variant; and determining the applicable
dated July 23, 2015.) Components made from the affected
life limit for certain components
(D) Appendix 4—Part number high strength steel are installed on the
installed on the MLG, NLG, and CLG.
identification for frame forks and bushings, MLG, NLG, and CLG. The NPRM
We are issuing this AD to address the
undated. proposed to require identifying the part
(ii) Reserved.
unsafe condition on these products.
number and serial number of certain
(5) For service information identified in DATES: This AD is effective November 5,
components installed on the MLG, NLG,
this AD, contact Airbus SAS, Airworthiness 2018. and CLG; replacing affected parts;
Office—EAW, Rond-Point Emile Dewoitine The Director of the Federal Register
identifying the airplane’s weight
No: 2, 31700 Blagnac Cedex, France; approved the incorporation by reference
variant; and determining the applicable
telephone +33 5 61 93 36 96; fax +33 5 61 of certain publications listed in this AD
life limit for certain components
93 44 51; email account.airworth-eas@ as of November 5, 2018.
installed on the MLG, NLG, and CLG.
airbus.com; Internet http://www.airbus.com. ADDRESSES: For service information
identified in this final rule, contact We are issuing this AD to address
(6) You may view this service information
Airbus SAS, Airworthiness Office— certain parts made from 300M high
at the FAA, Transport Standards Branch,
2200 South 216th St., Des Moines, WA. For EAL, Rond-Point Emile Dewoitine No: strength steel, which if uncorrected,
information on the availability of this 2, 31700 Blagnac Cedex, France; could lead to structural failure of the
material at the FAA, call 206–231–3195. telephone +33 5 61 93 36 96; fax +33 5 landing gear, and possible loss of
(7) You may view this service information 61 93 45 80; email airworthiness.A330- control of the airplane during take-off or
that is incorporated by reference at the A340@airbus.com; internet http:// landing.
National Archives and Records www.airbus.com. You may view this The European Aviation Safety Agency
Administration (NARA). For information on service information at the FAA, (EASA), which is the Technical Agent
the availability of this material at NARA, call Transport Standards Branch, 2200 for the Member States of the European
202–741–6030, or go to: http:// South 216th St., Des Moines, WA. For Union, has issued EASA AD 2017–0185,
www.archives.gov/federal-register/cfr/ibr- information on the availability of this dated September 22, 2017 (referred to
locations.html. material at the FAA, call 206–231–3195. after this as the Mandatory Continuing
It is also available on the internet at Airworthiness Information, or ‘‘the
Issued in Des Moines, Washington, on
MCAI’’), to correct an unsafe condition
amozie on DSK3GDR082PROD with RULES
September 21, 2018. http://www.regulations.gov by searching
for and locating Docket No. FAA–2018– for all Airbus SAS Model A330–200
John P. Piccola, Freighter series airplanes, Model A330–
0395.
Acting Director, System Oversight Division, 200 series airplanes, Model A330–300
Aircraft Certification Service. Examining the AD Docket series airplanes, Model A340–200 series
[FR Doc. 2018–21100 Filed 9–28–18; 8:45 am] You may examine the AD docket on airplanes, Model A340–300 series
BILLING CODE 4910–13–P the internet at http:// airplanes, Model A340–500 series
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Document Created: 2018-09-29 04:26:09
Document Modified: 2018-09-29 04:26:09
| 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 November 5, 2018. | |
| 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. | |
| FR Citation | 83 FR 49265 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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