82 FR 58718 - Airworthiness Directives; Airbus Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 82, Issue 239 (December 14, 2017)
Federal Aviation Administration
Federal Register Volume 82, Issue 239 (December 14, 2017)
| Page Range | 58718-58722 | |
| FR Document | 2017-26842 |
[Federal Register Volume 82, Number 239 (Thursday, December 14, 2017)] [Rules and Regulations] [Pages 58718-58722] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2017-26842] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2017-1104; Product Identifier 2017-NM-153-AD; Amendment 39-19130; AD 2017-25-16] RIN 2120-AA64 Airworthiness Directives; Airbus Airplanes AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for all Airbus Model A330-200, A330-200 [[Page 58719]] Freighter, and A330-300 series airplanes; and Airbus Model A340-200, A340-300, A340-500, and A340-600 series airplanes. This AD requires repetitive inspections of certain fuel pumps for cavitation erosion, corrective action if necessary, and revision of the minimum equipment list (MEL). This AD was prompted by a report indicating that a fuel pump showing cavitation erosion breached the fuel pump housing and exposed the fuel pump power supply wires. We are issuing this AD to address the unsafe condition on these products. DATES: This AD becomes effective December 29, 2017. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of December 29, 2017. We must receive comments on this AD by January 29, 2018. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods:Federal eRulemaking Portal: Go to http://www.regulations.gov. Follow the instructions for submitting comments. Fax: 202-493-2251. Mail: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590. Hand Delivery: U.S. Department of Transportation, Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New Jersey Avenue SE, Washington, DC, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service information identified in this final rule, contact Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +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 referenced service information at the FAA, Transport Standards Branch, 1601 Lind Avenue SW, Renton, WA. For information on the availability of this material at the FAA, call 425- 227-1221. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017- 1104. 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-2017- 1104; or in person at the Docket Operations office between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received, and other information. The street address for the Docket Operations office (telephone 800-647-5527) is in the ADDRESSES section. Comments will be available in the AD docket shortly after receipt. FOR FURTHER INFORMATION CONTACT: Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone 425-227-1138; fax 425-227- 1149. SUPPLEMENTARY INFORMATION: Discussion The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA Airworthiness Directive 2017-0224, dated November 10, 2017 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for all Airbus Model A330-200, A330-200 Freighter, and A330-300 series airplanes; and Airbus Model A340-200, A340-300, A340-500, and A340-600 series airplanes. The MCAI states: An occurrence was reported of a fuel pump showing cavitation erosion which breached the fuel pump housing through the inlet webs and exposed the fuel pump power supply wires. Inspections accomplished on fuel pumps removed from other aeroplanes identified signs of erosion in varying degrees. However, no other instance of break-through due to cavitation erosion was found. A list of potentially affected fuel pump Part Numbers (P/N) was established. This condition, if not detected and corrected, could result, in case the pump is running dry, in an ignition source in the fuel tank, which may result in a fuel tank explosion and consequent loss of the aeroplane. To address this potential unsafe condition, Airbus issued Alert Operators Transmission (AOT) A28L006-17 to provide instructions to inspect some fuel pumps when installed at specific positions, and to update the applicable Master Minimum Equipment List (MMEL). For the reasons described above, this [EASA] AD requires repetitive inspections of these fuel pumps and, depending on findings, replacement of damaged fuel pumps with serviceable parts. This [EASA] AD also requires an update of the applicable MMEL, and the reporting of inspection results to Airbus. This [EASA] AD is considered to be an interim measure and further [EASA] AD action may follow. Although the MCAI requires updating the ``master minimum equipment list (MMEL),'' this AD requires revising the ``minimum equipment list (MEL).'' The MMEL is a master list of the minimum equipment that the airplane can operate with under given circumstances. A MEL is derived from the MMEL and is tailored for individual operators. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-1104. Related Service Information Under 1 CFR Part 51 Airbus has issued Alert Operators Transmission A28L006-17, Rev. 00, dated November 3, 2017. The service information describes procedures for inspection of certain fuel pumps for cavitation erosion, and corrective actions. The service information also describes dispatch restrictions that affect the MEL. This service information is reasonably available because the interested parties have access to it through their normal course of business or by the means identified in the ADDRESSES section. FAA's Determination and Requirements of This AD This product has been approved by the aviation authority of another country, and is approved for operation in the United States. Pursuant to our bilateral agreement with the State of Design Authority, we have been notified of the unsafe condition described in the MCAI and service information referenced above. We are issuing this AD because we evaluated all pertinent information and determined the unsafe condition exists and is likely to exist or develop on other products of these same type designs. FAA's Determination of the Effective Date An unsafe condition exists that requires the immediate adoption of this AD. The FAA has found that the risk to the flying public justifies waiving notice and comment prior to adoption of this rule because the unsafe condition could result in an ignition source in the fuel tank, which could result in a fuel tank explosion. Therefore, we determined that notice and opportunity for public comment before issuing this AD are impracticable and that good cause exists for making this amendment effective in fewer than 30 days. Comments Invited This AD is a final rule that involves requirements affecting flight safety, and we did not precede it by notice and opportunity for public comment. We invite you to send any written relevant [[Page 58720]] data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ``Docket No. FAA- 2017-1104; Product Identifier 2017-NM-153-AD'' at the beginning of your comments. We specifically invite comments on the overall regulatory, economic, environmental, and energy aspects of this AD. We will consider all comments received by the closing date and may amend this AD based on those comments. We will post all comments we receive, without change, to http://www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Costs of Compliance We estimate that this AD affects 107 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 ---------------------------------------------------------------------------------------------------------------- Inspection................. 4 work-hours x $85 per $0 $340 per inspection $36,380 per hour = $340 per cycle. inspection cycle. inspection cycle. Reporting.................. 1 work-hour x $85 per 0 $85 per inspection $9,095 per hour = $85 per cycle. inspection cycle. inspection cycle. MEL revision............... 1 work-hour x $85 per 0 $85................ $9,095. hour = $85. ---------------------------------------------------------------------------------------------------------------- We estimate the following costs to do any necessary replacements that would be required based on the results of the inspection. We have no way of determining the number of aircraft that might need these replacements: On-Condition Costs ---------------------------------------------------------------------------------------------------------------- Cost per Action Labor cost Parts cost product ---------------------------------------------------------------------------------------------------------------- Replacement................................ 2 work-hours x $85 per hour = $170. $8,000 $8,170 ---------------------------------------------------------------------------------------------------------------- Paperwork Reduction Act A federal agency may not conduct or sponsor, and a person is not required to respond to, nor shall a person be subject to penalty for failure to comply with a collection of information subject to the requirements of the Paperwork Reduction Act unless that collection of information displays a current valid OMB control number. The control number for the collection of information required by this AD is 2120- 0056. The paperwork cost associated with this AD has been detailed in the Costs of Compliance section of this document and includes time for reviewing instructions, as well as completing and reviewing the collection of information. Therefore, all reporting associated with this AD is mandatory. Comments concerning the accuracy of this burden and suggestions for reducing the burden should be directed to the FAA at 800 Independence Ave. SW, Washington, DC 20591, ATTN: Information Collection Clearance Officer, AES-200. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. ``Subtitle VII: Aviation Programs,'' describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in ``Subtitle VII, Part A, Subpart III, Section 44701: General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes to the Director of the System Oversight Division. Regulatory Findings We determined that this AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: 1. Is not a ``significant regulatory action'' under Executive Order 12866; 2. Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979); 3. Will not affect intrastate aviation in Alaska; and 4. Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. 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. [[Page 58721]] Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2017-25-16 Airbus: Amendment 39-19130; Docket No. FAA-2017-1104; Product Identifier 2017-NM-153-AD. (a) Effective Date This AD becomes effective December 29, 2017. (b) Affected ADs None. (c) Applicability This AD applies to the Airbus airplanes identified in paragraphs (c)(1) through (c)(7) of this AD, certificated in any category, all manufacturer serial numbers. (1) Model A330-223F and -243F airplanes. (2) Model A330-201, -202, -203, -223, and -243 airplanes. (3) Model A330-301, -302, -303, -321, -322, -323, -341, -342, and -343 airplanes. (4) Model A340-211, -212, and -213 airplanes. (5) Model A340-311, -312, and -313 airplanes. (6) Model A340-541 airplanes. (7) Model A340-642 airplanes. (d) Subject Air Transport Association (ATA) of America Code 28, Fuel System. (e) Reason This AD was prompted by a report indicating that a fuel pump showing cavitation erosion breached the fuel pump housing and exposed the fuel pump power supply wires. We are issuing this AD to detect and correct cavitation erosion of certain fuel pumps, which could result, if the pump is running dry, in an ignition source in the fuel tank, and consequent fuel tank explosion. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Definition of Affected Fuel Pump (1) For the purpose of this AD, an affected fuel pump has part number (P/N) 568-1-28300-101, P/N 568-1-28300-103, or P/N 568-1- 28300-200, and is located at one of the positions specified in paragraph 3.3 of Airbus Alert Operators Transmission (AOT) A28L006- 17, Rev. 00, dated November 3, 2017. (2) A fuel pump having P/N 568-1-28300-101, P/N 568-1-28300-103, or P/N 568-1-28300-200 that is installed in locations other than those specified in paragraph 3.3 of Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017, is not affected by the inspection requirements of paragraph (i) of this AD. (h) Airplane Group Designations For the purpose of this AD, airplane groups are designated as specified in paragraphs (h)(1) and (h)(2) of this AD. (1) Group 1 airplanes are equipped with an affected fuel pump. (2) Group 2 airplanes are not equipped with an affected fuel pump. (i) Inspections For Group 1 airplanes: Before an affected pump exceeds 10,000 flight hours since first installation on an airplane, or the applicable time specified in paragraph (i)(1) or (i)(2) of this AD, whichever occurs later, inspect all affected fuel pumps for cavitation erosion, in accordance with the instruction of Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017. Repeat the inspection thereafter at intervals not to exceed the applicable time specified in table 1 to paragraph (i) of this AD. (1) For a center tank, rear center tank, or aft transfer fuel pump: Within 30 days after the effective date of this AD. (2) For a stand-by fuel pump: Within 40 days after the effective date of this AD. Table 1 to Paragraph (i) of This AD--Repetitive Inspection Intervals ------------------------------------------------------------------------ Inspection Erosion--as defined in the AOT interval in flight hours ------------------------------------------------------------------------ No erosion.............................................. 5,000 Case 1: Light erosion................................... 5,000 Case 2: Medium erosion.................................. 800 ------------------------------------------------------------------------ (j) Corrective Actions If, during any inspection required by paragraph (i) of this AD, severe erosion (Case 3), as specified in Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017, is found on a fuel pump: Before further flight, replace that fuel pump with a serviceable part, or deactivate that fuel pump as specified in the minimum equipment list (MEL), in accordance with the instructions of Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017. (k) Part Installation Limitations (1) As of the effective date of this AD, a fuel pump having P/N 568-1-28300-101, P/N 568-1-28300-103, or P/N 568-1-28300-200 may be installed on an airplane, provided that the part is new, or, prior to installation, the part has passed the inspection (no erosion or Case 1: Light erosion) required by paragraph (i) of this AD and, following installation, the part is inspected within the applicable repetitive intervals and as required by paragraph (i) of this AD. (2) As of the effective date of this AD, a fuel pump having P/N 568-1-28300-101, P/N 568-1-28300-103, or P/N 568-1-28300-200, with Case 2 (medium erosion), as specified in Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017, may be installed on an airplane provided the fuel pump is not installed at a location specified in paragraph 3.3 of Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017. (l) MEL Revision (1) Within 30 days after the effective date of this AD, revise the applicable MEL, in accordance with the instructions of Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017, and thereafter operate the airplane accordingly. (2) For Model A340-500 and A340-600 airplanes: In addition to the MEL revision required by paragraph (l)(1) of this AD, revise the applicable MEL to include the information specified in table 2 to paragraph (l)(2) of this AD, and thereafter operate the airplane accordingly. Table 2 to Paragraph (l)(2) of This AD--Amendment to MEL Items 28-27-06 and 28-27-07 ------------------------------------------------------------------------ Applicability MEL amendment ------------------------------------------------------------------------ Model A340-500 and A340-600 MEL Items 28-27-06 and 28-27-07 can be series airplanes. applied, provided that the related circuit breaker is pulled and tagged for the duration of the MEL item. ------------------------------------------------------------------------ (m) Reporting At the applicable time specified in paragraph (m)(1) or (m)(2) of this AD: Report the results (including no findings) of each inspection required by paragraph (i) of this AD to [email protected], in accordance with the instructions in Airbus AOT A28L006-17, Rev. 00, dated November 3, 2017. (1) If the inspection was done on or before the effective date of this AD: Report within 10 days after the effective date of this AD. (2) If the inspection was done after the effective date of this AD: Report within 10 days after the inspection. (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 Section, send it to the attention of the person identified in [[Page 58722]] 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 the European Aviation Safety Agency (EASA); or Airbus's EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA- authorized signature. (o) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2017-0224, dated November 10, 2017, for related information. You may examine the MCAI on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2017-1104. (2) For more information about this AD, contact Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone 425-227-1138; fax 425-227-1149. (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 Alert Operators Transmission A28L006-17, Rev. 00, dated November 3, 2017. (ii) Reserved. (3) For service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAL, 1 Rond Point Maurice Bellonte, 31707 Blagnac Cedex, France; telephone +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, 1601 Lind Avenue SW, Renton, WA. For information on the availability of this material at the FAA, call 425-227-1221. (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 Renton, Washington, on December 4, 2017. Dionne Palermo, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2017-26842 Filed 12-13-17; 8:45 am] BILLING CODE 4910-13-P
![58718 Federal Register / Vol. 82, No. 239 / Thursday, December 14, 2017 / Rules and Regulations
(1) For Model A300 series airplanes: (l) Other FAA AD Provisions (vi) Airbus Service Bulletin A300–28–
Airbus Service Bulletin A300–28–0092, The following provisions also apply to this 6114, Revision 00, dated January 9, 2017.
Revision 01, dated August 29, 2014 (for AD: (vii) Airbus Service Bulletin A310–28–
center and wing-inner tank fuel pump (1) Alternative Methods of Compliance 2173, Revision 03, dated December 16, 2016.
canister hood halves); and Airbus Service (AMOCs): The Manager, International (viii) Airbus Service Bulletin A310–28–
Bulletin A300–28–0094, Revision 00, dated Section, Transport Standards Branch, FAA, 2175, Revision 01, dated August 29, 2014.
January 9, 2017 (for wing-outer tank fuel has the authority to approve AMOCs for this (ix) Airbus Service Bulletin A310–28–
pump canister hood halves). AD, if requested using the procedures found 2178, Revision 00, dated January 9, 2017.
(2) For Model A300–600 series airplanes: in 14 CFR 39.19. In accordance with 14 CFR (4) The following service information was
Airbus Service Bulletin A300–28–6110, 39.19, send your request to your principal approved for IBR on November 27, 2012 (77
inspector or local Flight Standards District FR 64701, October 23, 2012).
Revision 01, dated August 29, 2014 (for
Office, as appropriate. If sending information (i) Airbus Mandatory Service Bulletin
center and wing-inner tank fuel pump
directly to the International Section, send it A300–28–0089, Revision 01, including
canister hood halves); and Airbus Service Inspection Findings—Reporting Sheet, dated
Bulletin A300–28–6114, Revision 00, dated to the attention of the person identified in
paragraph (m)(2) of this AD. Information may April 15, 2011.
January 9, 2017 (for wing-outer tank and trim (ii) Airbus Mandatory Service Bulletin
be emailed to: 9-ANM-116-AMOC-
tank fuel pump canister hood halves). A300–28–6106, Revision 01, including
REQUESTS@faa.gov.
(3) For Model A310 series airplanes: (i) Before using any approved AMOC, Inspection Findings—Reporting Sheet, dated
Airbus Service Bulletin A310–28–2175, notify your appropriate principal inspector, April 15, 2011.
Revision 01, dated August 29, 2014 (for or lacking a principal inspector, the manager (iii) Airbus Mandatory Service Bulletin
center and wing-inner tank fuel pump of the local flight standards district office/ A310–28–2173, Revision 01, including
canister hood halves); and Airbus Service certificate holding district office. Inspection Findings—Reporting Sheet, dated
Bulletin A310–28–2178, Revision 00, dated (ii) AMOCs approved previously for AD April 15, 2011.
January 9, 2017 (for wing-outer tank and trim 2012–21–04 are not approved as AMOCs (5) For service information identified in
tank fuel pump canister hood halves). with this AD. this AD, contact Airbus SAS, Airworthiness
(2) Contacting the Manufacturer: As of the Office—EAW, 1 Rond Point Maurice
(k) Credit for Previous Actions effective date of this AD, for any requirement Bellonte, 31707 Blagnac Cedex, France;
(1) This paragraph provides credit for the in this AD to obtain corrective actions from telephone: +33 5 61 93 36 96; fax: +33 5 61
actions required by paragraph (g) of this AD, a manufacturer, the action must be 93 44 51; email: account.airworth-eas@
if those actions were performed before the accomplished using a method approved by airbus.com; internet: http://www.airbus.com.
effective date of this AD using the applicable the Manager, International Section, Transport (6) You may view this service information
service information specified in paragraph Standards Branch, FAA; or the European at the FAA, Transport Standards Branch,
(k)(1)(i), (k)(1)(ii), or (k)(1)(iii) of this AD. Aviation Safety Agency (EASA); or Airbus’s 1601 Lind Avenue SW, Renton, WA. For
(i) Airbus Service Bulletin A300–28–0089, EASA Design Organization Approval (DOA). information on the availability of this
dated January 13, 2011; or Airbus Service If approved by the DOA, the approval must material at the FAA, call 425–227–1221.
Bulletin A300–28–0089, Revision 02, dated include the DOA-authorized signature. (7) You may view this service information
April 25, 2014. that is incorporated by reference at the
(m) Related Information
(ii) Airbus Service Bulletin A300–28–6106, National Archives and Records
(1) Refer to Mandatory Continuing Administration (NARA). For information on
dated January 13, 2011; or Airbus Service Airworthiness Information (MCAI) EASA AD the availability of this material at NARA, call
Bulletin A300–28–6106, Revision 02, dated 2017–0051, dated March 23, 2017, for related 202–741–6030, or go to: http://
April 25, 2014. information. This MCAI may be found in the www.archives.gov/federal-register/cfr/ibr-
(iii) Airbus Service Bulletin A310–28– AD docket on the internet at http:// locations.html.
2173, dated January 13, 2011; or Airbus www.regulations.gov by searching for and
Service Bulletin A310–28–2173, Revision 02, locating Docket No. FAA–2017–0714. Issued in Renton, Washington, on
dated April 25, 2014. (2) For more information about this AD, December 4, 2017.
(2) This paragraph provides credit for the contact Dan Rodina, Aerospace Engineer, Dionne Palermo,
actions required by paragraph (h) of this AD, International Section, Transport Standards Acting Director, System Oversight Division,
if those actions were performed before the Branch, FAA, 1601 Lind Avenue SW, Aircraft Certification Service.
effective date of this AD using the applicable Renton, WA 98057–3356; telephone 425–
[FR Doc. 2017–26627 Filed 12–13–17; 8:45 am]
service information specified in paragraph 227–2125; fax 425–227–1149.
(3) Service information identified in this BILLING CODE 4910–13–P
(k)(2)(i), (k)(2)(ii), or (k)(2)(iii) of this AD.
(i) Airbus Service Bulletin A300–28–0089, AD that is not incorporated by reference is
dated January 13, 2011; Airbus Mandatory available at the addresses specified in
Service Bulletin A300–28–0089, Revision 01, paragraphs (n)(5) and (n)(6) of this AD. DEPARTMENT OF TRANSPORTATION
dated April 15, 2011; or Airbus Service (n) Material Incorporated by Reference
Bulletin A300–28–0089, Revision 02, dated Federal Aviation Administration
April 25, 2014. (1) The Director of the Federal Register
(ii) Airbus Service Bulletin A300–28–6106, approved the incorporation by reference 14 CFR Part 39
(IBR) of the service information listed in this
dated January 13, 2011; Airbus Mandatory [Docket No. FAA–2017–1104; Product
paragraph under 5 U.S.C. 552(a) and 1 CFR
Service Bulletin A300–28–6106, Revision 01, Identifier 2017–NM–153–AD; Amendment
part 51.
dated April 15, 2011; or Airbus Service 39–19130; AD 2017–25–16]
(2) You must use this service information
Bulletin A300–28–6106, Revision 02, dated as applicable to do the actions required by
April 25, 2014. RIN 2120–AA64
this AD, unless this AD specifies otherwise.
(iii) Airbus Service Bulletin A310–28– (3) The following service information was
2173, dated January 13, 2011; Airbus approved for IBR on January 18, 2018. Airworthiness Directives; Airbus
Mandatory Service Bulletin A310–28–2173, (i) Airbus Service Bulletin A300–28–0089, Airplanes
Revision 01, dated April 15, 2011; or Airbus Revision 03, dated December 16, 2016. AGENCY: Federal Aviation
sradovich on DSK3GMQ082PROD with RULES
Service Bulletin A310–28–2173, Revision 02, (ii) Airbus Service Bulletin A300–28–0092,
dated April 25, 2014. Revision 01, dated August 29, 2014.
Administration (FAA), DOT.
(3) This paragraph provides credit for the (iii) Airbus Service Bulletin A300–28– ACTION: Final rule; request for
actions specified in paragraph (j) of this AD, 0094, Revision 00, dated January 9, 2017. comments.
if those actions were performed before the (iv) Airbus Service Bulletin A300–28–
effective date of this AD using Airbus Service 6106, Revision 03, dated December 16, 2016. SUMMARY: We are adopting a new
Bulletin A300–28–6110, Revision 00, dated (v) Airbus Service Bulletin A300–28–6110, airworthiness directive (AD) for all
November 28, 2013. Revision 01, dated August 29, 2014. Airbus Model A330–200, A330–200
VerDate Sep<11>2014 15:57 Dec 13, 2017 Jkt 244001 PO 00000 Frm 00012 Fmt 4700 Sfmt 4700 E:\FR\FM\14DER1.SGM 14DER1](https://thefederalregister.org/doc/82_FR_58957/page/1.svg)
![Federal Register / Vol. 82, No. 239 / Thursday, December 14, 2017 / Rules and Regulations 58719
Freighter, and A330–300 series Operations office between 9 a.m. and 5 (MMEL),’’ this AD requires revising the
airplanes; and Airbus Model A340–200, p.m., Monday through Friday, except ‘‘minimum equipment list (MEL).’’ The
A340–300, A340–500, and A340–600 Federal holidays. The AD docket MMEL is a master list of the minimum
series airplanes. This AD requires contains this AD, the regulatory equipment that the airplane can operate
repetitive inspections of certain fuel evaluation, any comments received, and with under given circumstances. A MEL
pumps for cavitation erosion, corrective other information. The street address for is derived from the MMEL and is
action if necessary, and revision of the the Docket Operations office (telephone tailored for individual operators. You
minimum equipment list (MEL). This 800–647–5527) is in the ADDRESSES may examine the MCAI on the internet
AD was prompted by a report indicating section. Comments will be available in at http://www.regulations.gov by
that a fuel pump showing cavitation the AD docket shortly after receipt. searching for and locating Docket No.
erosion breached the fuel pump housing FOR FURTHER INFORMATION CONTACT: FAA–2017–1104.
and exposed the fuel pump power Vladimir Ulyanov, Aerospace Engineer, Related Service Information Under 1
supply wires. We are issuing this AD to International Section, Transport CFR Part 51
address the unsafe condition on these Standards Branch, FAA, 1601 Lind
products. Avenue SW, Renton, WA 98057–3356; Airbus has issued Alert Operators
telephone 425–227–1138; fax 425–227– Transmission A28L006–17, Rev. 00,
DATES: This AD becomes effective dated November 3, 2017. The service
December 29, 2017. 1149.
SUPPLEMENTARY INFORMATION:
information describes procedures for
The Director of the Federal Register
inspection of certain fuel pumps for
approved the incorporation by reference Discussion cavitation erosion, and corrective
of a certain publication listed in this AD
The European Aviation Safety Agency actions. The service information also
as of December 29, 2017.
(EASA), which is the Technical Agent describes dispatch restrictions that
We must receive comments on this
for the Member States of the European affect the MEL. This service information
AD by January 29, 2018.
Union, has issued EASA Airworthiness is reasonably available because the
ADDRESSES: You may send comments, interested parties have access to it
using the procedures found in 14 CFR Directive 2017–0224, dated November
10, 2017 (referred to after this as the through their normal course of business
11.43 and 11.45, by any of the following or by the means identified in the
methods: Mandatory Continuing Airworthiness
Information, or ‘‘the MCAI’’), to correct ADDRESSES section.
• Federal eRulemaking Portal: Go to
http://www.regulations.gov. Follow the an unsafe condition for all Airbus FAA’s Determination and Requirements
instructions for submitting comments. Model A330–200, A330–200 Freighter, of This AD
• Fax: 202–493–2251. and A330–300 series airplanes; and
Airbus Model A340–200, A340–300, This product has been approved by
• Mail: U.S. Department of the aviation authority of another
Transportation, Docket Operations, M– A340–500, and A340–600 series
airplanes. The MCAI states: country, and is approved for operation
30, West Building Ground Floor, Room in the United States. Pursuant to our
W12–140, 1200 New Jersey Avenue SE, An occurrence was reported of a fuel pump bilateral agreement with the State of
Washington, DC 20590. showing cavitation erosion which breached Design Authority, we have been notified
• Hand Delivery: U.S. Department of the fuel pump housing through the inlet
of the unsafe condition described in the
Transportation, Docket Operations, M– webs and exposed the fuel pump power
supply wires. Inspections accomplished on MCAI and service information
30, West Building Ground Floor, Room fuel pumps removed from other aeroplanes referenced above. We are issuing this
W12–140, 1200 New Jersey Avenue SE, identified signs of erosion in varying degrees. AD because we evaluated all pertinent
Washington, DC, between 9 a.m. and 5 However, no other instance of break-through information and determined the unsafe
p.m., Monday through Friday, except due to cavitation erosion was found. A list condition exists and is likely to exist or
Federal holidays. of potentially affected fuel pump Part develop on other products of these same
For service information identified in Numbers (P/N) was established. type designs.
this final rule, contact Airbus SAS, This condition, if not detected and
Airworthiness Office—EAL, 1 Rond corrected, could result, in case the pump is FAA’s Determination of the Effective
Point Maurice Bellonte, 31707 Blagnac running dry, in an ignition source in the fuel Date
tank, which may result in a fuel tank
Cedex, France; telephone +33 5 61 93 36 explosion and consequent loss of the An unsafe condition exists that
96; fax +33 5 61 93 45 80; email aeroplane. requires the immediate adoption of this
airworthiness.A330-A340@airbus.com; To address this potential unsafe condition, AD. The FAA has found that the risk to
internet http://www.airbus.com. You Airbus issued Alert Operators Transmission the flying public justifies waiving notice
may view this referenced service (AOT) A28L006–17 to provide instructions to and comment prior to adoption of this
information at the FAA, Transport inspect some fuel pumps when installed at rule because the unsafe condition could
Standards Branch, 1601 Lind Avenue specific positions, and to update the result in an ignition source in the fuel
SW, Renton, WA. For information on applicable Master Minimum Equipment List tank, which could result in a fuel tank
the availability of this material at the (MMEL).
explosion. Therefore, we determined
For the reasons described above, this
FAA, call 425–227–1221. It is also [EASA] AD requires repetitive inspections of that notice and opportunity for public
available on the internet at http:// these fuel pumps and, depending on comment before issuing this AD are
www.regulations.gov by searching for findings, replacement of damaged fuel impracticable and that good cause exists
and locating Docket No. FAA–2017– pumps with serviceable parts. This [EASA] for making this amendment effective in
1104. AD also requires an update of the applicable fewer than 30 days.
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MMEL, and the reporting of inspection
Examining the AD Docket results to Airbus. Comments Invited
You may examine the AD docket on This [EASA] AD is considered to be an This AD is a final rule that involves
the internet at http:// interim measure and further [EASA] AD requirements affecting flight safety, and
www.regulations.gov by searching for action may follow. we did not precede it by notice and
and locating Docket No. FAA–2017– Although the MCAI requires updating opportunity for public comment. We
1104; or in person at the Docket the ‘‘master minimum equipment list invite you to send any written relevant
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![Federal Register / Vol. 82, No. 239 / Thursday, December 14, 2017 / Rules and Regulations 58721
§ 39.13 [Amended] 28300–101, P/N 568–1–28300–103, or P/N (j) Corrective Actions
568–1–28300–200, and is located at one of
■ 2. The FAA amends § 39.13 by adding If, during any inspection required by
the positions specified in paragraph 3.3 of
the following new airworthiness Airbus Alert Operators Transmission (AOT)
paragraph (i) of this AD, severe erosion (Case
directive (AD): A28L006–17, Rev. 00, dated November 3, 3), as specified in Airbus AOT A28L006–17,
2017–25–16 Airbus: Amendment 39–19130; 2017. Rev. 00, dated November 3, 2017, is found on
Docket No. FAA–2017–1104; Product (2) A fuel pump having P/N 568–1–28300– a fuel pump: Before further flight, replace
Identifier 2017–NM–153–AD. 101, P/N 568–1–28300–103, or P/N 568–1– that fuel pump with a serviceable part, or
28300–200 that is installed in locations other deactivate that fuel pump as specified in the
(a) Effective Date
than those specified in paragraph 3.3 of minimum equipment list (MEL), in
This AD becomes effective December 29, Airbus AOT A28L006–17, Rev. 00, dated accordance with the instructions of Airbus
2017. November 3, 2017, is not affected by the AOT A28L006–17, Rev. 00, dated November
(b) Affected ADs inspection requirements of paragraph (i) of 3, 2017.
this AD.
None. (k) Part Installation Limitations
(h) Airplane Group Designations
(c) Applicability (1) As of the effective date of this AD, a
For the purpose of this AD, airplane groups fuel pump having P/N 568–1–28300–101, P/
This AD applies to the Airbus airplanes
are designated as specified in paragraphs
identified in paragraphs (c)(1) through (c)(7) N 568–1–28300–103, or P/N 568–1–28300–
(h)(1) and (h)(2) of this AD.
of this AD, certificated in any category, all 200 may be installed on an airplane,
manufacturer serial numbers. (1) Group 1 airplanes are equipped with an
affected fuel pump. provided that the part is new, or, prior to
(1) Model A330–223F and –243F airplanes. installation, the part has passed the
(2) Model A330–201, –202, –203, –223, and (2) Group 2 airplanes are not equipped
with an affected fuel pump. inspection (no erosion or Case 1: Light
–243 airplanes.
(3) Model A330–301, –302, –303, –321, erosion) required by paragraph (i) of this AD
(i) Inspections and, following installation, the part is
–322, –323, –341, –342, and –343 airplanes.
(4) Model A340–211, –212, and –213 For Group 1 airplanes: Before an affected inspected within the applicable repetitive
airplanes. pump exceeds 10,000 flight hours since first intervals and as required by paragraph (i) of
(5) Model A340–311, –312, and –313 installation on an airplane, or the applicable this AD.
airplanes. time specified in paragraph (i)(1) or (i)(2) of (2) As of the effective date of this AD, a
(6) Model A340–541 airplanes. this AD, whichever occurs later, inspect all
fuel pump having P/N 568–1–28300–101, P/
(7) Model A340–642 airplanes. affected fuel pumps for cavitation erosion, in
N 568–1–28300–103, or P/N 568–1–28300–
accordance with the instruction of Airbus
(d) Subject AOT A28L006–17, Rev. 00, dated November 200, with Case 2 (medium erosion), as
Air Transport Association (ATA) of 3, 2017. Repeat the inspection thereafter at specified in Airbus AOT A28L006–17, Rev.
America Code 28, Fuel System. intervals not to exceed the applicable time 00, dated November 3, 2017, may be installed
specified in table 1 to paragraph (i) of this on an airplane provided the fuel pump is not
(e) Reason
AD. installed at a location specified in paragraph
This AD was prompted by a report (1) For a center tank, rear center tank, or 3.3 of Airbus AOT A28L006–17, Rev. 00,
indicating that a fuel pump showing aft transfer fuel pump: Within 30 days after dated November 3, 2017.
cavitation erosion breached the fuel pump the effective date of this AD.
housing and exposed the fuel pump power (2) For a stand-by fuel pump: Within 40 (l) MEL Revision
supply wires. We are issuing this AD to days after the effective date of this AD. (1) Within 30 days after the effective date
detect and correct cavitation erosion of
certain fuel pumps, which could result, if the of this AD, revise the applicable MEL, in
pump is running dry, in an ignition source TABLE 1 TO PARAGRAPH (i) OF THIS accordance with the instructions of Airbus
in the fuel tank, and consequent fuel tank AD—REPETITIVE INSPECTION INTER- AOT A28L006–17, Rev. 00, dated November
explosion. VALS 3, 2017, and thereafter operate the airplane
accordingly.
(f) Compliance
Inspection (2) For Model A340–500 and A340–600
Comply with this AD within the Erosion—as defined in the interval in airplanes: In addition to the MEL revision
compliance times specified, unless already AOT
flight hours required by paragraph (l)(1) of this AD, revise
done.
the applicable MEL to include the
(g) Definition of Affected Fuel Pump No erosion ............................ 5,000
information specified in table 2 to paragraph
Case 1: Light erosion ........... 5,000
(1) For the purpose of this AD, an affected Case 2: Medium erosion ...... 800 (l)(2) of this AD, and thereafter operate the
fuel pump has part number (P/N) 568–1– airplane accordingly.
TABLE 2 TO PARAGRAPH (l)(2) OF THIS AD—AMENDMENT TO MEL ITEMS 28–27–06 AND 28–27–07
Applicability MEL amendment
Model A340–500 and A340–600 series air- MEL Items 28–27–06 and 28–27–07 can be applied, provided that the related circuit breaker
planes. is pulled and tagged for the duration of the MEL item.
(m) Reporting (1) If the inspection was done on or before (1) Alternative Methods of Compliance
the effective date of this AD: Report within (AMOCs): The Manager, International
At the applicable time specified in
10 days after the effective date of this AD. Section, Transport Standards Branch, FAA,
paragraph (m)(1) or (m)(2) of this AD: Report
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(2) If the inspection was done after the has the authority to approve AMOCs for this
the results (including no findings) of each AD, if requested using the procedures found
inspection required by paragraph (i) of this effective date of this AD: Report within 10
in 14 CFR 39.19. In accordance with 14 CFR
AD to inspection.results@airbus.com, in days after the inspection. 39.19, send your request to your principal
accordance with the instructions in Airbus (n) Other FAA AD Provisions inspector or local Flight Standards District
AOT A28L006–17, Rev. 00, dated November Office, as appropriate. If sending information
The following provisions also apply to this directly to the International Section, send it
3, 2017.
AD: to the attention of the person identified in
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![58722 Federal Register / Vol. 82, No. 239 / Thursday, December 14, 2017 / Rules and Regulations
paragraph (o)(2) of this AD. Information may DEPARTMENT OF TRANSPORTATION I. Executive Summary
be emailed to: 9-ANM-116-AMOC-
REQUESTS@faa.gov. Before using any This action amends the prohibition of
Federal Aviation Administration flight operations in specified areas of
approved AMOC, notify your appropriate
principal inspector, or lacking a principal the Sanaa (OYSC) FIR by all: U.S. air
inspector, the manager of the local flight
14 CFR Part 91 carriers; U.S. commercial operators;
standards district office/certificate holding persons exercising the privileges of an
district office. [Docket No.: FAA–2015–8672; Amdt. No. airman certificate issued by the FAA,
(2) Contacting the Manufacturer: For any 91–340A] except when such persons are operating
requirement in this AD to obtain corrective U.S.-registered aircraft for a foreign air
actions from a manufacturer, the action must
be accomplished using a method approved
RIN 2120–AL27 carrier; and operators of U.S.-registered
by the Manager, International Section, civil aircraft, except where the operator
Transport Standards Branch, FAA; or the Amendment of the Prohibition Against of such aircraft is a foreign air carrier.
European Aviation Safety Agency (EASA); or Certain Flights in Specified Areas of Due to a reduction in the level of risk
Airbus’s EASA Design Organization the Sanaa (OYSC) Flight Information to U.S. civil aviation operating in
Approval (DOA). If approved by the DOA, Region limited portions of the specified areas of
the approval must include the DOA- the Sanaa (OYSC) FIR where the FAA
authorized signature. AGENCY: Federal Aviation had prohibited U.S. civil aviation
Administration (FAA), Department of operations under SFAR No. 115, title 14
(o) Related Information
Transportation (DOT). Code of Federal Regulations (CFR)
(1) Refer to Mandatory Continuing
Airworthiness Information (MCAI) EASA ACTION: Final rule. 91.1611, this action amends SFAR No.
Airworthiness Directive 2017–0224, dated 115, § 91.1611, to reduce the amount of
November 10, 2017, for related information. SUMMARY: This action amends the airspace in the Sanaa (OYSC) FIR in
You may examine the MCAI on the internet Special Federal Aviation Regulation which U.S. civil aviation operations are
at http://www.regulations.gov by searching (SFAR) that prohibits certain flights in prohibited. Specifically, the FAA is
for and locating Docket No. FAA–2017–1104. specified areas of the Sanaa (OYSC) revising SFAR No. 115, § 91.1611, to
(2) For more information about this AD, prohibit U.S. civil aviation operations in
Flight Information Region (FIR) by all:
contact Vladimir Ulyanov, Aerospace
Engineer, International Section, Transport United States (U.S.) air carriers; U.S. the Sanaa (OYSC) FIR, except that
Standards Branch, FAA, 1601 Lind Avenue commercial operators; persons airspace east of a line drawn direct from
SW, Renton, WA 98057–3356; telephone exercising the privileges of an airman KAPET (163322N 0530614E) to NODMA
425–227–1138; fax 425–227–1149. certificate issued by the FAA, except (152603N 0533359E), southeast of a line
when such persons are operating U.S.- drawn direct from NODMA to ORBAT
(p) Material Incorporated by Reference
registered aircraft for a foreign air (140638N 0503924E) then from ORBAT
(1) The Director of the Federal Register carrier; and operators of U.S.-registered to PAKER (115500N 0463500E), south of
approved the incorporation by reference a line drawn direct from PAKER to
civil aircraft, except where the operator
(IBR) of the service information listed in this
of such aircraft is a foreign air carrier. PARIM (123142N 0432712E), and west
paragraph under 5 U.S.C. 552(a) and 1 CFR
part 51. There has been a reduction in the level of a line drawn direct from PARIM to
(2) You must use this service information of risk to U.S. civil aviation operations RIBOK (154700N 0415230E). However,
as applicable to do the actions required by in limited portions of the specified areas there continues to be an unacceptable
this AD, unless this AD specifies otherwise. of the Sanaa (OYSC) Flight Information level of risk to U.S. civil aviation
(i) Airbus Alert Operators Transmission region (FIR) where the FAA had operations in the remainder the
A28L006–17, Rev. 00, dated November 3, prohibited flight operations under the specified areas of the Sanaa (OYSC) FIR,
2017. SFAR. As a result, the FAA is reducing as described in this rule, resulting from
(ii) Reserved. terrorist and militant activity.
the amount of airspace in the Sanaa
(3) For service information identified in Consequently, the FAA is also
this AD, contact Airbus SAS, Airworthiness (OYSC) FIR in which U.S. civil aviation
operations are prohibited. However, amending this SFAR to extend its
Office—EAL, 1 Rond Point Maurice Bellonte,
31707 Blagnac Cedex, France; telephone +33 there continues to be an unacceptable expiration date until January 7, 2020.
5 61 93 36 96; fax +33 5 61 93 45 80; email level of risk to U.S. civil aviation The FAA finds this action necessary due
airworthiness.A330-A340@airbus.com; operations in the remainder of the to continued hazards to U.S. civil
internet http://www.airbus.com. specified areas of the Sanaa (OYSC) FIR, aviation operations in these areas.
(4) You may view this service information as described in this rule, resulting from
at the FAA, Transport Standards Branch, II. Legal Authority and Good Cause
terrorist and militant activity.
1601 Lind Avenue SW, Renton, WA. For A. Legal Authority
Consequently, the FAA is also
information on the availability of this
material at the FAA, call 425–227–1221. amending this SFAR to extend its The FAA is responsible for the safety
(5) You may view this service information expiration date. The FAA is also of flight in the U.S. and for the safety
that is incorporated by reference at the republishing, with minor revisions, the of U.S. civil operators, U.S.-registered
National Archives and Records approval process and exemption civil aircraft, and U.S.-certificated
Administration (NARA). For information on information for this SFAR. airmen throughout the world. The
the availability of this material at NARA, call FAA’s authority to issue rules on
202–741–6030, or go to: http://
This final rule is effective on
DATES:
December 14, 2017. aviation safety is found in title 49, U.S.
www.archives.gov/federal-register/cfr/ibr-
Code. Subtitle I, sections 106(f) and (g),
locations.html. FOR FURTHER INFORMATION CONTACT: describe the authority of the FAA
sradovich on DSK3GMQ082PROD with RULES
Issued in Renton, Washington, on Michael Filippell, Air Transportation Administrator. Subtitle VII of title 49,
December 4, 2017. Division, Flight Standards Service, Aviation Programs, describes in more
Dionne Palermo, Federal Aviation Administration, 800 detail the scope of the agency’s
Acting Director, System Oversight Division, Independence Avenue SW, Washington, authority. Section 40101(d)(1) provides
Aircraft Certification Service. DC 20591; telephone (202) 267–8166; that the Administrator shall consider in
[FR Doc. 2017–26842 Filed 12–13–17; 8:45 am] email michael.e.filippell@faa.gov. the public interest, among other matters,
BILLING CODE 4910–13–P SUPPLEMENTARY INFORMATION: assigning, maintaining, and enhancing
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Document Created: 2018-10-25 10:52:48
Document Modified: 2018-10-25 10:52:48
| Category | Regulatory Information | |
| Collection | Federal Register | |
| sudoc Class | AE 2.7: GS 4.107: AE 2.106: | |
| Publisher | Office of the Federal Register, National Archives and Records Administration | |
| Section | Rules and Regulations | |
| Action | Final rule; request for comments. | |
| Dates | This AD becomes effective December 29, 2017. | |
| Contact | Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 1601 Lind Avenue SW, Renton, WA 98057-3356; telephone 425-227-1138; fax 425-227- 1149. | |
| FR Citation | 82 FR 58718 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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