83 FR 51825 - Airworthiness Directives; Airbus SAS Airplanes
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration Federal Register Volume 83, Issue 199 (October 15, 2018)
Federal Aviation Administration
Federal Register Volume 83, Issue 199 (October 15, 2018)
| Page Range | 51825-51829 | |
| FR Document | 2018-21967 |
[Federal Register Volume 83, Number 199 (Monday, October 15, 2018)] [Rules and Regulations] [Pages 51825-51829] From the Federal Register Online [www.thefederalregister.org] [FR Doc No: 2018-21967] ----------------------------------------------------------------------- DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA-2018-0498; Product Identifier 2018-NM-013-AD; Amendment 39-19465; AD 2018-21-07] RIN 2120-AA64 Airworthiness Directives; Airbus SAS Airplanes AGENCY: Federal Aviation Administration (FAA), Department of Transportation (DOT). ACTION: Final rule. ----------------------------------------------------------------------- SUMMARY: We are adopting a new airworthiness directive (AD) for certain Airbus SAS Model A330-200 Freighter, -200, and -300 series airplanes. This AD was prompted by reports of Angle of Attack (AOA) blockages not detected by upgraded flight control primary computer (FCPC) software standards. This AD requires upgrading certain FCPCs, which terminates a certain airplane flight manual revision for certain airplanes. We are issuing this AD to address the unsafe condition on these products. DATES: This AD is effective November 19, 2018. The Director of the Federal Register approved the incorporation by reference of certain publications listed in this AD as of November 19, 2018. ADDRESSES: For service information identified in this final rule, contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email airworthiness.A330-A340@airbus.com; internet http://www.airbus.com. You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. It is also available on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018- 0498. 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- 0498; 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: Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229. SUPPLEMENTARY INFORMATION: Discussion We issued a notice of proposed rulemaking (NPRM) to amend 14 CFR part 39 by adding an AD that would apply to certain Airbus SAS Model A330-200 Freighter, -200, and -300 series airplanes. The NPRM published in the Federal Register on June 4, 2018 (83 FR 25595). The NPRM was prompted by reports of AOA blockages not detected by upgraded FCPC software standards. The NPRM proposed to require upgrading certain FCPCs, which would terminate a certain airplane flight [[Page 51826]] manual revision for certain airplanes. We are issuing this AD to address Alpha protection activation due to blocked AOA probes, which could result in reduced controllability of the airplane. The European Aviation Safety Agency (EASA), which is the Technical Agent for the Member States of the European Union, has issued EASA AD 2017-0246R1, dated April 6, 2018 (referred to after this as the Mandatory Continuing Airworthiness Information, or ``the MCAI''), to correct an unsafe condition for certain Airbus SAS Model A330-200 Freighter, -200, and -300 series airplanes. The MCAI states: In 2015, occurrences were reported of multiple Angle of Attack (AOA) blockages. Investigation results indicated the need for AOA monitoring in order to better detect cases of AOA blockage. This condition, if not corrected, could, under specific circumstances, lead to undue activation of the Alpha protection, possibly resulting in reduced control of the aeroplane. To address this potential unsafe condition, Airbus developed new FCPC software standards for enhanced AOA monitoring and, consequently, EASA issued AD 2015-0124 (later revised) [which corresponds to FAA AD 2016-25-30, Amendment 39-18756, (82 FR 1175, January 5, 2017) (``AD 2016-25-30'')] to require these software standard upgrades. Since EASA AD 2015-0124R3 was issued, it was identified that, for some cases, AOA blockages were not detected by those FCPC software standards. Consequently, new FCPC software standards, as specified in Table 1 of this [EASA] AD, have been developed (Airbus modification (mod) 206412, mod 206413 and mod 206414) to further improve the detection of AOA blockage. Airbus issued Service Bulletin (SB) A330-27-3222 and SB A330-27-3223 to implement these mods on in-service aeroplanes. Consequently, EASA issued AD 2017- 0246 to require a software standard upgrade of the three FCPCs, either by modification or replacement. Since that [EASA] AD was issued, it was determined that the Aircraft Flight Manual (AFM) Emergency Procedure, as previously required by EASA AD 2014-0267-E [which corresponds to FAA AD 2014- 25-52, Amendment 39-18066, (80 FR 3161, January 22, 2015) (``AD 2014-25-52'')] can also be removed for other AOA sensors and FCPC configurations. This [EASA] AD revises paragraph (2) accordingly, also introducing Table 2 for that purpose. 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- 0498. Comments We gave the public the opportunity to participate in developing this final rule. The following presents the comments received on the NPRM and the FAA's response to each comment. Support for the NPRM The Air Line Pilots Association, International (ALPA) expressed support for the NPRM. Request To Change Applicability Delta Air Lines (Delta) asked that we further restrict the applicability identified in paragraph (c) of the proposed AD by including the effectivity in the referenced service information. Delta stated that operators should be held accountable only for airplanes on which an airworthiness concern exists, and those airplanes correspond to the effectivity of the referenced service information. Delta added that if there are airplanes outside of this effectivity, operators will incur costs to produce and maintain records for those airplanes, regardless of whether or not there is an unsafe condition. Delta asserted that the service information provides a list of production airplanes that will be, or will have been, delivered with the affected software. We do agree to clarify the applicability. This AD is applicable to airplanes equipped with certain FCPC and not only to specific airplane manufacturer serial numbers (MSNs). For airplanes equipped with certain FCPC, only those that are in a pre-mod configuration as specified in paragraph (g) of this AD are required to do the upgrade specified in paragraph (h) of this AD. Airplanes in a post-mod configuration are not required to do an upgrade; however, they must comply with paragraph (k) of this AD. Paragraph (k) of this AD prohibits the installation of any software or hardware of a standard earlier than one listed in table 1 to paragraphs (h) and (k) of this AD on all airplanes identified in paragraph (c) of this AD. In order for this installation prohibition to be effective, airplanes in a post-mod configuration must be included in the applicability. We are also matching the applicability in the MCAI. Therefore, we have not changed this AD in this regard. Request To Remove Reference to Group 2 Airplanes Delta asked that we remove references to Group 2 airplanes from paragraphs (g) and (k) of the proposed AD, ``Definition of Groups'' and ``Parts Installation Prohibition,'' respectively. Delta stated that Group 1 airplanes are those in pre-mod 206412, 206413, or 206414 configuration, as applicable; Group 2 airplanes are those in post-mod 206412, 206413, or 206414 configuration, as applicable. Delta added that Group 2 airplanes are those that do not require modification, since they are already equipped with the FCPC software; therefore, those airplanes should be excluded from the applicability since the unsafe condition does not exist on those airplanes. Delta noted that a Group 1/Group 2 definition is redundant to the applicability paragraph because that paragraph defines only those airplanes on which the unsafe condition exists. Delta also noted that the proposed language in paragraph (k) of the proposed AD would allow continued installation of existing hardware/software before the AD effective date and prohibit removal of the modification after the effective date of the AD. We do not agree with the commenter's request. Airplanes in Groups 1 and 2 represent the total of the airplanes identified in paragraph (c) of the AD. Group 1 and Group 2 are defined in paragraph (g) of this AD to distinguish one from another, for the purpose of identifying the applicable requirements. Removing the definition of Group 2 airplanes from paragraph (g) of this AD would not remove Group 2 airplanes from the applicability. Airplanes in Group 2 may in the future be subject to the unsafe condition identified in this AD if an earlier standard of software or hardware is installed on that airplane. Therefore, so that Group 2 airplanes remain in an airworthy configuration after the effective date of the AD, paragraph (k) of this AD prohibits the installation of any software or hardware of a standard earlier than that listed in table 1 to paragraphs (h) and (k) of this AD. Therefore, we have not changed this AD in this regard. Request To Reference to Later Revisions of Service Information Delta asked that we change paragraph (h) of the proposed AD to allow use of subsequent service bulletins. Delta stated that the FCPC software standard has changed approximately every two years. Delta noted that adding the term ``or relative later software standard'' will allow operators to immediately install the latest software standard without having to request an alternative method of compliance (AMOC). We disagree with the commenter's request. In general terms, we are required by the Office of the Federal Register (OFR) regulations to either publish the service document contents as part of the actual AD language; or submit the service document to the OFR for approval as ``referenced'' material, in which case we may only refer to such material in the text of an AD. The AD may refer to the service document only if the OFR approved it for [[Page 51827]] ``incorporation by reference.'' See 1 CFR part 51. To allow operators to use later revisions of the referenced document (issued after publication of the AD), either we must revise the AD to reference specific later revisions, or operators must request approval to use later revisions or later software standards as an AMOC for this AD under the provisions of paragraph (l)(1) of this AD. We have not changed this AD in this regard. Conclusion We reviewed the relevant data, considered the comments 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. Related Service Information Under 1 CFR Part 51 Airbus SAS has issued the following service information: Service Bulletin A330-27-3222, dated February 16, 2017. Service Bulletin A330-27-3223, dated June 6, 2017. This service information describes procedures for upgrading (by modification or replacement, as applicable) certain FCPCs. These documents are distinct since they apply to different airplanes in different configurations. 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 103 airplanes of U.S. registry. We estimate the following costs to comply with this AD: Estimated Costs ---------------------------------------------------------------------------------------------------------------- Cost per Cost on U.S. Action Labor cost Parts cost product operators ---------------------------------------------------------------------------------------------------------------- Modification/replacement........... 3 work-hours x $85 per hour $0 $255 $26,265 = $255. ---------------------------------------------------------------------------------------------------------------- According to the manufacturer, some or all of the costs of this AD may be covered under warranty, thereby reducing the cost impact on affected individuals. We do not control warranty coverage for affected individuals. As a result, we have included all known costs in our cost estimate. Authority for This Rulemaking Title 49 of the United States Code specifies the FAA's authority to issue rules on aviation safety. Subtitle I, section 106, describes the authority of the FAA Administrator. Subtitle VII: Aviation Programs, describes in more detail the scope of the Agency's authority. We are issuing this rulemaking under the authority described in Subtitle VII, Part A, Subpart III, Section 44701: ``General requirements.'' Under that section, Congress charges the FAA with promoting safe flight of civil aircraft in air commerce by prescribing regulations for practices, methods, and procedures the Administrator finds necessary for safety in air commerce. This regulation is within the scope of that authority because it addresses an unsafe condition that is likely to exist or develop on products identified in this rulemaking action. This AD is issued in accordance with authority delegated by the Executive Director, Aircraft Certification Service, as authorized by FAA Order 8000.51C. In accordance with that order, issuance of ADs is normally a function of the Compliance and Airworthiness Division, but during this transition period, the Executive Director has delegated the authority to issue ADs applicable to transport category airplanes and associated appliances to the Director of the System Oversight Division. Regulatory Findings This AD will not have federalism implications under Executive Order 13132. This AD will not have a substantial direct effect on the States, on the relationship between the national government and the States, or on the distribution of power and responsibilities among the various levels of government. For the reasons discussed above, I certify that this AD: (1) Is not a ``significant regulatory action'' under Executive Order 12866, (2) Is not a ``significant rule'' under the DOT Regulatory Policies and Procedures (44 FR 11034, February 26, 1979), (3) Will not affect intrastate aviation in Alaska, and (4) Will not have a significant economic impact, positive or negative, on a substantial number of small entities under the criteria of the Regulatory Flexibility Act. List of Subjects in 14 CFR Part 39 Air transportation, Aircraft, Aviation safety, Incorporation by reference, Safety. Adoption of the Amendment Accordingly, under the authority delegated to me by the Administrator, the FAA amends 14 CFR part 39 as follows: PART 39--AIRWORTHINESS DIRECTIVES 0 1. The authority citation for part 39 continues to read as follows: Authority: 49 U.S.C. 106(g), 40113, 44701. Sec. 39.13 [Amended] 0 2. The FAA amends Sec. 39.13 by adding the following new airworthiness directive (AD): 2018-21-07 Airbus SAS: Amendment 39-19465; Docket No. FAA-2018-0498; Product Identifier 2018-NM-013-AD. (a) Effective Date This AD is effective November 19, 2018. (b) Affected ADs This AD affects AD 2014-25-52, Amendment 39-18066 (80 FR 3161, January 22, 2015) (``AD 2014-25-52''); and AD 2016-25-30, Amendment 39-18756, (82 FR 1175, January 5, 2017) (``AD 2016-25-30''). (c) Applicability This AD applies to the airplanes, certificated in any category, identified in paragraphs (c)(1), (c)(2), and (c)(3) of this AD; all manufacturer serial numbers; equipped with flight control primary computers (FCPCs) having software standard P13/M22 (hardware 2K2), P14/M23 (hardware 2K1), or M23 (hardware 2K0), or earlier standard. (1) Airbus Model A330-223F and -243F airplanes. (2) Airbus Model A330-201, -202, -203, -223, and -243 airplanes. (3) Airbus Model A330-301, -302, -303, -321, -322, -323, -341, - 342, and -343 airplanes. Note 1 to paragraph (c) of this AD: The software standards specified in paragraph (c) of this AD correspond, respectively, to part number (P/N) LA2K2B100DG0000, P/N [[Page 51828]] LA2K1A100DF0000, and P/N LA2K01500AF0000. All affected airplanes should be equipped with this software, as required by AD 2016-25-30. (d) Subject Air Transport Association (ATA) of America Code 27, Flight Controls. (e) Reason This AD was prompted by reports of Angle of Attack (AOA) blockages not detected by upgraded FCPC software standards. We are issuing this AD to prevent Alpha protection activation due to blocked AOA probes, which could result in reduced controllability of the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Definitions of Groups Group 1 airplanes are those in pre-mod 206412, pre-mod 206413, or pre-mod 206414 configuration, as applicable. Group 2 airplanes are those in post-mod (206412, 206413, or 206414, as applicable) configuration. (h) Upgrade Flight Control Primary Computer Software For Group 1 airplanes: Within 12 months after the effective date of this AD: Upgrade (by modification or replacement, as applicable) the three FCPCs, as specified in table 1 to paragraphs (h) and (k) of this AD, in accordance with the Accomplishment Instructions of the applicable service information specified in table 1 to paragraphs (h) and (k) of this AD. [GRAPHIC] [TIFF OMITTED] TR15OC18.001 (i) Terminating Action for Certain Requirements of AD 2014-25-52 For airplanes with an AOA configuration as identified in figure 1 to paragraph (i) of this AD, or as identified in paragraph (m)(2) of AD 2016-12-15, Amendment 39-18564 (81 FR 40160, June 21, 2016) (``AD 2016-12-15''), as applicable: Accomplishing the upgrade required by paragraph (h) of this AD terminates the requirements of paragraph (g) of AD 2014-25-52, and the airplane flight manual (AFM) procedure required by paragraph (g) of AD 2014-25-52 may be removed from the AFM. [GRAPHIC] [TIFF OMITTED] TR15OC18.002 (j) Terminating Action for Certain Requirements of AD 2016-25-30 Accomplishment of the actions required by paragraph (h) of this AD terminates the requirements of paragraph (g) of AD 2016-25-30 for that airplane. (k) Parts Installation Prohibition Installation of any software or hardware of a version earlier than the one listed in table 1 to paragraphs (h) and (k) of this AD is prohibited, as required by paragraphs (k)(1) and (k)(2) of this AD, as applicable. (1) For Group 1 airplanes: After modification of an airplane as required by paragraph (h) of this AD. (2) For Group 2 airplanes: As of the effective date of this AD. (l) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Section, Transport Standards Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the manager of the International Branch, send it to the attention of the person [[Page 51829]] identified in paragraph (m)(2) of this AD. Information may be emailed to: 9-ANM-116-AMOC-REQUESTS@faa.gov. Before using any approved AMOC, notify your appropriate principal inspector, or lacking a principal inspector, the manager of the local flight standards district office/certificate holding district office. (2) Contacting the Manufacturer: For any requirement in this AD to obtain corrective actions from a manufacturer, the action must be accomplished using a method approved by the Manager, International Section, Transport Standards Branch, FAA; or the European Aviation Safety Agency (EASA); or EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOA-authorized signature. (3) Required for Compliance (RC): 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. (m) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA AD 2017-0246R1, dated April 6, 2018, for related information. This MCAI may be found in the AD docket on the internet at http://www.regulations.gov by searching for and locating Docket No. FAA-2018-0498. (2) For more information about this AD, contact Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229. (n) Material Incorporated by Reference (1) The Director of the Federal Register approved the incorporation by reference (IBR) of the service information listed in this paragraph under 5 U.S.C. 552(a) and 1 CFR part 51. (2) You must use this service information as applicable to do the actions required by this AD, unless this AD specifies otherwise. (i) Airbus Service Bulletin A330-27-3222, dated February 16, 2017. (ii) Airbus Service Bulletin A330-27-3223, dated June 6, 2017. (3) For service information identified in this AD, contact Airbus SAS, Airworthiness Office--EAL, Rond-Point Emile Dewoitine No: 2, 31700 Blagnac Cedex, France; telephone +33 5 61 93 36 96; fax +33 5 61 93 45 80; email airworthiness.A330-A340@airbus.com; internet http://www.airbus.com. (4) You may view this service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206-231-3195. (5) You may view this service information that is incorporated by reference at the National Archives and Records Administration (NARA). For information on the availability of this material at NARA, call 202-741-6030, or go to: http://www.archives.gov/federal-register/cfr/ibr-locations.html. Issued in Des Moines, Washington, on September 23, 2018. John P. Piccola, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018-21967 Filed 10-12-18; 8:45 am] BILLING CODE 4910-13-P
![Federal Register / Vol. 83, No. 199 / Monday, October 15, 2018 / Rules and Regulations 51825
if those actions were performed before the paragraph under 5 U.S.C. 552(a) and 1 CFR certain airplanes. We are issuing this
effective date of this AD using the applicable part 51. AD to address the unsafe condition on
service information identified in paragraphs (2) You must use this service information these products.
(h)(1)(i) through (h)(1)(iv) of this AD. as applicable to do the actions required by
this AD, unless this AD specifies otherwise. DATES: This AD is effective November
(i) Bombardier Service Bulletin 700–1A11–
53–025, dated July 14, 2016. (i) Bombardier Service Bulletin 700–53– 19, 2018.
(ii) Bombardier Service Bulletin 700–53– 050, Revision 01, dated December 16, 2016. The Director of the Federal Register
050, dated July 14, 2016. (ii) Bombardier Service Bulletin 700–53– approved the incorporation by reference
(iii) Bombardier Service Bulletin 700–53– 5009, Revision 01, dated December 16, 2016. of certain publications listed in this AD
5009, dated July 14, 2016. (iii) Bombardier Service Bulletin 700– as of November 19, 2018.
(iv) Bombardier Service Bulletin 700–53– 1A11–53–025, Revision 01, dated December
ADDRESSES: For service information
6008, dated July 14, 2016. 16, 2016.
(iv) Bombardier Service Bulletin 700–53– identified in this final rule, contact
(2) Incorporation of Bombardier Service
6008, Revision 01, dated December 16, 2016. Airbus SAS, Airworthiness Office—
Request for Product Support Action 124026
on an airplane prior to the effective date of (3) For service information identified in EAL, Rond-Point Emile Dewoitine No:
this AD meets the intent of paragraph (g) of this AD, contact Bombardier, Inc., 400 Côte- 2, 31700 Blagnac Cedex, France;
this AD for that airplane. Vertu Road West, Dorval, Québec H4S 1Y9, telephone +33 5 61 93 36 96; fax +33 5
Canada; telephone 514–855–5000; fax 514– 61 93 45 80; email airworthiness.A330-
(i) Other FAA AD Provisions 855–7401; email thd.crj@ A340@airbus.com; internet http://
The following provisions also apply to this aero.bombardier.com; internet http://
www.airbus.com. You may view this
AD: www.bombardier.com.
(4) You may view this service information service information at the FAA,
(1) Alternative Methods of Compliance
at the FAA, Transport Standards Branch, Transport Standards Branch, 2200
(AMOCs): The Manager, New York ACO
Branch, FAA, has the authority to approve 2200 South 216th St., Des Moines, WA. For South 216th St., Des Moines, WA. For
AMOCs for this AD, if requested using the information on the availability of this information on the availability of this
procedures found in 14 CFR 39.19. In material at the FAA, call 206–231–3195. material at the FAA, call 206–231–3195.
accordance with 14 CFR 39.19, send your (5) You may view this service information It is also available on the internet at
request to your principal inspector or local that is incorporated by reference at the http://www.regulations.gov by searching
Flight Standards District Office, as National Archives and Records
for and locating Docket No. FAA–2018–
appropriate. If sending information directly Administration (NARA). For information on
the availability of this material at NARA, call 0498.
to the manager of the certification office,
send it to ATTN: Program Manager, 202–741–6030, or go to: http:// Examining the AD Docket
Continuing Operational Safety, FAA, New www.archives.gov/federal-register/cfr/ibr-
locations.html. You may examine the AD docket on
York ACO Branch, 1600 Stewart Avenue,
Suite 410, Westbury, NY 11590; telephone
the internet at http://
Issued in Des Moines, Washington, on
516–228–7300; fax 516–794–5531. Before October 2, 2018.
www.regulations.gov by searching for
using any approved AMOC, notify your and locating Docket No. FAA–2018–
Michael Kaszycki,
appropriate principal inspector, or lacking a 0498; or in person at Docket Operations
Acting Director, System Oversight Division, between 9 a.m. and 5 p.m., Monday
principal inspector, the manager of the local
Aircraft Certification Service.
flight standards district office/certificate through Friday, except Federal holidays.
holding district office. [FR Doc. 2018–21972 Filed 10–12–18; 8:45 am]
The AD docket contains this final rule,
(2) Contacting the Manufacturer: For any BILLING CODE 4910–13–P the regulatory evaluation, any
requirement in this AD to obtain corrective comments received, and other
actions from a manufacturer, the action must
be accomplished using a method approved
information. The address for Docket
DEPARTMENT OF TRANSPORTATION Operations (phone: 800–647–5527) is
by the Manager, New York ACO Branch,
FAA; or Transport Canada Civil Aviation Federal Aviation Administration U.S. Department of Transportation,
(TCCA); or Bombardier, Inc.’s TCCA Design Docket Operations, M–30, West
Approval Organization (DAO). If approved by 14 CFR Part 39 Building Ground Floor, Room W12–140,
the DAO, the approval must include the 1200 New Jersey Avenue SE,
DAO-authorized signature. [Docket No. FAA–2018–0498; Product Washington, DC 20590.
Identifier 2018–NM–013–AD; Amendment
(j) Related Information FOR FURTHER INFORMATION CONTACT:
39–19465; AD 2018–21–07]
(1) Refer to Mandatory Continuing Vladimir Ulyanov, Aerospace Engineer,
Airworthiness Information (MCAI) Canadian RIN 2120–AA64 International Section, Transport
AD CF–2017–31, dated September 22, 2017, Standards Branch, FAA, 2200 South
for related information. This MCAI may be Airworthiness Directives; Airbus SAS 216th St., Des Moines, WA 98198;
found in the AD docket on the internet at Airplanes telephone and fax 206–231–3229.
http://www.regulations.gov by searching for SUPPLEMENTARY INFORMATION:
AGENCY: Federal Aviation
and locating Docket No. FAA–2018–0546.
(2) For more information about this AD, Administration (FAA), Department of Discussion
contact Andrea Jimenez, Aerospace Engineer, Transportation (DOT).
Airframe and Mechanical Systems Section, ACTION: Final rule. We issued a notice of proposed
FAA, New York ACO Branch, 1600 Stewart rulemaking (NPRM) to amend 14 CFR
Avenue, Suite 410, Westbury, NY 11590; SUMMARY: We are adopting a new part 39 by adding an AD that would
telephone 516–228–7330; fax 516–794–5531; airworthiness directive (AD) for certain apply to certain Airbus SAS Model
email 9-avs-nyaco-cos@faa.gov. Airbus SAS Model A330–200 Freighter, A330–200 Freighter, –200, and –300
(3) Service information identified in this –200, and –300 series airplanes. This series airplanes. The NPRM published
khammond on DSK30JT082PROD with RULES
AD that is not incorporated by reference is AD was prompted by reports of Angle in the Federal Register on June 4, 2018
available at the addresses specified in of Attack (AOA) blockages not detected (83 FR 25595). The NPRM was
paragraphs (k)(3) and (k)(4) of this AD.
by upgraded flight control primary prompted by reports of AOA blockages
(k) Material Incorporated by Reference computer (FCPC) software standards. not detected by upgraded FCPC software
(1) The Director of the Federal Register This AD requires upgrading certain standards. The NPRM proposed to
approved the incorporation by reference FCPCs, which terminates a certain require upgrading certain FCPCs, which
(IBR) of the service information listed in this airplane flight manual revision for would terminate a certain airplane flight
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manual revision for certain airplanes. Support for the NPRM modification, since they are already
We are issuing this AD to address Alpha The Air Line Pilots Association, equipped with the FCPC software;
protection activation due to blocked International (ALPA) expressed support therefore, those airplanes should be
AOA probes, which could result in for the NPRM. excluded from the applicability since
reduced controllability of the airplane. the unsafe condition does not exist on
The European Aviation Safety Agency Request To Change Applicability those airplanes. Delta noted that a
(EASA), which is the Technical Agent Delta Air Lines (Delta) asked that we Group 1/Group 2 definition is
for the Member States of the European further restrict the applicability redundant to the applicability paragraph
Union, has issued EASA AD 2017– identified in paragraph (c) of the because that paragraph defines only
0246R1, dated April 6, 2018 (referred to proposed AD by including the those airplanes on which the unsafe
after this as the Mandatory Continuing effectivity in the referenced service condition exists. Delta also noted that
Airworthiness Information, or ‘‘the information. Delta stated that operators the proposed language in paragraph (k)
MCAI’’), to correct an unsafe condition should be held accountable only for of the proposed AD would allow
for certain Airbus SAS Model A330–200 airplanes on which an airworthiness continued installation of existing
Freighter, –200, and –300 series concern exists, and those airplanes hardware/software before the AD
airplanes. The MCAI states: effective date and prohibit removal of
correspond to the effectivity of the
the modification after the effective date
In 2015, occurrences were reported of referenced service information. Delta
multiple Angle of Attack (AOA) blockages. of the AD.
added that if there are airplanes outside We do not agree with the commenter’s
Investigation results indicated the need for of this effectivity, operators will incur
AOA monitoring in order to better detect request. Airplanes in Groups 1 and 2
costs to produce and maintain records represent the total of the airplanes
cases of AOA blockage.
for those airplanes, regardless of identified in paragraph (c) of the AD.
This condition, if not corrected, could,
under specific circumstances, lead to undue whether or not there is an unsafe Group 1 and Group 2 are defined in
activation of the Alpha protection, possibly condition. Delta asserted that the service paragraph (g) of this AD to distinguish
resulting in reduced control of the aeroplane. information provides a list of one from another, for the purpose of
To address this potential unsafe condition, production airplanes that will be, or identifying the applicable requirements.
Airbus developed new FCPC software will have been, delivered with the Removing the definition of Group 2
standards for enhanced AOA monitoring and, affected software.
consequently, EASA issued AD 2015–0124
airplanes from paragraph (g) of this AD
We do agree to clarify the would not remove Group 2 airplanes
(later revised) [which corresponds to FAA applicability. This AD is applicable to
AD 2016–25–30, Amendment 39–18756, (82 from the applicability. Airplanes in
airplanes equipped with certain FCPC Group 2 may in the future be subject to
FR 1175, January 5, 2017) (‘‘AD 2016–25–
30’’)] to require these software standard and not only to specific airplane the unsafe condition identified in this
upgrades. manufacturer serial numbers (MSNs). AD if an earlier standard of software or
Since EASA AD 2015–0124R3 was issued, For airplanes equipped with certain hardware is installed on that airplane.
it was identified that, for some cases, AOA FCPC, only those that are in a pre-mod Therefore, so that Group 2 airplanes
blockages were not detected by those FCPC configuration as specified in paragraph remain in an airworthy configuration
software standards. Consequently, new FCPC (g) of this AD are required to do the after the effective date of the AD,
software standards, as specified in Table 1 of upgrade specified in paragraph (h) of
this [EASA] AD, have been developed
paragraph (k) of this AD prohibits the
this AD. Airplanes in a post-mod installation of any software or hardware
(Airbus modification (mod) 206412, mod
configuration are not required to do an of a standard earlier than that listed in
206413 and mod 206414) to further improve
the detection of AOA blockage. Airbus issued upgrade; however, they must comply table 1 to paragraphs (h) and (k) of this
Service Bulletin (SB) A330–27–3222 and SB with paragraph (k) of this AD. Paragraph AD. Therefore, we have not changed
A330–27–3223 to implement these mods on (k) of this AD prohibits the installation this AD in this regard.
in-service aeroplanes. Consequently, EASA of any software or hardware of a
issued AD 2017–0246 to require a software standard earlier than one listed in table Request To Reference to Later
standard upgrade of the three FCPCs, either 1 to paragraphs (h) and (k) of this AD Revisions of Service Information
by modification or replacement. on all airplanes identified in paragraph Delta asked that we change paragraph
Since that [EASA] AD was issued, it was (c) of this AD. In order for this (h) of the proposed AD to allow use of
determined that the Aircraft Flight Manual
installation prohibition to be effective, subsequent service bulletins. Delta
(AFM) Emergency Procedure, as previously
required by EASA AD 2014–0267–E [which airplanes in a post-mod configuration stated that the FCPC software standard
corresponds to FAA AD 2014–25–52, must be included in the applicability. has changed approximately every two
Amendment 39–18066, (80 FR 3161, January We are also matching the applicability years. Delta noted that adding the term
22, 2015) (‘‘AD 2014–25–52’’)] can also be in the MCAI. Therefore, we have not ‘‘or relative later software standard’’ will
removed for other AOA sensors and FCPC changed this AD in this regard. allow operators to immediately install
configurations. This [EASA] AD revises the latest software standard without
paragraph (2) accordingly, also introducing Request To Remove Reference to Group
having to request an alternative method
Table 2 for that purpose. 2 Airplanes
of compliance (AMOC).
You may examine the MCAI in the Delta asked that we remove references We disagree with the commenter’s
AD docket on the internet at http:// to Group 2 airplanes from paragraphs (g) request. In general terms, we are
www.regulations.gov by searching for and (k) of the proposed AD, ‘‘Definition required by the Office of the Federal
and locating Docket No. FAA–2018– of Groups’’ and ‘‘Parts Installation Register (OFR) regulations to either
0498. Prohibition,’’ respectively. Delta stated publish the service document contents
khammond on DSK30JT082PROD with RULES
that Group 1 airplanes are those in pre- as part of the actual AD language; or
Comments mod 206412, 206413, or 206414 submit the service document to the OFR
We gave the public the opportunity to configuration, as applicable; Group 2 for approval as ‘‘referenced’’ material, in
participate in developing this final rule. airplanes are those in post-mod 206412, which case we may only refer to such
The following presents the comments 206413, or 206414 configuration, as material in the text of an AD. The AD
received on the NPRM and the FAA’s applicable. Delta added that Group 2 may refer to the service document only
response to each comment. airplanes are those that do not require if the OFR approved it for
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![Federal Register / Vol. 83, No. 199 / Monday, October 15, 2018 / Rules and Regulations 51827
‘‘incorporation by reference.’’ See 1 CFR public interest require adopting this This service information describes
part 51. final rule as proposed, except for minor procedures for upgrading (by
To allow operators to use later editorial changes. We have determined modification or replacement, as
revisions of the referenced document that these minor changes: applicable) certain FCPCs. These
(issued after publication of the AD), • Are consistent with the intent that documents are distinct since they apply
either we must revise the AD to was proposed in the NPRM for to different airplanes in different
reference specific later revisions, or addressing the unsafe condition; and configurations. This service information
• Do not add any additional burden is reasonably available because the
operators must request approval to use
upon the public than was already interested parties have access to it
later revisions or later software
proposed in the NPRM. through their normal course of business
standards as an AMOC for this AD
under the provisions of paragraph (l)(1) Related Service Information Under 1 or by the means identified in the
of this AD. We have not changed this CFR Part 51 ADDRESSES section.
AD in this regard. Airbus SAS has issued the following Costs of Compliance
Conclusion service information:
• Service Bulletin A330–27–3222, We estimate that this AD affects 103
We reviewed the relevant data, dated February 16, 2017. airplanes of U.S. registry.
considered the comments received, and • Service Bulletin A330–27–3223, We estimate the following costs to
determined that air safety and the dated June 6, 2017. comply with this AD:
ESTIMATED COSTS
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
Modification/replacement ................................ 3 work-hours × $85 per hour = $255 ............. $0 $255 $26,265
According to the manufacturer, some delegated the authority to issue ADs PART 39—AIRWORTHINESS
or all of the costs of this AD may be applicable to transport category DIRECTIVES
covered under warranty, thereby airplanes and associated appliances to
reducing the cost impact on affected the Director of the System Oversight ■ 1. The authority citation for part 39
individuals. We do not control warranty Division. continues to read as follows:
coverage for affected individuals. As a Authority: 49 U.S.C. 106(g), 40113, 44701.
result, we have included all known Regulatory Findings
costs in our cost estimate. This AD will not have federalism § 39.13 [Amended]
implications under Executive Order ■ 2. The FAA amends § 39.13 by adding
Authority for This Rulemaking 13132. This AD will not have a the following new airworthiness
Title 49 of the United States Code substantial direct effect on the States, on directive (AD):
specifies the FAA’s authority to issue the relationship between the national 2018–21–07 Airbus SAS: Amendment 39–
rules on aviation safety. Subtitle I, government and the States, or on the 19465; Docket No. FAA–2018–0498;
section 106, describes the authority of distribution of power and Product Identifier 2018–NM–013–AD.
the FAA Administrator. Subtitle VII: responsibilities among the various
Aviation Programs, describes in more (a) Effective Date
levels of government.
detail the scope of the Agency’s For the reasons discussed above, I This AD is effective November 19, 2018.
authority. certify that this AD: (b) Affected ADs
We are issuing this rulemaking under (1) Is not a ‘‘significant regulatory This AD affects AD 2014–25–52,
the authority described in Subtitle VII, action’’ under Executive Order 12866, Amendment 39–18066 (80 FR 3161, January
Part A, Subpart III, Section 44701: (2) Is not a ‘‘significant rule’’ under 22, 2015) (‘‘AD 2014–25–52’’); and AD 2016–
‘‘General requirements.’’ Under that the DOT Regulatory Policies and 25–30, Amendment 39–18756, (82 FR 1175,
section, Congress charges the FAA with Procedures (44 FR 11034, February 26, January 5, 2017) (‘‘AD 2016–25–30’’).
promoting safe flight of civil aircraft in 1979), (c) Applicability
air commerce by prescribing regulations (3) Will not affect intrastate aviation
for practices, methods, and procedures in Alaska, and This AD applies to the airplanes,
the Administrator finds necessary for certificated in any category, identified in
(4) Will not have a significant paragraphs (c)(1), (c)(2), and (c)(3) of this AD;
safety in air commerce. This regulation economic impact, positive or negative, all manufacturer serial numbers; equipped
is within the scope of that authority on a substantial number of small entities with flight control primary computers
because it addresses an unsafe condition under the criteria of the Regulatory (FCPCs) having software standard P13/M22
that is likely to exist or develop on Flexibility Act. (hardware 2K2), P14/M23 (hardware 2K1), or
products identified in this rulemaking M23 (hardware 2K0), or earlier standard.
action. List of Subjects in 14 CFR Part 39 (1) Airbus Model A330–223F and –243F
This AD is issued in accordance with Air transportation, Aircraft, Aviation airplanes.
authority delegated by the Executive safety, Incorporation by reference, (2) Airbus Model A330–201, –202, –203,
khammond on DSK30JT082PROD with RULES
–223, and –243 airplanes.
Director, Aircraft Certification Service, Safety. (3) Airbus Model A330–301, –302, –303,
as authorized by FAA Order 8000.51C. –321, –322, –323, –341, –342, and –343
In accordance with that order, issuance Adoption of the Amendment
airplanes.
of ADs is normally a function of the Accordingly, under the authority Note 1 to paragraph (c) of this AD: The
Compliance and Airworthiness delegated to me by the Administrator, software standards specified in paragraph (c)
Division, but during this transition the FAA amends 14 CFR part 39 as of this AD correspond, respectively, to part
period, the Executive Director has follows: number (P/N) LA2K2B100DG0000, P/N
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![Federal Register / Vol. 83, No. 199 / Monday, October 15, 2018 / Rules and Regulations 51829
identified in paragraph (m)(2) of this AD. National Archives and Records District Avenue, Burlington, MA 01803.
Information may be emailed to: 9-ANM-116- Administration (NARA). For information on For information on the availability of
AMOC-REQUESTS@faa.gov. Before using the availability of this material at NARA, call this material at the FAA, call 781–238–
any approved AMOC, notify your appropriate 202–741–6030, or go to: http:// 7759. It is also available on the internet
principal inspector, or lacking a principal www.archives.gov/federal-register/cfr/ibr-
inspector, the manager of the local flight locations.html.
at http://www.regulations.gov by
standards district office/certificate holding searching for and locating Docket No.
district office. Issued in Des Moines, Washington, on FAA–2017–1116.
(2) Contacting the Manufacturer: For any September 23, 2018.
requirement in this AD to obtain corrective John P. Piccola, Examining the AD Docket
actions from a manufacturer, the action must Acting Director, System Oversight Division, You may examine the AD docket on
be accomplished using a method approved Aircraft Certification Service. the internet at http://
by the Manager, International Section, [FR Doc. 2018–21967 Filed 10–12–18; 8:45 am] www.regulations.gov by searching for
Transport Standards Branch, FAA; or the and locating Docket No. FAA–2017–
BILLING CODE 4910–13–P
European Aviation Safety Agency (EASA); or
EASA Design Organization Approval (DOA).
1116; or in person at Docket Operations
If approved by the DOA, the approval must between 9 a.m. and 5 p.m., Monday
include the DOA-authorized signature. DEPARTMENT OF TRANSPORTATION through Friday, except Federal holidays.
(3) Required for Compliance (RC): If any The AD docket contains this final rule,
service information contains procedures or Federal Aviation Administration the regulatory evaluation, any
tests that are identified as RC, those comments received, and other
procedures and tests must be done to comply 14 CFR Part 39 information. The address for Docket
with this AD; any procedures or tests that are Operations (phone: 800–647–5527) is
not identified as RC are recommended. Those [Docket No. FAA–2017–1116; Product
Identifier 2016–NE–32–AD; Amendment 39– U.S. Department of Transportation,
procedures and tests that are not identified
as RC may be deviated from using accepted 19459; AD 2018–21–01] Docket Operations, M–30, West
methods in accordance with the operator’s Building Ground Floor, Room W12–140,
maintenance or inspection program without RIN 2120–AA64 1200 New Jersey Avenue SE,
obtaining approval of an AMOC, provided Washington, DC 20590.
the procedures and tests identified as RC can Airworthiness Directives; Honeywell FOR FURTHER INFORMATION CONTACT:
be done and the airplane can be put back in International Inc. Turbofan Engines Joseph Costa, Aerospace Engineer, Los
an airworthy condition. Any substitutions or Angeles ACO Branch, FAA, 3960
changes to procedures or tests identified as AGENCY: Federal Aviation
RC require approval of an AMOC. Administration (FAA), DOT. Paramount Blvd., Lakewood, CA 90712–
ACTION: Final rule.
4137; phone: 562–627–5246; fax: 562–
(m) Related Information 627–5210; email: joseph.costa@faa.gov.
(1) Refer to Mandatory Continuing SUMMARY: We are superseding SUPPLEMENTARY INFORMATION:
Airworthiness Information (MCAI) EASA AD Airworthiness Directive (AD) 2017–20–
2017–0246R1, dated April 6, 2018, for related Discussion
06 for certain Honeywell International
information. This MCAI may be found in the We issued a notice of proposed
AD docket on the internet at http://
Inc. (Honeywell) AS907–1–1A turbofan
engines. AD 2017–20–06 required a one- rulemaking (NPRM) to amend 14 CFR
www.regulations.gov by searching for and
locating Docket No. FAA–2018–0498. time inspection of the second stage low- part 39 to supersede AD 2017–20–06,
(2) For more information about this AD, pressure turbine (LPT2) blades and, if Amendment 39–19063 (82 FR 46379,
contact Vladimir Ulyanov, Aerospace the blades fail the inspection, the October 5, 2017), (‘‘AD 2017–20–06’’).
Engineer, International Section, Transport replacement of the blades with a part AD 2017–20–06 applied to certain
Standards Branch, FAA, 2200 South 216th eligible for installation. This AD Honeywell International Inc.
St., Des Moines, WA 98198; telephone and continues to require a one-time (Honeywell) AS907–1–1A turbofan
fax 206–231–3229. engines. The NPRM published in the
inspection of the LPT2 blades and, if the
(n) Material Incorporated by Reference blades fail the inspection, the Federal Register on January 30, 2018
(1) The Director of the Federal Register replacement of the blades with a part (83 FR 4167). The NPRM was prompted
approved the incorporation by reference eligible for installation. This AD was by the need to clarify the Applicability
(IBR) of the service information listed in this prompted by the need to clarify the and Compliance sections of AD 2017–
paragraph under 5 U.S.C. 552(a) and 1 CFR Applicability and Compliance sections 20–06. The NPRM proposed to continue
part 51. of AD 2017–20–06. We are issuing this to require one-time inspection of the
(2) You must use this service information LPT2 blades and, if the blades fail the
AD to address the unsafe condition on
as applicable to do the actions required by inspection, the replacement of the
this AD, unless this AD specifies otherwise. these products.
DATES: This AD is effective November
blades with a part eligible for
(i) Airbus Service Bulletin A330–27–3222,
dated February 16, 2017. 19, 2018. installation. We are issuing this AD to
(ii) Airbus Service Bulletin A330–27–3223, The Director of the Federal Register address the unsafe condition on these
dated June 6, 2017. approved the incorporation by reference products.
(3) For service information identified in of a certain publication listed in this AD
this AD, contact Airbus SAS, Airworthiness
Comments
Office—EAL, Rond-Point Emile Dewoitine as of November 9, 2017 (82 FR 46379, We gave the public the opportunity to
No: 2, 31700 Blagnac Cedex, France; October 5, 2017). participate in developing this AD. The
telephone +33 5 61 93 36 96; fax +33 5 61 ADDRESSES: For service information following presents the comments
93 45 80; email airworthiness.A330-A340@ identified in this final rule, contact received on the NPRM and the FAA’s
khammond on DSK30JT082PROD with RULES
airbus.com; internet http://www.airbus.com. Honeywell International Inc., 111 S 34th
(4) You may view this service information
response to each comment.
Street, Phoenix, AZ 85034–2802; phone:
at the FAA, Transport Standards Branch, Request To Align the Compliance
2200 South 216th St., Des Moines, WA. For
800–601–3099; internet: https://
myaerospace2.honeywell.com/wps/ Requirements With the Service Bulletin
information on the availability of this (SB)
material at the FAA, call 206–231–3195. portal. You may view this service
(5) You may view this service information information at the FAA, Engine and Bombardier Aerospace (Bombardier)
that is incorporated by reference at the Propeller Standards Branch, 1200 requested that the compliance
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Document Created: 2018-10-13 10:05:08
Document Modified: 2018-10-13 10:05:08
| 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 19, 2018. | |
| Contact | Vladimir Ulyanov, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3229. | |
| FR Citation | 83 FR 51825 | |
| RIN Number | 2120-AA64 | |
| CFR Associated | Air Transportation; Aircraft; Aviation Safety; Incorporation by Reference and Safety |
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