Airworthiness Directives; Airbus Airplanes, 15048-15050 [2018-06946]

Download as PDF 15048 Federal Register / Vol. 83, No. 68 / Monday, April 9, 2018 / Rules and Regulations Administration (NARA). For information on the availability of this material at NARA, call 202–741–6030, or go to: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Des Moines, Washington, on March 20, 2018. Michael Kaszycki, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018–06712 Filed 4–6–18; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 39 [Docket No. FAA–2018–0269; Product Identifier 2018–NM–051–AD; Amendment 39–19243; AD 2018–07–12] RIN 2120–AA64 Airworthiness Directives; Airbus Airplanes Federal Aviation Administration (FAA), DOT. ACTION: Final rule; request for comments. AGENCY: We are adopting a new airworthiness directive (AD) for all Airbus Model A350–941 airplanes. This AD requires performing repetitive station position pick-off unit (SPPU) calibration tests, and applying the corresponding airplane fault isolation if necessary. This AD was prompted by a report indicating malfunctions of the SPPU and failures of the internal wiring due to water ingress via certain electrical connectors, inducing subsequent icing during flight. We are issuing this AD to address the unsafe condition on these products. DATES: This AD becomes effective April 24, 2018. The Director of the Federal Register approved the incorporation by reference of a certain publication listed in this AD as of April 24, 2018. We must receive comments on this AD by May 24, 2018. ADDRESSES: You may send comments, using the procedures found in 14 CFR 11.43 and 11.45, by any of the following methods: • Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments. • Fax: 202–493–2251. • Mail: U.S. Department of Transportation, Docket Operations, M– 30, West Building Ground Floor, Room W12–140, 1200 New Jersey Avenue SE, Washington, DC 20590. sradovich on DSK3GMQ082PROD with RULES SUMMARY: VerDate Sep<11>2014 16:01 Apr 06, 2018 Jkt 244001 • 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 continued-airworthiness.a350@ airbus.com; internet https:// www.airbus.com. You may view this referenced service information at the FAA, Transport Standards Branch, 2200 South 216th St., Des Moines, WA. For information on the availability of this material at the FAA, call 206–231–3195. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2018– 0269. This condition, if not detected and corrected, could lead to hidden sensor signal drift (at flap station 3) which, in combination with an independent failure of a flap down drive disconnect, might lead to in-flight detachment of the outer flap surface, possibly resulting in damage to the aeroplane, and/or injury to persons on the ground. Airbus determined that the SPPU calibration test can highlight all hidden faults, but this test is only scheduled after removal/installation of the equipment. Consequently, to address this potential unsafe condition, Airbus issued the SB [Service Bulletin A350–27–P021, dated February 13, 2018], providing instructions to accomplish the SPPU calibration test at regular intervals. For the reason described above, this [EASA] AD requires repetitive SPPU calibration test and, depending on findings, accomplishment of applicable corrective action(s) [applying corresponding airplane fault isolation]. Pending the results of the on-going investigation, this [EASA] AD is still considered to be an interim measure and further [EASA] AD action may follow. Examining the AD Docket You may examine the AD docket on the internet at https:// www.regulations.gov by searching for and locating Docket No. FAA–2018– 0269; 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: Kathleen Arrigotti, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3218. SUPPLEMENTARY INFORMATION: You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2018–0269. 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 2018–0058, dated March 14, 2018 (referred to after this as the Mandatory Continuing Airworthiness Information, or ‘‘the MCAI’’), to correct an unsafe condition for all Airbus Model A350–941 airplanes. The MCAI states: Occurrences have been reported by Airbus A350 operators of malfunctions of Station Position Pick-Off Units (SPPU). Investigations indicated that internal wiring failures occurred due to water ingress via certain electrical connectors, inducing subsequent icing during flight. PO 00000 Frm 00030 Fmt 4700 Sfmt 4700 Related Service Information Under 1 CFR Part 51 Airbus has issued Service Bulletin A350–27–P021, dated February 13, 2018. The service information describes performing repetitive SPPU calibration tests, and applying the corresponding airplane fault isolation if necessary. 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 the same type design. 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 E:\FR\FM\09APR1.SGM 09APR1 Federal Register / Vol. 83, No. 68 / Monday, April 9, 2018 / Rules and Regulations rule because malfunctions of the SPPU and failures of the internal wiring due to water ingress via certain electrical connectors can induce icing, which under certain conditions, could lead to in-flight detachment of the outer flap surface, and consequent damage to the airplane. 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 data, views, or arguments about this AD. Send your comments to an address listed under the ADDRESSES section. Include ‘‘Docket No. FAA–2018–0269; Product Identifier 2018–NM–051–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 15049 received by the closing date and may amend this AD based on those comments. We will post all comments we receive, without change, to https:// www.regulations.gov, including any personal information you provide. We will also post a report summarizing each substantive verbal contact we receive about this AD. Costs of Compliances We estimate that this AD affects 6 airplanes of U.S. registry. We estimate the following costs to comply with this AD: ESTIMATED COSTS Action Labor cost SPPU calibration test .... 2 work-hours × $85 per hour = $170 per test cycle. We have received no definitive data that would enable us to provide cost estimates for the on-condition actions specified in this AD. sradovich on DSK3GMQ082PROD with RULES 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. VerDate Sep<11>2014 16:01 Apr 06, 2018 Jkt 244001 Cost per product Parts cost $0 $170 per test cycle ...... Regulatory Findings § 39.13 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. Cost on U.S. operators $1,020 per test cycle ■ 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 1. The authority citation for part 39 continues to read as follows: ■ Authority: 49 U.S.C. 106(g), 40113, 44701. PO 00000 Frm 00031 Fmt 4700 Sfmt 4700 [Amended] 2. The FAA amends § 39.13 by adding the following new airworthiness directive (AD): 2018–07–12 Airbus: Amendment 39–19243; Docket No. FAA–2018–0269; Product Identifier 2018–NM–051–AD. (a) Effective Date This AD becomes effective April 24, 2018. (b) Affected ADs None. (c) Applicability This AD applies to all Airbus Model A350– 941 airplanes, certificated in any category. (d) Subject Air Transport Association (ATA) of America Code 27, Flight controls. (e) Reason This AD was prompted by a report indicating malfunctions of the station position pick-off unit (SPPU) and failures of the internal wiring due to water ingress via certain electrical connectors, inducing subsequent icing during flight. We are issuing this AD to address a hidden sensor signal drift, which, in combination with an independent failure of a flap down drive disconnect, could lead to in-flight detachment of the outer flap surface, and possibly result in damage to the airplane. (f) Compliance Comply with this AD within the compliance times specified, unless already done. (g) Repetitive SPPU Calibration Tests and Corrective Action Within 200 flight cycles or 30 days after the effective date of this AD, whichever occurs first, accomplish a SPPU calibration test in accordance with the Accomplishment E:\FR\FM\09APR1.SGM 09APR1 15050 Federal Register / Vol. 83, No. 68 / Monday, April 9, 2018 / Rules and Regulations Instructions of Airbus Service Bulletin A350– 27–P021, dated February 13, 2018. If any fault message appears after accomplishment of the SPPU calibration test, before further flight, apply the corresponding airplane fault isolation and continue with the SPPU calibration test. Repeat the SPPU calibration test thereafter at intervals not to exceed 200 flight cycles. (h) Other FAA AD Provisions The following provisions also apply to this AD: (1) Alternative Methods of Compliance (AMOCs): The Manager, International Section, Transport Standards Branch, FAA, has the authority to approve AMOCs for this AD, if requested using the procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request to your principal inspector or local Flight Standards District Office, as appropriate. If sending information directly to the International Section, send it to the attention of the person identified in paragraph (i)(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 Airbus’s EASA Design Organization Approval (DOA). If approved by the DOA, the approval must include the DOAauthorized signature. sradovich on DSK3GMQ082PROD with RULES (i) Related Information (1) Refer to Mandatory Continuing Airworthiness Information (MCAI) EASA Airworthiness Directive 2018–0058, dated March 14, 2018, for related information. You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA–2018–0269. (2) For more information about this AD, contact Kathleen Arrigotti, Aerospace Engineer, International Section, Transport Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; telephone and fax 206–231–3218. (j) 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 A350–27–P021, dated February 13, 2018. (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 VerDate Sep<11>2014 16:01 Apr 06, 2018 Jkt 244001 continued-airworthiness.a350@airbus.com; internet https://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: https:// www.archives.gov/federal-register/cfr/ibrlocations.html. Issued in Des Moines, Washington, on March 27, 2018. Chris Spangenberg, Acting Director, System Oversight Division, Aircraft Certification Service. [FR Doc. 2018–06946 Filed 4–6–18; 8:45 am] BILLING CODE 4910–13–P DEPARTMENT OF TRANSPORTATION Federal Aviation Administration 14 CFR Part 71 [Docket No. FAA–2016–9559; Airspace Docket No. 16–ACE–11] RIN 2120–AA66 Group, Central Service Center, 10101 Hillwood Parkway, Fort Worth, TX 76177; telephone (817) 222–5711. SUPPLEMENTARY INFORMATION: History The FAA published a final rule in the Federal Register (83 FR 5707; February 9, 2018) for Docket No. FAA–2016–9559 modifying Class D airspace at Spirit of St. Louis Airport, St. Louis, MO; Class E airspace designated as a surface area at Cape Girardeau Regional Airport, Cape Girardeau, MO, and Spirit of St. Louis Airport; Class E airspace designated as an extension at Cape Girardeau Regional Airport; and Class E airspace extending upward from 700 feet above the surface at Cape Girardeau Regional Airport, Spirit of St. Louis Airport, and Macon-Fower Memorial Airport, Macon, MO. A typographical error was made in the geographic coordinates for the St. Louis Lambert International Runway 30L Localizer listed in the legal description of Class E airspace extending upward from 700 feet above the surface for St. Louis, MO. This action corrects this error. Correction to Final Rule Amendment of Class D and E Airspace for the Following Missouri Towns; Cape Girardeau, MO; St. Louis, MO; and Macon, MO Federal Aviation Administration (FAA), DOT. ACTION: Final rule, correction. AGENCY: This action corrects the final rule published in the Federal Register on February 9, 2018, modifying Class D airspace at Spirit of St. Louis Airport, St. Louis, MO; Class E airspace designated as a surface area at Cape Girardeau Regional Airport, Cape Girardeau, MO, and Spirit of St. Louis Airport; Class E airspace designated as an extension at Cape Girardeau Regional Airport; and Class E airspace extending upward from 700 feet above the surface at Cape Girardeau Regional Airport, Spirit of St. Louis Airport, and MaconFower Memorial Airport, Macon, MO. A typographical error was made in the geographic coordinates for the St. Louis Lambert International Runway 30L Localizer listed in the legal description of the Class E airspace extending upward from 700 feet above the surface for St. Louis, MO. DATES: Effective date 0901 UTC, May 24, 2018. FOR FURTHER INFORMATION CONTACT: Jeffrey Claypool, Federal Aviation Administration, Operations Support SUMMARY: PO 00000 Frm 00032 Fmt 4700 Sfmt 9990 Accordingly, pursuant to the authority delegated to me, in the Federal Register of February 9, 2018 (83 FR 5707) FR Doc. 2018–02139, Amendment of Class D and E Airspace for the Following Missouri Towns; Cape Girardeau, MO; St. Louis, MO; and Macon, MO, is corrected as follows: § 71.1 [Amended] ACE MO E5 St. Louis, MO [Corrected] On page 5710, column 2, line 38, remove (lat. 38°45′44″ N, long. 90°22′56″ W) and add in its place (lat. 38°45′19″ N, long. 90°22′56″ W). Issued in Fort Worth, Texas, on April 2, 2018. Christopher L. Southerland, Acting Manager, Operations Support Group, ATO Central Service Center. [FR Doc. 2018–07100 Filed 4–6–18; 8:45 am] BILLING CODE 4910–13–P E:\FR\FM\09APR1.SGM 09APR1

Agencies

[Federal Register Volume 83, Number 68 (Monday, April 9, 2018)]
[Rules and Regulations]
[Pages 15048-15050]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2018-06946]


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

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2018-0269; Product Identifier 2018-NM-051-AD; Amendment 
39-19243; AD 2018-07-12]
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 A350-941 airplanes. This AD requires performing repetitive 
station position pick-off unit (SPPU) calibration tests, and applying 
the corresponding airplane fault isolation if necessary. This AD was 
prompted by a report indicating malfunctions of the SPPU and failures 
of the internal wiring due to water ingress via certain electrical 
connectors, inducing subsequent icing during flight. We are issuing 
this AD to address the unsafe condition on these products.

DATES: This AD becomes effective April 24, 2018.
    The Director of the Federal Register approved the incorporation by 
reference of a certain publication listed in this AD as of April 24, 
2018.
    We must receive comments on this AD by May 24, 2018.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
     Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
     Fax: 202-493-2251.
     Mail: U.S. Department of Transportation, Docket 
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New 
Jersey Avenue SE, Washington, DC 20590.
     Hand Delivery: 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 
https://www.airbus.com. You may view this referenced service information 
at the FAA, Transport Standards Branch, 2200 South 216th St., Des 
Moines, WA. For information on the availability of this material at the 
FAA, call 206-231-3195. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0269.

Examining the AD Docket

    You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0269; 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: Kathleen Arrigotti, Aerospace 
Engineer, International Section, Transport Standards Branch, FAA, 2200 
South 216th St., Des Moines, WA 98198; telephone and fax 206-231-3218.

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 2018-0058, dated March 14, 2018 (referred to 
after this as the Mandatory Continuing Airworthiness Information, or 
``the MCAI''), to correct an unsafe condition for all Airbus Model 
A350-941 airplanes. The MCAI states:

    Occurrences have been reported by Airbus A350 operators of 
malfunctions of Station Position Pick-Off Units (SPPU). 
Investigations indicated that internal wiring failures occurred due 
to water ingress via certain electrical connectors, inducing 
subsequent icing during flight.
    This condition, if not detected and corrected, could lead to 
hidden sensor signal drift (at flap station 3) which, in combination 
with an independent failure of a flap down drive disconnect, might 
lead to in-flight detachment of the outer flap surface, possibly 
resulting in damage to the aeroplane, and/or injury to persons on 
the ground.
    Airbus determined that the SPPU calibration test can highlight 
all hidden faults, but this test is only scheduled after removal/
installation of the equipment. Consequently, to address this 
potential unsafe condition, Airbus issued the SB [Service Bulletin 
A350-27-P021, dated February 13, 2018], providing instructions to 
accomplish the SPPU calibration test at regular intervals.
    For the reason described above, this [EASA] AD requires 
repetitive SPPU calibration test and, depending on findings, 
accomplishment of applicable corrective action(s) [applying 
corresponding airplane fault isolation].
    Pending the results of the on-going investigation, this [EASA] 
AD is still considered to be an interim measure and further [EASA] 
AD action may follow.

    You may examine the MCAI on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2018-
0269.

Related Service Information Under 1 CFR Part 51

    Airbus has issued Service Bulletin A350-27-P021, dated February 13, 
2018. The service information describes performing repetitive SPPU 
calibration tests, and applying the corresponding airplane fault 
isolation if necessary. 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 the same 
type design.

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

[[Page 15049]]

rule because malfunctions of the SPPU and failures of the internal 
wiring due to water ingress via certain electrical connectors can 
induce icing, which under certain conditions, could lead to in-flight 
detachment of the outer flap surface, and consequent damage to the 
airplane. 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 data, views, or 
arguments about this AD. Send your comments to an address listed under 
the ADDRESSES section. Include ``Docket No. FAA-2018-0269; Product 
Identifier 2018-NM-051-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 https://www.regulations.gov, including any personal information you provide. We 
will also post a report summarizing each substantive verbal contact we 
receive about this AD.

Costs of Compliances

    We estimate that this AD affects 6 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
----------------------------------------------------------------------------------------------------------------
SPPU calibration test..........  2 work-hours x $85 per               $0  $170 per test       $1,020 per test
                                  hour = $170 per test                     cycle.              cycle
                                  cycle.
----------------------------------------------------------------------------------------------------------------

    We have received no definitive data that would enable us to provide 
cost estimates for the on-condition actions specified in this AD.

Authority for This Rulemaking

    Title 49 of the United States Code specifies the FAA's authority to 
issue rules on aviation safety. Subtitle I, section 106, describes the 
authority of the FAA Administrator. Subtitle VII: Aviation Programs, 
describes in more detail the scope of the Agency's authority.
    We are issuing this rulemaking under the authority described in 
Subtitle VII, Part A, Subpart III, Section 44701: ``General 
requirements.'' Under that section, Congress charges the FAA with 
promoting safe flight of civil aircraft in air commerce by prescribing 
regulations for practices, methods, and procedures the Administrator 
finds necessary for safety in air commerce. This regulation is within 
the scope of that authority because it addresses an unsafe condition 
that is likely to exist or develop on products identified in this 
rulemaking action.
    This AD is issued in accordance with authority delegated by the 
Executive Director, Aircraft Certification Service, as authorized by 
FAA Order 8000.51C. In accordance with that order, issuance of ADs is 
normally a function of the Compliance and Airworthiness Division, but 
during this transition period, the Executive Director has delegated the 
authority to issue ADs applicable to transport category airplanes to 
the Director of the System Oversight Division.

Regulatory Findings

    We determined that this AD will not have federalism implications 
under Executive Order 13132. This AD will not have a substantial direct 
effect on the States, on the relationship between the national 
government and the States, or on the distribution of power and 
responsibilities among the various levels of government.
    For the reasons discussed above, I certify that this AD:
    1. Is not a ``significant regulatory action'' under Executive Order 
12866;
    2. Is not a ``significant rule'' under the DOT Regulatory Policies 
and Procedures (44 FR 11034, February 26, 1979);
    3. Will not affect intrastate aviation in Alaska; and
    4. Will not have a significant economic impact, positive or 
negative, on a substantial number of small entities under the criteria 
of the Regulatory Flexibility Act.

List of Subjects in 14 CFR Part 39

    Air transportation, Aircraft, Aviation safety, Incorporation by 
reference, Safety.

Adoption of the Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA amends 14 CFR part 39 as follows:

PART 39--AIRWORTHINESS DIRECTIVES

0
1. The authority citation for part 39 continues to read as follows:

    Authority: 49 U.S.C. 106(g), 40113, 44701.


Sec.  39.13  [Amended]

0
2. The FAA amends Sec.  39.13 by adding the following new airworthiness 
directive (AD):

2018-07-12 Airbus: Amendment 39-19243; Docket No. FAA-2018-0269; 
Product Identifier 2018-NM-051-AD.

(a) Effective Date

    This AD becomes effective April 24, 2018.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Airbus Model A350-941 airplanes, 
certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 27, Flight 
controls.

(e) Reason

    This AD was prompted by a report indicating malfunctions of the 
station position pick-off unit (SPPU) and failures of the internal 
wiring due to water ingress via certain electrical connectors, 
inducing subsequent icing during flight. We are issuing this AD to 
address a hidden sensor signal drift, which, in combination with an 
independent failure of a flap down drive disconnect, could lead to 
in-flight detachment of the outer flap surface, and possibly result 
in damage to the airplane.

(f) Compliance

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

(g) Repetitive SPPU Calibration Tests and Corrective Action

    Within 200 flight cycles or 30 days after the effective date of 
this AD, whichever occurs first, accomplish a SPPU calibration test 
in accordance with the Accomplishment

[[Page 15050]]

Instructions of Airbus Service Bulletin A350-27-P021, dated February 
13, 2018. If any fault message appears after accomplishment of the 
SPPU calibration test, before further flight, apply the 
corresponding airplane fault isolation and continue with the SPPU 
calibration test. Repeat the SPPU calibration test thereafter at 
intervals not to exceed 200 flight cycles.

(h) Other FAA AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
International Section, Transport Standards Branch, FAA, has the 
authority to approve AMOCs for this AD, if requested using the 
procedures found in 14 CFR 39.19. In accordance with 14 CFR 39.19, 
send your request to your principal inspector or local Flight 
Standards District Office, as appropriate. If sending information 
directly to the International Section, send it to the attention of 
the person identified in paragraph (i)(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.

(i) Related Information

    (1) Refer to Mandatory Continuing Airworthiness Information 
(MCAI) EASA Airworthiness Directive 2018-0058, dated March 14, 2018, 
for related information. You may examine the MCAI on the internet at 
https://www.regulations.gov by searching for and locating Docket No. 
FAA-2018-0269.
    (2) For more information about this AD, contact Kathleen 
Arrigotti, Aerospace Engineer, International Section, Transport 
Standards Branch, FAA, 2200 South 216th St., Des Moines, WA 98198; 
telephone and fax 206-231-3218.

(j) 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 A350-27-P021, dated February 13, 
2018.
    (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 https://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: https://www.archives.gov/federal-register/cfr/ibr-locations.html.

    Issued in Des Moines, Washington, on March 27, 2018.
Chris Spangenberg,
Acting Director, System Oversight Division, Aircraft Certification 
Service.
[FR Doc. 2018-06946 Filed 4-6-18; 8:45 am]
 BILLING CODE 4910-13-P
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