AD 2020-05-18

[Federal Register Volume 85, Number 51 (Monday, March 16, 2020)]
[Rules and Regulations]
[Pages 14784-14786]
From the Federal Register Online via the Government Publishing Office [<a href="http://www.gpo.gov">www.gpo.gov</a>]
[FR Doc No: 2020-05264]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2019-0979; Product Identifier 2019-NM-182-AD; Amendment 
39-19868; AD 2020-05-18]
RIN 2120-AA64


Airworthiness Directives; Airbus SAS Airplanes

AGENCY: Federal Aviation Administration (FAA), Department of 
Transportation (DOT).

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for 
certain Airbus SAS Model A350-941 and -1041 airplanes. This AD was 
prompted by a report of incorrectly engaged lock washer tabs of the 
main landing gear (MLG) forward pintle bearing (FPB) at the forward 
face of the trunnion block. This AD requires detailed inspections of 
the left-hand (LH) and right-hand (RH) side MLG FPB nuts and lock 
washer tabs, and depending on findings, accomplishment of repetitive 
detailed inspections or corrective actions, as specified in a European 
Union Aviation Safety Agency (EASA) AD, which is incorporated by 
reference. The FAA is issuing this AD to address the unsafe condition 
on these products.

DATES: This AD is effective April 20, 2020.
    The Director of the Federal Register approved the incorporation by 
reference

[[Page 14785]]

of a certain publication listed in this AD as of April 20, 2020.

ADDRESSES: For the material incorporated by reference (IBR) in this AD, 
contact the EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; 
phone: +49 221 89990 1000; email: <a href="/cdn-cgi/l/email-protection#e5a4a196a580849684cb8090978a9584cb8090"><span class="__cf_email__" data-cfemail="46070235062327352768233334293627682333">[email&#160;protected]</span></a>; internet: 
www.easa.europa.eu. You may find this IBR material on the EASA website 
at <a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</a>. You may view this IBR material 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 in the AD docket on the internet at 
<a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. 
FAA-2019-0979.

Examining the AD Docket

    You may examine the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-2019-
0979; 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 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: Kathleen Arrigotti, Aerospace 
Engineer, International Section, Transport Standards Branch, FAA, 2200 
South 216th St., Des Moines, WA 98198; phone and fax: 206-231-3218; 
email: <a href="/cdn-cgi/l/email-protection#fb909a8f93979e9e95d59a8989929c948f8f92bb9d9a9ad59c948d"><span class="__cf_email__" data-cfemail="e28983968a8e87878ccc8390908b858d96968ba2848383cc858d94">[email&#160;protected]</span></a>.

SUPPLEMENTARY INFORMATION: 

Discussion

    The EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2019-0265, dated October 25, 2019 
(``EASA AD 2019-0265'') (also referred to as the Mandatory Continuing 
Airworthiness Information, or ``the MCAI''), to correct an unsafe 
condition for certain Airbus SAS Model A350-941 and -1041 airplanes.
    The FAA 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 A350-941 and -1041 airplanes. The NPRM published in the Federal 
Register on December 13, 2019 (84 FR 68063). The NPRM was prompted by a 
report of incorrectly engaged lock washer tabs of the MLG FPB at the 
forward face of the trunnion block. The NPRM proposed to require 
detailed inspections of the LH and RH side MLG FPB nuts and lock washer 
tabs, and depending on findings, accomplishment of repetitive detailed 
inspections or corrective actions, as specified in an EASA AD.
    The FAA is issuing this AD to address absence of an engaged lock 
washer tab at the bearing nut, which could cause an unexpected rotation 
of the nut and loss of torque, progressively allowing an axial movement 
of the bearing housing. This condition, if not detected and corrected, 
could lead to collapse of a MLG, possibly resulting in damage to the 
airplane and/or injury to occupants. See the MCAI for additional 
background information.

Comments

    The FAA gave the public the opportunity to participate in 
developing this final rule. The FAA has considered the comment 
received. Air Line Pilots Association, International (ALPA) indicated 
its support for the NPRM.

Conclusion

    The FAA reviewed the relevant data, considered the comment 
received, and determined that air safety and the public interest 
require adopting this final rule as proposed, except for minor 
editorial changes. The FAA has determined that these minor changes:
    <bullet> Are consistent with the intent that was proposed in the 
NPRM for addressing the unsafe condition; and
    <bullet> Do not add any additional burden upon the public than was 
already proposed in the NPRM.

Related IBR Material Under 1 CFR Part 51

    EASA AD 2019-0265 describes procedures for detailed inspections of 
the LH and RH side MLG FPB nuts and lock washer tabs for any MLG FPB 
nut not correctly locked by the lock washer tab, and depending on 
findings, accomplishment of repetitive detailed inspections for 
discrepancies or corrective actions. Corrective actions include bending 
the washer tab to lock the bearing nut and replacing any parts that 
have damage or wear. This material 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

    The FAA estimates that this AD affects 12 airplanes of U.S. 
registry. The FAA estimates the following costs to comply with this AD:

                                      Estimated Costs for Required Actions
----------------------------------------------------------------------------------------------------------------
                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
2 work-hours x $85 per hour = $170...........................              $0             $170           $2,040
----------------------------------------------------------------------------------------------------------------

    The FAA has 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.
    The FAA is 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.

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

[[Page 14786]]

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) Will not affect intrastate aviation in Alaska, and
    (3) 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):

2020-05-18 Airbus SAS: Amendment 39-19868; Docket No. FAA-2019-0979; 
Product Identifier 2019-NM-182-AD.

(a) Effective Date

    This AD is effective April 20, 2020.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Airbus SAS Model A350-941 and -1041 
airplanes, certificated in any category, as identified in European 
Union Aviation Safety Agency (EASA) AD 2019-0265, dated October 25, 
2019 (``EASA AD 2019-0265'').

(d) Subject

    Air Transport Association (ATA) of America Code 57, Wings.

(e) Reason

    This AD was prompted by a report of incorrectly engaged lock 
washer tabs of the main landing gear (MLG) forward pintle bearing 
(FPB) at the forward face of the trunnion block. The FAA is issuing 
this AD to address absence of an engaged lock washer tab at the 
bearing nut, which could cause an unexpected rotation of the nut and 
loss of torque, progressively allowing an axial movement of the 
bearing housing. This condition, if not detected and corrected, 
could lead to collapse of a MLG, possibly resulting in damage to the 
airplane and/or injury to occupants.

(f) Compliance

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

(g) Requirements

    Except as specified in paragraph (h) of this AD: Comply with all 
required actions and compliance times specified in, and in 
accordance with, EASA AD 2019-0265.

(h) Exceptions to EASA AD 2019-0265

    (1) Where EASA AD 2019-0265 refers to its effective date, this 
AD requires using the effective date of this AD.
    (2) The ``Remarks'' section of EASA AD 2019-0265 does not apply 
to this AD.

(i) No Reporting Requirement

    Although the service information referenced in EASA AD 2019-0265 
specifies to submit certain information to the manufacturer, this AD 
does not include that requirement.

(j) 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 (k) of this AD. Information may 
be emailed to: <a href="/cdn-cgi/l/email-protection#0d34204c4340203c3c3b204c40424e205f485c58485e595e4d6b6c6c236a627b"><span class="__cf_email__" data-cfemail="241d09656a69091515120965696b67097661757161777077644245450a434b52">[email&#160;protected]</span></a>. 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 instructions from a manufacturer, the instructions must be 
accomplished using a method approved by the Manager, International 
Section, Transport Standards Branch, FAA; or EASA; or Airbus SAS's 
EASA Design Organization Approval (DOA). If approved by the DOA, the 
approval must include the DOA-authorized signature.
    (3) Required for Compliance (RC): For any service information 
referenced in EASA AD 2019-0265 that contains RC procedures and 
tests: Except as required by paragraph (j)(2) of this AD, RC 
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.

(k) Related Information

    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; phone and 
fax: 206-231-3218; email: <a href="/cdn-cgi/l/email-protection#8fe4eefbe7e3eaeae1a1eefdfde6e8e0fbfbe6cfe9eeeea1e8e0f9"><span class="__cf_email__" data-cfemail="8ce7edf8e4e0e9e9e2a2edfefee5ebe3f8f8e5cceaededa2ebe3fa">[email&#160;protected]</span></a>.

(l) 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) European Union Aviation Safety Agency (EASA) AD 2019-0265, 
dated October 25, 2019.
    (ii) [Reserved]
    (3) For information about EASA AD 2019-0265, contact the EASA, 
Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; phone: +49 221 89990 
6017; email: <a href="/cdn-cgi/l/email-protection#dd9c99ae9db8bcaebcf3b8a8afb2adbcf3b8a8"><span class="__cf_email__" data-cfemail="b1f0f5c2f1d4d0c2d09fd4c4c3dec1d09fd4c4">[email&#160;protected]</span></a>; internet: www.easa.europa.eu. You 
may find this EASA AD on the EASA website at <a href="https://ad.easa.europa.eu">https://ad.easa.europa.eu</a>.
    (4) You may view this material 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. This 
material may be found in the AD docket on the internet at <a href="https://www.regulations.gov">https://www.regulations.gov</a> by searching for and locating Docket No. FAA-
2019-0979.
    (5) You may view this material that is incorporated by reference 
at the National Archives and Records Administration (NARA). For 
information on the availability of this material at NARA, email 
<a href="/cdn-cgi/l/email-protection#117774756374763f7d7476707d517f7063703f767e67"><span class="__cf_email__" data-cfemail="fe989b9a8c9b99d0929b999f92be909f8c9fd0999188">[email&#160;protected]</span></a>, or go to: <a href="https://www.archives.gov/federal-register/cfr/ibr-locations.html">https://www.archives.gov/federal-register/cfr/ibr-locations.html</a>.

    Issued on March 4, 2020.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2020-05264 Filed 3-13-20; 8:45 am]
 BILLING CODE 4910-13-P