[Federal Register Volume 87, Number 132 (Tuesday, July 12, 2022)]
[Proposed Rules]
[Pages 41265-41267]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-14691]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0817; Project Identifier MCAI-2022-00369-T]
RIN 2120-AA64


Airworthiness Directives; Airbus SAS Airplanes

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD) 
for certain Airbus SAS Model Airbus A350-941 and A350-1041 airplanes. 
This proposed AD was prompted by a determination that, in the event of 
rapid decompression at a specific location of the airplane, possible 
deflections of the passenger floor cross beams may result in wiring 
damages, leading to potential system losses. This proposed AD would 
require amending the existing airplane flight manual (AFM) to update 
the landing performance database, as specified in a European Union 
Aviation Safety Agency (EASA) AD, which is proposed for incorporation 
by reference. The FAA is proposing this AD to address the unsafe 
condition on these products.

DATES: The FAA must receive comments on this proposed AD by August 26, 
2022.

ADDRESSES: You may send comments, using the procedures found in 14 CFR 
11.43 and 11.45, by any of the following methods:
    <bullet> Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
    <bullet> Fax: 202-493-2251.
    <bullet> 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.
    <bullet> Hand Delivery: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For material that will be incorporated by reference (IBR) in this 
AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany; 
telephone +49 221 8999 000; email <a href="/cdn-cgi/l/email-protection#6425201724010517054a0111160b14054a0111"><span class="__cf_email__" data-cfemail="d9989daa99bcb8aab8f7bcacabb6a9b8f7bcac">[email protected]</span></a>; internet 
www.easa.europa.eu. You may find this material on the EASA website at 
https://ad.easa.europa.eu. You may view this material at the FAA, 
Airworthiness Products Section, Operational Safety 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 at https://www.regulations.gov by searching for and locating 
Docket No. FAA-2022-0817.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2022-0817; 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 NPRM, the 
mandatory continuing airworthiness information (MCAI), any comments 
received, and other information. The street address for Docket 
Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Dan Rodina, Aerospace Engineer, Large 
Aircraft Section, International Validation Branch, FAA, 2200 South 
216th Street, Des Moines, WA 98198; telephone 206-231-3225; email 
<a href="/cdn-cgi/l/email-protection#f397929ddd819c979a9d92b3959292dd949c85"><span class="__cf_email__" data-cfemail="bdd9dcd393cfd2d9d4d3dcfddbdcdc93dad2cb">[email protected]</span></a>.

SUPPLEMENTARY INFORMATION: 

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposal. Send your comments to an address listed 
under ADDRESSES. Include ``Docket No. FAA-2022-0817; Project Identifier 
MCAI-2022-00369-T'' at the beginning of your comments. The most helpful 
comments reference a specific portion of the proposal, explain the 
reason for any recommended change, and include supporting data. The FAA 
will consider all comments received by the closing date and may amend 
this proposal because of those comments.
    Except for Confidential Business Information (CBI) as described in 
the following paragraph, and other information as described in 14 CFR 
11.35, the FAA will post all comments received, without change, to 
https://www.regulations.gov, including any personal information you 
provide. The agency will also post a report summarizing each 
substantive verbal contact received about this NPRM.

Confidential Business Information

    CBI is commercial or financial information that is both customarily 
and actually treated as private by its owner. Under the Freedom of 
Information Act (FOIA) (5 U.S.C. 552), CBI is exempt from public 
disclosure. If your comments responsive to this NPRM contain commercial 
or financial information that is customarily treated as private, that 
you actually treat as private, and that is relevant or responsive to 
this NPRM, it is important that you clearly designate the submitted 
comments as CBI. Please mark each page of your submission containing 
CBI as ``PROPIN.'' The FAA will treat such marked submissions as 
confidential under the FOIA, and they will not be placed in the public 
docket of this NPRM. Submissions containing CBI should be sent to Dan 
Rodina, Aerospace Engineer, Large Aircraft Section, International 
Validation Branch, FAA, 2200 South 216th Street, Des Moines, WA 98198; 
telephone and 206-231-3225; email <a href="/cdn-cgi/l/email-protection#ee8a8f80c09c818a87808fae888f8fc0898198"><span class="__cf_email__" data-cfemail="aecacfc080dcc1cac7c0cfeec8cfcf80c9c1d8">[email protected]</span></a>. Any commentary 
that the FAA receives which is not specifically designated as CBI will 
be placed in the public docket for this rulemaking.

Background

    EASA, which is the Technical Agent for the Member States of the 
European Union, has issued EASA AD 2022-0054, dated March 23, 2022 
(EASA AD 2022-0054) (also referred to as the MCAI), to correct an 
unsafe condition for certain Airbus A350-941 and A350-1041 airplanes. 
EASA AD 2022-0054 supersedes EASA AD 2022-0045, dated March 16, 2022 
(EASA AD 2022-0045), which was issued to correct the unsafe condition. 
However, the revision of the AFM referenced in EASA AD 2022-0045 did 
not include the required amendments.

[[Page 41266]]

    This proposed AD was prompted by a determination that, in the event 
of rapid decompression at a specific location of the airplane, possible 
deflections of the passenger floor cross beams may result in wiring 
damages, leading to potential system losses. The FAA is proposing this 
AD to address this potential unsafe condition, which could lead to an 
increase of the landing distance, exceeding the value provided in the 
current in-flight failure data file for landing, and potentially 
resulting in a runway excursion. See the MCAI for additional background 
information.

Related Service Information Under 1 CFR Part 51

    EASA AD 2022-0054 describes procedures for revising the existing 
Airbus A350 AFM to update the landing performance database.
    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.

FAA's Determination

    This product has been approved by the aviation authority of another 
country and is approved for operation in the United States. Pursuant to 
the FAA's bilateral agreement with the State of Design Authority, it 
has notified the FAA of the unsafe condition described in the MCAI 
referenced above. The FAA is issuing this NPRM after determining that 
the unsafe condition described previously is likely to exist or develop 
in other products of the same type design.

Proposed AD Requirements in This NPRM

    This proposed AD would require accomplishing the actions specified 
in EASA AD 2022-0054 described previously, except for any differences 
identified as exceptions in the regulatory text of this proposed AD.
    EASA AD 2022-0054 requires operators to ``inform all flight crews'' 
of revisions to the AFM, and thereafter to ``operate the aeroplane 
accordingly.'' However, this proposed AD would not specifically require 
those actions as those actions are already required by FAA regulations. 
FAA regulations require operators furnish to pilots any changes to the 
AFM (for example, 14 CFR 121.137), and to ensure the pilots are 
familiar with the AFM (for example, 14 CFR 91.505). As with any other 
flight crew training requirement, training on the updated AFM content 
is tracked by the operators and recorded in each pilot's training 
record, which is available for the FAA to review. FAA regulations also 
require pilots to follow the procedures in the existing AFM including 
all updates. 14 CFR 91.9 requires that any person operating a civil 
aircraft must comply with the operating limitations specified in the 
AFM. Therefore, including a requirement in this proposed AD to operate 
the airplane according to the revised AFM would be redundant and 
unnecessary. Further, compliance with such a requirement in an AD would 
be impracticable to demonstrate or track on an ongoing basis; 
therefore, a requirement to operate the airplane in such a manner would 
be unenforceable.

Explanation of Required Compliance Information

    In the FAA's ongoing efforts to improve the efficiency of the AD 
process, the FAA developed a process to use some civil aviation 
authority (CAA) ADs as the primary source of information for compliance 
with requirements for corresponding FAA ADs. The FAA has been 
coordinating this process with manufacturers and CAAs. As a result, the 
FAA proposes to incorporate EASA AD 2022-0054 by reference in the FAA 
final rule. This proposed AD would, therefore, require compliance with 
EASA AD 2022-0054 in its entirety through that incorporation, except 
for any differences identified as exceptions in the regulatory text of 
this proposed AD. Using common terms that are the same as the heading 
of a particular section in EASA AD 2022-0054 does not mean that 
operators need comply only with that section. For example, where the AD 
requirement refers to ``all required actions and compliance times,'' 
compliance with this AD requirement is not limited to the section 
titled ``Required Action(s) and Compliance Time(s)'' in EASA AD 2022-
0054. Service information required by EASA AD 2022-0054 for compliance 
will be available at https://www.regulations.gov by searching for and 
locating Docket No. FAA-2022-0817 after the FAA final rule is 
published.

Costs of Compliance

    The FAA estimates that this proposed AD would affect 30 airplanes 
of U.S. registry. The FAA estimates the following costs to comply with 
this proposed AD:

                                      Estimated Costs for Required Actions
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                                                                                    Cost per       Cost on U.S.
                          Labor cost                              Parts cost        product         operators
----------------------------------------------------------------------------------------------------------------
1 work-hour x $85 per hour = $85.............................              $0              $85           $2,550
----------------------------------------------------------------------------------------------------------------

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

    The FAA determined that this proposed AD would not have federalism 
implications under Executive Order 13132. This proposed AD would 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 this proposed 
regulation:
    (1) Is not a ``significant regulatory action'' under Executive 
Order 12866,
    (2) Would not affect intrastate aviation in Alaska, and
    (3) Would not have a significant economic impact, positive or 
negative, on a substantial number of small entities

[[Page 41267]]

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.

The Proposed Amendment

    Accordingly, under the authority delegated to me by the 
Administrator, the FAA proposes to amend 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:

Airbus SAS: Docket No. FAA-2022-0817; Project Identifier MCAI-2022-
00369-T.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) by August 26, 2022.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to all Airbus SAS Model A350-941 and A350-1041 
airplanes, certificated in any category.

(d) Subject

    Air Transport Association (ATA) of America Code 53, Fuselage.

(e) Unsafe Condition

    This AD was prompted by a determination that, in the event of 
rapid decompression at a specific location of the airplane, possible 
deflections of the passenger floor crossbeams may result in wiring 
damages, leading to potential system losses. The FAA is issuing this 
AD to address this unsafe condition, which could lead to an increase 
of the landing distance, exceeding the value provided in the current 
in-flight failure data file for landing, and potentially resulting 
in a runway excursion.

(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, European Union Aviation Safety Agency (EASA) AD 
2022-0054, dated March 23, 2022 (EASA AD 2022-0054).

(h) Exceptions to EASA AD 2022-0054

    (1) Where EASA AD 2022-0054 refers to March 30, 2022 (the 
effective date of EASA AD 2022-0045, dated March 16, 2022), this AD 
requires using the effective date of this AD.
    (2) Where EASA AD 2022-0054 specifies to ``inform all flight 
crews, and thereafter, operate the aeroplane accordingly'' this AD 
does not require those actions as those actions are already required 
by existing FAA operating regulations.
    (3) Where the ``AFM Amendment'' paragraph of EASA AD 2022-0054 
specifies implementing an AFM [airplane flight manual] revision, for 
this AD, replace the text ''implement the AFM revision, as defined 
in this [EASA] AD'' with ``revise the existing AFM to incorporate 
the aircraft performance database specified in the AFM revision, as 
defined in this [EASA] AD.''
    (4) The ``Remarks'' section of EASA AD 2022-0054 does not apply 
to this AD.

(i) Additional AD Provisions

    The following provisions also apply to this AD:
    (1) Alternative Methods of Compliance (AMOCs): The Manager, 
Large Aircraft Section, International Validation 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 responsible Flight 
Standards Office, as appropriate. If sending information directly to 
the Large Aircraft Section, International Validation Branch, send it 
to the attention of the person identified in paragraph (j)(2) of 
this AD. Information may be emailed to: <a href="/cdn-cgi/l/email-protection#bd8490fcebee90fcf4ef908a8e8d90fcf0f2fefddbdcdc93dad2cb"><span class="__cf_email__" data-cfemail="261f0b6770750b676f740b1115160b676b69656640474708414950">[email protected]</span></a>. 
Before using any approved AMOC, notify your appropriate principal 
inspector, or lacking a principal inspector, the manager of the 
responsible Flight Standards 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, Large Aircraft 
Section, International Validation 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): Except as required by 
paragraph (i)(2) of this AD, if any service information contains 
procedures or tests that are identified as RC, those procedures and 
tests must be done to comply with this AD; any procedures or tests 
that are not identified as RC are recommended. Those procedures and 
tests that are not identified as RC may be deviated from using 
accepted methods in accordance with the operator's maintenance or 
inspection program without obtaining approval of an AMOC, provided 
the procedures and tests identified as RC can be done and the 
airplane can be put back in an airworthy condition. Any 
substitutions or changes to procedures or tests identified as RC 
require approval of an AMOC.

(j) Related Information

    (1) For EASA AD 2022-0054, contact EASA, Konrad-Adenauer-Ufer 3, 
50668 Cologne, Germany; telephone +49 221 8999 000; email 
<a href="/cdn-cgi/l/email-protection#19585d6a597c786a78377c6c6b766978377c6c"><span class="__cf_email__" data-cfemail="f9b8bd8ab99c988a98d79c8c8b968998d79c8c">[email protected]</span></a>; internet www.easa.europa.eu. You may find this 
EASA AD on the EASA website at https://ad.easa.europa.eu. You may 
view this material at the FAA, Airworthiness Products Section, 
Operational Safety 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 at https://www.regulations.gov by searching for and locating Docket No. FAA-
2022-0817.
    (2) For more information about this AD, contact Dan Rodina, 
Aerospace Engineer, Large Aircraft Section, International Validation 
Branch, FAA, 2200 South 216th Street, Des Moines, WA 98198; 
telephone 206-231-3225; email <a href="/cdn-cgi/l/email-protection#dbbfbab5f5a9b4bfb2b5ba9bbdbabaf5bcb4ad"><span class="__cf_email__" data-cfemail="b3d7d2dd9dc1dcd7daddd2f3d5d2d29dd4dcc5">[email protected]</span></a>.

    Issued on July 5, 2022.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft 
Certification Service.
[FR Doc. 2022-14691 Filed 7-11-22; 8:45 am]
BILLING CODE 4910-13-P


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