[Federal Register Volume 87, Number 28 (Thursday, February 10, 2022)]
[Proposed Rules]
[Pages 7770-7774]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2022-02768]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0096; Project Identifier MCAI-2021-01092-R]
RIN 2120-AA64


Airworthiness Directives; Airbus Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of proposed rulemaking (NPRM).

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SUMMARY: The FAA proposes to supersede Airworthiness Directive (AD) 
2020-22-01 which applies to all Airbus Helicopters Model AS332C, 
AS332C1, AS332L, and AS332L1 helicopters. AD 2020-22-01 requires 
inspecting the affected parts and associated frame bores for 
discrepancies, applicable corrective actions, and reporting certain 
information if necessary. Since the FAA issued AD 2020-22-01, a 
significant number of reports were received of finding corrosion on the 
affected parts. This proposed AD would retain the requirements of AD 
2020-22-01, add recurring inspections, and update the applicable 
service information. 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 March 28, 
2022.

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: Deliver to Mail address above between 9 
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
    For service information identified in this NPRM, contact Airbus 
Helicopters, 2701 N. Forum Drive, Grand Prairie, TX, 75052, telephone: 
(972) 641-0000; or (800) 232-0323; fax (972) 641-3775; or at https://www.airbus.com/helicopters/services/technical-support.html. You may 
view this referenced service information at the FAA, Office of the 
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321, 
Fort Worth, TX 76177. For information on the availability of this 
material at the FAA, call (817) 222-5110.

[[Page 7771]]

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by 
searching for and locating Docket No. FAA-2022-0096; 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 European 
Union Aviation Safety Agency (EASA) AD, any comments received, and 
other information. The street address for Docket Operations is listed 
above.

FOR FURTHER INFORMATION CONTACT: Andrea Jimenez, Aerospace Engineer, 
COS Program Management Section, Operational Safety Branch, Compliance & 
Airworthiness Division, FAA, 1600 Stewart Ave., Suite 410, Westbury, NY 
11590; telephone (516) 228-7330; email [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    The FAA invites you to send any written relevant data, views, or 
arguments about this proposed AD. Send your comments to an address 
listed under the ADDRESSES. Include ``Docket No. FAA-2022-0096; Project 
Identifier MCAI-2021-01092-R'' 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 
Andrea Jimenez, Aerospace Engineer, COS Program Management Section, 
Operational Safety Branch, Compliance & Airworthiness Division, FAA, 
1600 Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-
7330; email [email protected]. Any commentary that the FAA 
receives which is not specifically designated as CBI will be placed in 
the public docket for this rulemaking.

Background

    The FAA issued AD 2020-22-01, Amendment 39-21297 (85 FR 69126, 
November 2, 2020), (AD 2020-22-01), for all Airbus Helicopters Model 
AS332C, AS332C1, AS332L, and AS332L1 helicopters. AD 2020-22-01 
requires, within certain compliance times specified in the 
manufacturers service information, inspecting the attachment fittings 
and attachment screws of the main gearbox (MGB) suspension bars and 
their frame bores for discrepancies and corrective actions in 
accordance with the actions specified in the service information. AD 
2020-22-01 also requires sending certain information to the 
manufacturer. AD 2020-22-01 resulted from reports of corrosion on 
attachment screws and fittings fastening the MGB suspension bars to the 
fuselage. The FAA issued AD 2020-22-01 to address corrosion on 
attachment fittings and attachment screws for the MGB suspension bars.
    AD 2020-22-01 was prompted by EASA AD 2019-0295, dated December 5, 
2019 (EASA AD 2019-0295), issued by EASA, which is the Technical Agent 
for the Member States of the European Union, to correct an unsafe 
condition for all Airbus Helicopters Model AS 332 C, AS 332 C1, AS 332 
L, and AS 332 L1 helicopters, all manufacturer serial numbers. EASA 
advised that there were reports of corrosion on attachment screws and 
fittings fastening the rear MGB suspension bars, right and left hand 
sides, to the fuselage, and the attachment screws and fitting fastening 
the front MGB suspension bar to the fuselage. EASA advised that 
subsequent investigation determined that during maintenance visits of 
an identified batch of helicopters between September 2012 and April 
2019, application of compound sealant on MGB suspension bar attachment 
screws may not have been accomplished using the approved maintenance 
data. This condition, if not addressed, could lead to structural 
failure of the MGB attachment screws, resulting in detachment of MGB 
suspension bars from the fuselage and subsequent loss of control of the 
helicopter.
    Accordingly, EASA AD 2019-0295 required a one-time inspection of 
the affected parts, and depending on findings, accomplishment of 
applicable corrective actions. The compliance times varied depending on 
helicopter configuration.

Actions Since AD 2020-22-01 Was Issued

    Since the FAA issued AD 2020-22-01, EASA issued EASA AD 2021-0222, 
dated October 6, 2021 (EASA AD 2021-0222), which supersedes EASA AD 
2019-0295. EASA advises a significant number of reports were received 
about corrosion being detected on the affected parts. EASA also advises 
Airbus Helicopters issued updated service information, which includes 
instructions for repetitive inspections. Accordingly, EASA AD 2021-0222 
retains the requirements of EASA AD 2019-0295 and adds repetitive 
inspections and updated service information. Additionally, Airbus 
Helicopters advised of a typo in the applicable service information in 
the reference to G.2 of one of the work cards. Accordingly, the FAA has 
identified this typo in the exceptions in the regulatory text of this 
proposed AD.

FAA's Determination

    These helicopters have been approved by EASA and are approved for 
operation in the United States. Pursuant to the FAA's bilateral 
agreement with the European Union, EASA has notified the FAA about the 
unsafe condition described in its AD. The FAA is proposing this AD 
after evaluating all known relevant information and determining that 
the unsafe condition described previously is likely to exist or develop 
on other products of the same type design.

Related Service Information Under 1 CFR Part 51

    The FAA reviewed Airbus Helicopters Alert Service Bulletin (ASB) 
No. AS332-53.02.05, Revision 2, and ASB No. AS332-53.02.07, Revision 1, 
both dated August 19, 2021, which specify procedures for inspecting the 
attachment fittings and attachment screws of the MGB suspension bars 
and their frame bores for discrepancies and corrective actions. This 
inspection includes inspecting the attachment fittings for corrosion 
and inspecting the attachment screws for corrosion and evidence of 
sealing compound. The corrective actions include replacing or

[[Page 7772]]

repairing corroded parts and replacing screws that have sealing 
compound on them. These documents are distinct since they apply to 
different helicopter models 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.

Other Related Service Information

    The FAA also reviewed Airbus Helicopters ASB No. AS332-53.02.05, 
Revision 0, dated April 18, 2019; Airbus Helicopters ASB No. AS332-
53.02.05, Revision 1, dated March 2, 2020; and Airbus Helicopters ASB 
No. AS332-53.02.07, Revision 0, dated October 21, 2019, which also 
specify procedures for inspecting the attachment fittings and 
attachment screws of the MGB suspension bars and their frame bores for 
discrepancies and corrective actions.

Proposed AD Requirements

    This proposed AD would retain all requirements of AD 2020-22-01. 
This proposed AD would add repetitive inspections and update the 
applicable service information. This proposed AD would require 
accomplishing the actions specified in the service information 
described previously.

Costs of Compliance

    The FAA estimates that this AD would affect 10 helicopters of U.S. 
Registry. Labor rates are estimated at $85 per work-hour. Based on 
these numbers, the FAA estimates that operators may incur the following 
costs in order to comply with this proposed AD.
    Inspecting each attachment screw and fitting of the rear MGB 
suspension bars; each attachment screw and fitting of the front MGB 
suspension bar; and the frame bores would take about 16 work-hours, for 
an estimated cost of $1,360 per helicopter and $13,600 for the U.S. 
fleet per inspection cycle.
    The FAA estimates the following costs to do any necessary on-
condition corrective actions that would be required based on the 
results of the inspection. The agency has no way of determining the 
number of helicopters that might need these on-condition replacements:
    If required, replacing an affected screw, nut, split pin, concave 
washer, convex washer, or peel shim would take a minimal amount of time 
with a minimal cost.
    If required, replacing an affected MGB attachment fitting would 
take about 8 work-hours and parts would cost about $7,000 for an 
estimated cost of $7,680 per replacement.
    If required, reporting any discrepancies to Airbus Helicopters 
would take about 1 work-hour for an estimated cost of $85 per 
helicopter.

Paperwork Reduction Act

    A federal agency may not conduct or sponsor, and a person is not 
required to respond to, nor shall a person be subject to a penalty for 
failure to comply with a collection of information subject to the 
requirements of the Paperwork Reduction Act unless that collection of 
information displays a currently valid OMB Control Number. The OMB 
Control Number for this information collection is 2120-0056. Public 
reporting for this collection of information is estimated to be 
approximately 1 hour per response, including the time for reviewing 
instructions, searching existing data sources, gathering and 
maintaining the data needed, and completing and reviewing the 
collection of information. All responses to this collection of 
information are mandatory. Send comments regarding this burden estimate 
or any other aspect of this collection of information, including 
suggestions for reducing this burden to: Information Collection 
Clearance Officer, Federal Aviation Administration, 10101 Hillwood 
Parkway, Fort Worth, TX 76177-1524.

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 has 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 that the 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 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:
0
a. Removing Airworthiness Directive AD 2020-22-01, Amendment 39-21297 
(85 FR 69126, November 2, 2020); and
0
b. Adding the following new airworthiness directive:

Airbus Helicopters: Docket No. FAA-2022-0096; Project Identifier 
MCAI-2021-01092-R.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive 
(AD) action by March 28, 2022.

(b) Affected ADs

    This AD replaces AD 2020-22-01, Amendment 39-21297 (85 FR 69126, 
November 2, 2020) (AD 2020-22-01).

(c) Applicability

    This AD applies to all Airbus Helicopters Model AS332C, AS332C1, 
AS332L, and AS332L1 helicopters, certificated in any category.

(d) Subject

    Joint Aircraft System Component (JASC) Code 5340, Fuselage main, 
attach fittings.

(e) Reason

    This AD was prompted by reports of corrosion on attachment 
screws and fittings fastening the main gearbox (MGB) suspension bars 
to the fuselage. The FAA is issuing this AD to address corrosion on

[[Page 7773]]

attachment fittings and attachment screws for the MGB suspension 
bars. The unsafe condition, if not addressed, could lead to 
structural failure of the MGB attachment screws, resulting in 
detachment of MGB suspension bars from the fuselage and subsequent 
loss of control of the helicopter.

(f) Compliance

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

(g) Definitions

    Affected parts are attachment screws and fitting(s) fastening 
the parts identified in paragraphs (g)(1) and (2) of this AD.
    (1) Rear MGB suspension bars, right and left sides, to the 
fuselage.
    (2) Front MGB suspension bar to the fuselage.

(h) Repetitive Inspections

    Except as specified in paragraphs (j)(1) through (10) of this 
AD: Within the applicable compliance times identified in paragraphs 
(h)(1) or (2) of this AD, inspect each affected part and its frame 
bores for discrepancies, in accordance with the Accomplishment 
Instructions, paragraphs 3.B.2. through 3.B.2.b.3 of Airbus 
Helicopters Alert Service Bulletin (ASB) No. AS332-53.02.05, 
Revision 2, dated August 19, 2021 (ASB AS332-53.02.05 Rev 2); or in 
accordance with the Accomplishment Instructions, paragraphs 3.B.2. 
through 3.B.2.d. of Airbus Helicopters ASB No. AS332-53.02.07, 
Revision 1, dated August 19, 2021 (ASB AS332-53.02.07 Rev 1), as 
applicable to your model helicopter. For the purposes of this 
inspection, a discrepancy may be indicated by corrosion on the MGB 
attachment fitting or by sealing compound on the attachment screws.
    (1) Perform the initial inspection within the applicable 
compliance times identified in the ``Deadlines'' column of Tables 1 
through 4, as applicable, of paragraph 1.E.2, ``Compliance in 
service,'' of ASB AS332-53.02.05 Rev 2, and thereafter, at intervals 
not to exceed the compliance time identified in the ``Periodicity'' 
column of Table 1 through 4, as applicable.
    (2) Perform the initial inspection within the applicable 
compliance times identified in the ``Deadlines'' column of Tables 1 
and 2, as applicable, of paragraph 1.E.2, ``Compliance in service,'' 
of ASB AS332-53.02.07 Rev 1, and thereafter, at intervals not to 
exceed the compliance time identified in the ``Periodicity'' column 
of Table 1 and 2, as applicable.

(i) Corrective Action

    Except as required by paragraphs (j)(7) through (10) of this AD: 
If, during any inspection required by paragraph (h) of this AD, 
there is any discrepancy, before further flight, perform the 
applicable corrective action (including replacing or repairing 
corroded parts and replacing screws that have sealing compound on 
them), in accordance with the Accomplishment Instructions, 
paragraphs 3.B.2. through 3.B.2.b.3 of ASB AS332-53.02.05 Rev 2 or 
in accordance with the Accomplishment Instructions, paragraphs 
3.B.2. through 3.B.2.d. of ASB AS332-53.02.07 Rev 1, as applicable.

(j) Exceptions to Service Information Specifications

    (1) Where Tables 1 and 3 of ASB AS332-53.02.05 Rev 2 use the 
phrase ``receipt of Revision 0 of this Alert Service Bulletin issued 
April 18, 2019,'' this AD requires using December 7, 2020 (the 
effective date of AD 2020-22-01).
    (2) Where Table 1 of ASB AS332-53.02.07 Rev 1 uses the phrase 
``receipt of Revision 0 of this Alert Service Bulletin,'' this AD 
requires using December 7, 2020 (the effective date of AD 2020-22-
01).
    (3) Where Tables 2 and 4 of ASB AS332-53.02.05 Rev 2 use the 
phrase ``receipt of Revision 2 of this Alert Service Bulletin,'' 
this AD requires using the effective date of this AD.
    (4) Where Table 2 of ASB AS332-53.02.07 Rev 1, uses the phrase 
``that follow receipt of Revision 1 of this Alert Service 
Bulletin,'' this AD requires using the effective date of this AD.
    (5) Where Tables 2 and 4 of ASB AS332-53.02.05 Rev 2, and Table 
2 of ASB AS332-53.02.07 Rev 1, specify certain configurations in the 
``Configuration'' column, this AD requires compliance for those 
configurations as of the effective date of this AD. Note 1 to 
paragraph (h)(5): An example for the exception specified in (h)(5) 
of this AD is where a service bulletin specifies, ``3700 flight 
hours or more since compliance with this Alert Service Bulletin,'' 
use ``3700 flight hours or more since compliance with this Alert 
Service Bulletin as of the effective date of this AD.''
    (6) Where Tables 1 and 3 of ASB AS332-53.02.05 Rev 2, and Table 
1 of ASB AS332-53.02.07 Rev 1, specify certain configurations in the 
``Configuration'' column, this AD requires compliance for those 
configurations as of December 7, 2020 (the effective date of AD 
2020-22-01).
    (7) Where the Accomplishment Instructions, paragraph 3.B.2.b.3) 
of ASB AS332-53.02.05 Rev 2, and the Accomplishment Instructions, 
paragraph 3.B.2.b.2) of ASB AS332-53.02.07 Rev 1 specify performing 
a check of the condition of the bores and frames, for this AD for 
ASB AS332-53.02.05 Rev 2 replace the text, ``Perform a check of the 
state of the frame bores as per paragraph G.2. of the Work Card 53-
10-00-402 (MET),'' with ``Perform a check of the state of the frame 
bores as per paragraph F.2.b.(2) of the Work Card 53-10-00-402 
(MET);'' and for ASB AS332-53.02.07 Rev 1 replace the text, ``Check 
the condition of the bores and the frames using the endoscope (yy) 
as per paragraph G.2. of Work Card 53-10-00-402 (MET),'' with 
``Check the condition of the bores and the frames using the 
endoscope (yy) as per paragraph F.2.b.(2) of Work Card 53-10-00-402 
(MET).''
    (8) Where ASB AS332-53.02.05 Rev 2 and ASB AS332-53.02.07 Rev 1 
specify discarding parts, you are not required to discard parts.
    (9) Where ASB AS332-53.02.05 Rev 2 and ASB AS332-53.02.07 Rev 1 
specify contacting Airbus Helicopters for repair instructions, this 
AD requires repair done in accordance with a method approved by the 
Manager, General Aviation and Rotorcraft Section, International 
Validation Branch, FAA; or EASA; or Airbus Helicopters' EASA Design 
Organization Approval (DOA). If approved by the DOA, the approval 
must include the DOA-authorized signature.
    (10) Where ASB AS332-53.02.05 Rev 2, and ASB AS332-53.02.07 Rev 
1, specify if sealing compound is present, or if no sealing compound 
is present but there is corrosion, take a photo, place the part in 
quarantine, and contact Airbus Helicopters for repair instructions, 
this AD requires repair done in accordance with a method approved by 
the Manager, General Aviation and Rotorcraft Section, International 
Validation Branch, FAA; or EASA; or Airbus Helicopters' EASA DOA. If 
approved by the DOA, the approval must include the DOA-authorized 
signature. This AD does not require taking a photo or placing the 
part in quarantine.

(k) Reporting

    If, during any inspection required by paragraph (h) of this AD, 
there is any discrepancy, report the inspection results to Airbus 
Helicopters at the applicable time specified in paragraphs (k)(1) or 
(2) of this AD. The report should include the information specified 
in Appendix 4.A. of Airbus Helicopters ASB AS332-53.02.05 Rev 2; or 
ASB AS332-53.02.07 Rev 1, as applicable.
    (1) If the inspection was done on or after the effective date of 
this AD: Submit the report within 30 days after the inspection.
    (2) If the inspection was done before the effective date of this 
AD: Submit the report within 30 days after the effective date of 
this AD.

(l) Credit for Previous Actions

    (1) For helicopters identified in ASB AS332-53.02.05 Rev 2: This 
paragraph provides credit for initial inspections required by 
paragraph (h) of this AD, if those actions were performed before the 
effective date of this AD using Airbus Helicopters ASB AS332-
53.02.05, Revision 1, dated March 2, 2020, or Airbus Helicopters ASB 
AS332-53.02.05, Revision 0, dated April 18, 2019.
    (2) For helicopters identified in ASB AS332-53.02.07 Rev 1: This 
paragraph provides credit for initial inspections required by 
paragraph (h) of this AD, if those actions were performed before the 
effective date of this AD using Airbus Helicopters ASB AS332-53-
02.07 Revision 0, dated October 21, 2019.

(m) Special Flight Permit

    Special flight permits may be issued in accordance with 14 CFR 
21.197 and 21.199, provided no passengers are onboard.

(n) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, 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 local Flight 
Standards District Office, as appropriate. If sending information 
directly to the manager of the International Validation

[[Page 7774]]

Branch, send it to the attention of the person identified in 
paragraph (o)(1) of this AD. Information may be emailed to: [email protected].
    (2) 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.

(o) Related Information

    (1) For more information about this AD, contact Andrea Jimenez, 
Aerospace Engineer, COS Program Management Section, Operational 
Safety Branch, Compliance & Airworthiness Division, FAA, 1600 
Stewart Ave., Suite 410, Westbury, NY 11590; telephone (516) 228-
7330; email [email protected].
    (2) For service information identified in this AD, contact 
Airbus Helicopters, 2701 N. Forum Drive, Grand Prairie, TX, 75052, 
telephone: (972) 641-0000; or (800) 232-0323; fax (972) 641-3775; or 
at https://www.airbus.com/helicopters/services/technical-support.html. You may view this referenced service information at 
the FAA, Office of the Regional Counsel, Southwest Region, 10101 
Hillwood Pkwy., Room 6N-321, Fort Worth, TX 76177. For information 
on the availability of this material at the FAA, call (817) 222-
5110.
    (3) The subject of this AD is addressed in European Union 
Aviation Safety Agency (EASA) AD 2021-0222, dated October 6, 2021, 
for more information. You may view the EASA AD on the internet at 
https://www.regulations.gov in Docket No. FAA-2022-0096.

    Issued on February 4, 2022.
Gaetano A. Sciortino,
Deputy Director for Strategic Initiatives, Compliance & Airworthiness 
Division, Aircraft Certification Service.
[FR Doc. 2022-02768 Filed 2-9-22; 8:45 am]
BILLING CODE 4910-13-P


