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2021-25-01 LEONARDO S.P.A.: Amendment 39-21844; Docket No. FAA-2021-0834; Project Identifier MCAI-2021-00298-R.
(a) EFFECTIVE DATE

    This airworthiness directive (AD) is effective January 24, 2022.

(b) AFFECTED ADS

    None.

(c) APPLICABILITY

    This AD applies to Leonardo S.p.a. Model A109S and AW109SP helicopters
    certificated in any category, as identified in European Union Aviation
    Safety Agency (EASA) AD 2021-0065,  dated March 8, 2021 (EASA AD 2021-
    0065).

(d) SUBJECT

    Joint Aircraft Service Component (JASC) Code:  2497,  Electrical Power
    System Wiring.

(e) UNSAFE CONDITION

    This AD was prompted  by the discovery  that rubber protection of cer-
    tain electrical wiring had not been installed in the baggage  avionics
    bay during production. The FAA  is issuing this AD to  prevent chafing
    of electrical wiring.  The unsafe condition,  if not addressed,  could
    result  in fire  ignition and  smoke  in  the baggage  compartment and
    subsequent loss of control of the helicopter.

(f) COMPLIANCE

    Comply with this AD within the compliance times specified,  unless al-
    ready done.

(g) REQUIREMENTS

    Except as specified in paragraph (h)  of this AD:  Comply with all re-
    quired actions and compliance times specified in,  and  in  accordance
    with, EASA AD 2021-0065.

(h) EXCEPTIONS TO EASA AD 2021-0065

(1) Where EASA AD 2021-0065 requires compliance  in terms of flight hours,
    this AD requires using hours time-in-service.

(2) Where EASA AD 2021-0065 refers to its effective date, this AD requires
    using the effective date of this AD.

(3) This AD does not mandate compliance with the "Remarks" section of EASA
    AD 2021-0065.

(i) NO REPORTING REQUIREMENT

    Although the service information referenced in EASA AD 2021-0065 spec-
    ifies to submit certain information to the manufacturer,  this AD does
    not include that requirement.

(j) SPECIAL FLIGHT PERMIT

    Special flight permits are prohibited.

(k) 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  Branch, send  it  to the  attention  of the
    person identified  in paragraph  (l) of  this AD.  Information may  be
    emailed to: 9-AVS-AIR-730-AMOC@faa.gov.

(2) Before using any approved AMOC,  notify your appropriate principal in-
    spector, or lacking  a principal inspector,  the manager of  the local
    flight standards district office/certificate holding district office.

(l) RELATED INFORMATION

    For more information about this AD, contact Hal Jensen, Aerospace Eng-
    ineer, Operational Safety Branch, Compliance & Airworthiness Division,
    FAA,  950 L'Enfant Plaza N SW,  Washington, DC 20024;  telephone (202)
    267-9167; email hal.jensen@faa.gov.

(m) MATERIAL INCORPORATED BY REFERENCE

(1) The Director of the Federal Register  approved  the  incorporation  by
    reference 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 2021-0065, dated March
    8, 2021.

(ii) [Reserved]

(3) For EASA AD 2021-0065,  contact  EASA,  Konrad-Adenauer-Ufer 3,  50668
    Cologne, Germany; telephone +49 221 8999 000; email ADs@easa.europa.eu
    internet  www.easa.europa.eu.  You may find  the EASA material  on the
    EASA website at https://ad.easa.europa.eu.

(4) You may view  this  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. This material may  be found
    in the AD docket  at https://www.regulations.gov by searching  for and
    locating Docket No. FAA-2021-0834.

(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 fr.inspection@nara
    .gov,  or  go  to:  https://www.archives.gov/federal-register/cfr/ibr-
    locations.html.

Issued on November 23, 2021. Lance T Gant, Director, Compliance & Airworth
-iness Division, Aircraft Certification Service.

FOR FURTHER INFORMATION CONTACT:  Hal Jensen,  Aerospace Engineer,  Opera-
tional  Safety  Branch,  Compliance &  Airworthiness  Division,  FAA,  950
L'Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267-9167; email
hal.jensen@faa.gov.
PREAMBLE 

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2021-0834; Project Identifier MCAI-2021-00298-R;
Amendment 39-21844; AD 2021-25-01]
RIN 2120-AA64

Airworthiness Directives; Leonardo S.p.a. Helicopters

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Leonardo S.p.a. Model A109S and AW109SP helicopters. This AD
was prompted by the discovery that rubber protection of certain
electrical wiring had not been installed in the baggage avionics bay
during production. This AD requires installing protective rubber
borders on the edge of the baggage avionics bay frames, 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 January 24, 2022.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of January 24,
2022.

ADDRESSES: For EASA material incorporated by reference (IBR) in this
AD, contact EASA, Konrad-Adenauer-Ufer 3, 50668 Cologne, Germany;
telephone +49 221 8999 000; email ADs@easa.europa.eu; internet
www.easa.europa.eu. You may find the EASA material on the EASA website
at https://ad.easa.europa.eu. For Leonardo Helicopters service
information identified in this final rule, contact Leonardo S.p.A.
Helicopters, Emanuele Bufano, Head of Airworthiness, Viale G.Agusta
520, 21017 C.Costa di Samarate (Va) Italy; telephone +39-0331-225074;
fax +39-0331-229046; or at https://customerportal.leonardocompany.com/
en-US/. You may view this material 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. Service information that is
incorporated by reference is also available in the AD docket at https://
www.regulations.gov by searching for and locating Docket No. FAA-2021-0834.

Examining the AD Docket

You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2021-0834; 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
EASA AD, 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: Hal Jensen, Aerospace Engineer,
Operational Safety Branch, Compliance & Airworthiness Division, FAA,
950 L'Enfant Plaza N SW, Washington, DC 20024; telephone (202) 267-
9167; email hal.jensen@faa.gov.

SUPPLEMENTARY INFORMATION:

Background

EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA AD 2021-0065, dated March 8, 2021 (EASA
AD 2021-0065), to correct an unsafe condition for certain serial-
numbered Leonardo S.p.A. Helicopters, formerly Finmeccanica S.p.A.,
AgustaWestland S.p.A., Agusta S.p.A., Model A109S and AW109SP
helicopters.
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to Leonardo S.p.a. Model
A109S and AW109SP helicopters as identified in EASA AD 2021-0065. The
NPRM published in the Federal Register on September 30, 2021 (86 FR
54124). The NPRM was prompted by the discovery that rubber protection
of certain electrical wiring had not been installed in the baggage
avionics bay during production. The NPRM proposed to require installing
protective rubber borders on the edge of the baggage avionics bay
frames, as specified in EASA AD 2021-0065.
The FAA is issuing this AD to prevent chafing of electrical wiring,
which if not addressed, could result in fire ignition and smoke in the
baggage compartment and subsequent loss of control of the helicopter.
See EASA AD 2021-0065 for additional background information.

Discussion of Final Airworthiness Directive

Comments

The FAA received no comments on the NPRM or on the determination of
the costs.

Conclusion

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 reviewed the relevant
data and determined that air safety requires adopting this AD as
proposed. Accordingly, the FAA is issuing this AD to address the unsafe
condition on these helicopters.

Related Service Information Under 1 CFR Part 51


EASA AD 2021-0065 requires installing rubber protections on the
electrical wiring in the baggage/avionics compartment.
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.

Other Related Service Information

The FAA reviewed Leonardo Helicopters Alert Service Bulletin (ASB)
No. 109S-100, dated February 2, 2021, for Model A109S helicopters, and
Leonardo Helicopters ASB No. 109SP-142, also dated February 2, 2021,
for Model AW109SP helicopters. This service information specifies
procedures for installing protective rubber borders on the edge of the
baggage avionics bay frames.

Costs of Compliance


The FAA estimates that this AD affects 3 helicopters of U.S.
Registry. Labor rates are estimated at $85 per work-hour. Based on
these numbers, the FAA estimates the following costs to comply with
this AD.
Installing protective rubber borders on the edge of the baggage
avionics bay frames will take about 2 work-hours and parts will cost
about $24 for an estimated cost of $194 per helicopter and $582 for the
U.S. fleet.
The FAA has included all known costs in its cost estimate.
According to the manufacturer, however, some of the costs of this AD
may be covered under warranty, thereby reducing the cost impact on
affected operators.

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 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.

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.

Sec. 39.13 [Amended]

2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive: