[Federal Register Volume 87, Number 76 (Wednesday, April 20, 2022)]
[Proposed Rules]
[Pages 23477-23480]
[FR Doc No: 2022-08304]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-0465; Project Identifier AD-2022-00330-R]
RIN 2120-AA64

Airworthiness Directives; Leonardo S.p.a. 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)
2021-20-10, which applies to certain Leonardo S.p.a. Model AB139 and
AW139 helicopters. AD 2021-20-10 requires removing from service a
certain part-numbered main gearbox (MGB) spherical bearing lock nut
(lock nut) that is installed on certain part-numbered MGBs and
replacing it with a newly designed MGB lock nut. AD 2021-20-10 also
prohibits installing any MGB with the affected MGB lock nut and
prohibits installing any affected MGB lock nut on any helicopter. Since
the FAA issued AD 2021-20-10, it was discovered that a part number (P/
N) was incorrectly listed and that the applicability needed to be
clarified. This proposed AD would retain the requirements of AD 2021-
20-10 and would clarify the applicability. 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 June 6,
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:<PHONE_NUMBER>.
     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 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 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.

Examining the AD Docket

    You may examine the AD docket at https://www.regulations.gov by
searching for and locating Docket No. FAA-2022-0465; 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: Kristi Bradley, Program Manager, COS
Program Management Section, Operational Safety Branch, Compliance &
Airworthiness Division, FAA, 10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone<PHONE_NUMBER>; email [email protected].

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-2022-0465; Project Identifier
AD-2022-00330-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
Kristi Bradley, Program Manager, COS Program Management Section,
Operational Safety Branch, Compliance & Airworthiness Division, FAA,
10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone<PHONE_NUMBER>;
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 2021-20-10, Amendment 39-21748 (86 FR 57574,
October 18, 2021) (AD 2021-20-10), for Leonardo S.p.a. Model AB139 and
AW139 helicopters, without MGB lock nut P/N 3G6320A09152 installed and
with MGB P/N 3G6320A00131, 3G6320A00132, 3G6320A00133, 3G6320A00134,
3G6320A00135, 3G6320A00136, 3G6320A22031, 4G6320A00132, or 4G6320A00133
installed; or MGB P/N 3G320A00133 with serial number (S/N) M23, or MGB
P/N 3G6320A00134, with S/N M6, N76, N92, P124, P129, P131, P162, P184,
Q230, Q243, Q249, R272, V21, V39, V96, V163, V211, V241, V272, V281,
V384, V386, or V622 installed; or MGB P/N 3G6320A00136 with S/N AW1,
AW2, AW3, AW5, or AW10 installed.
    AD 2021-20-10 requires, within 100 hours time in service (TIS), or
during the next scheduled MGB overhaul, whichever occurs first after
the effective date of the AD, removing a certain part-numbered MGB lock
nut from service and replacing it with a different part-numbered MGB
lock nut. AD 2021-20-10 also prohibits installing an MGB having an
affected MGB lock nut on any helicopter and also prohibits installing
an affected MGB lock nut on any helicopter as of the effective date of
the AD.
    AD 2021-20-10 was prompted by a series of EASA ADs beginning with
EASA AD 2019-0036, dated February 15, 2019 (EASA AD 2019-0036), issued
by EASA, which is the Technical Agent for the Member States of the
European Union, to correct an unsafe condition for all serial-numbered
Leonardo S.p.a. Helicopters (formerly Finmeccanica S.p.A,
AgustaWestland S.p.A., Agusta S.p.A.; and AgustaWestland Philadelphia
Corporation, formerly Agusta Aerospace Corporation) Model AB139 and
AW139 helicopters. EASA advised that an occurrence was reported of a
cracked MGB lock nut P/N 3G6310A09151, which is used to keep the
planetary gears in position. EASA AD 2019-0036 required replacing each
MGB lock nut with an airworthy MGB lock nut. EASA advised this
condition, if not detected and corrected, could lead to failure of the
MGB planetary gears, resulting in loss of control of the helicopter.
    After EASA issued EASA AD 2019-0036, an additional occurrence was
reported of a cracked MGB lock nut P/N 3G6320A09151. Accordingly, EASA
superseded EASA AD 2019-0036 with EASA AD 2019-0174, dated July 18,
2019 (EASA AD 2019-0174), which retained the requirements of EASA AD
2019-0036 but reduced the compliance times. After EASA issued EASA AD
2019-0174, Leonardo Helicopters issued Alert Service Bulletin No. 139-
609, dated December 18, 2019, to provide instructions for replacing the
affected MGB lock nut with MGB lock nut P/N 3G6320A09152, which has a
redesigned flange reducing the stress at the bearing nut locations
where cracks were detected.
    Accordingly, EASA then issued EASA AD 2020-0011, dated January 29,
2020, and corrected January 30, 2020 (EASA AD 2020-0011), which
superseded EASA AD 2019-0174, and partially retained the requirements
of EASA AD 2019-0174. EASA AD 2020-0011 revised the compliance times in
EASA AD 2019-0174, required replacing each affected MGB lock nut with a
newly designed MGB lock nut, and prohibited installing an affected MGB
on any helicopter. After EASA issued EASA AD 2020-0011, EASA identified
certain MGB part numbers that were inadvertently categorized
incorrectly and therefore listed in the wrong group of helicopters.
Accordingly, EASA issued EASA AD 2020-0011R1, dated November 20, 2020
(EASA AD 2020-011R1), thereby revising EASA AD 2020-0011. EASA AD 2020-
0011R1 retained the requirements of EASA AD 2020-0011 and corrected
Appendix 1 of EASA AD 2020-0011.
    After EASA issued EASA AD 2020-0011R1, Leonardo Helicopters issued
Alert Service Bulletin No. 139-609, Revision A, dated April 13, 2021,
which identifies an additional part-numbered MGB, which is also
affected by the unsafe condition. Accordingly, EASA superseded EASA AD
2020-0011R1 with EASA AD 2021-0121, dated May 4, 2021 (EASA AD 2021-
0121). EASA AD 2021-0121 adds an additional part-numbered MGB with a
certain S/N to the list of affected parts. EASA AD 2021-0121 retains
the requirements of EASA AD 2020-0011R1, and corrects Table 1 and
Appendix 1 of EASA AD 2020-0011R1.
    Accordingly, EASA AD 2021-0121 requires replacing each affected MGB
lock nut with a newly designed MGB lock nut, and prohibits installing
an affected MGB on any helicopter.

Actions Since AD 2021-20-10 Was Issued

    Since the FAA issued AD 2021-20-10, it was discovered that MGB P/N
3G6320A00133 is incorrectly listed as MGB P/N 3G320A00133 in both the
preamble and applicability paragraph of the AD. Also, the FAA
determined that

all MGBs, regardless of S/N, are affected by the unsafe condition.
Therefore, this proposed AD would remove any reference to S/Ns in the
applicability. In addition, this proposed AD includes the total U.S.
fleet costs, which were inadvertently excluded in AD 2021-20-10.

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 helicopters of the same type designs.

Related Service Information Under 1 CFR Part 51

    This proposed AD would require Leonardo Helicopters Alert Service
Bulletin No. 139-609, Revision A, dated April 13, 2021, which the
Director of the Federal Register approved for incorporation by
reference as of November 22, 2021 (86 FR 57574, October 18, 2021).
    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 Leonardo Helicopters Alert Service Bulletin
No. 139-567, Revision B, dated October 18, 2019, which provides
additional information for replacing the MGB lock nut.

Proposed AD Requirements in This NPRM

    This proposed AD would retain all of the requirements of AD 2021-
20-10.

Differences Between This Proposed AD and EASA AD 2021-0121

    EASA AD 2021-0121 requires a compliance time based on number of
landings, whereas this proposed AD would require a compliance time
based on hours TIS. The service information referenced in EASA AD 2021-
0121 requires submitting certain information and parts to Leonardo,
whereas this proposed AD would not. EASA AD 2021-0121 applies to all
serial-numbered Model AB139 and AW139 helicopters, whereas this
proposed AD would apply to all Model AB139 and AW139 helicopters,
regardless of S/N, with a certain part-numbered MGB lock nut and MGB
installed.

Costs of Compliance

    The FAA estimates that this AD, if adopted as proposed, would
affect 130 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 proposed AD.
    Replacing each affected MGB lock nut with a newly designed MGB lock
nut would take about 190 work-hours (during next MGB overhaul) and
parts would cost about $7,600 for an estimated cost of $23,750 per
helicopter and $3,087,500 for the U.S. fleet.

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, 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 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 2021-20-10, Amendment 39-21748 (86
FR 57574, October 18, 2021); and
0
b. Adding the following new airworthiness directive:

Leonardo S.p.a.: Docket No. FAA-2022-0465; Project Identifier AD-
2022-00330-R.

(a) Comments Due Date

    The FAA must receive comments on this airworthiness directive
(AD) action by June 6, 2022.

(b) Affected ADs

    This AD replaces AD 2021-20-10, Amendment 39-21748 (86 FR 57574,
October 18, 2021) (AD 2021-20-10).

(c) Applicability

    This AD applies to Leonardo S.p.a. Model AB139 and AW139
helicopters, certificated in any category, with a main rotor gearbox
(MGB) part number (P/N) 3G6320A00131, 3G6320A00132, 3G6320A00133,
3G6320A00134, 3G6320A00135, 3G6320A00136, 3G6320A22031,
4G6320A00132, or 4G6320A00133, and MGB spherical bearing lock nut
(lock nut) P/N 3G6320A09151 installed.

(d) Subject

    Joint Aircraft Service Component (JASC) Code: 6320, Main Rotor
Gearbox.

(e) Unsafe Condition

    This AD was prompted by a cracked MGB lock nut. The FAA is
issuing this AD to replace an affected MGB lock nut with a new MGB
lock nut. The unsafe condition, if not addressed, could result in
failure of the MGB planetary gears, resulting in loss of control of
the helicopter.

(f) Compliance

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

(g) Required Actions

    (1) Within 100 hours time-in-service, or during the next
scheduled MGB overhaul, whichever occurs first after November 22,
2021 (the effective date of AD 2021-20-10),

remove each MGB lock nut P/N 3G6320A09151 from service and replace
with MGB lock nut P/N 3G6320A09152 in accordance with Annex A, steps
1 through 17, of Leonardo Helicopters Alert Service Bulletin No.
139-609, Revision A, dated April 13, 2021, except you are not
required to send parts to Leonardo Helicopters.

    Note to paragraph (g)(1):  Leonardo Helicopters service
information refers to an MGB lock nut as a ring nut.

    (2) As of November 22, 2021 (the effective date of AD 2021-20-
10), do not install any MGB having MGB lock nut P/N 3G630A09151 on
any helicopter, and do not install any MGB lock nut P/N 3G630A09151
on any helicopter.

(h) Special Flight Permits

    Special flight permits are prohibited.

(i) 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 (j)(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.

(j) Related Information

    (1) For more information about this AD, contact Kristi Bradley,
Program Manager, COS Program Management Section, Operational Safety
Branch, Compliance & Airworthiness Division, FAA, 10101 Hillwood
Pkwy., Fort Worth, TX 76177; telephone<PHONE_NUMBER>; email
[email protected].
    (2) For service information identified in this AD, 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
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<PHONE_NUMBER>.
    (3) The subject of this AD is addressed in European Union
Aviation Safety Agency (EASA) AD 2021-0121, dated May 4, 2021. You
may view the EASA AD at https://www.regulations.gov in Docket No.
FAA-2022-0465.

    Issued on April 13, 2022.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2022-08304 Filed 4-19-22; 8:45 am]
BILLING CODE 4910-13-P


September 15, 2004 MEMORANDUM From: Michael Galbraith, USEPA/ OSW To: Hazardous Waste Combustor MACT Rule Docket, OAR 2004 0022 Subject: September 9, 2004 Meeting with Environmental Technology Council On September 9, 2004, the Environmental Technology Council ( ETC), represented by Dave Case and Bill Ziegler, met with USEPA staff ( Michael Galbraith, Bob Holloway, Frank Behan, Shiva Garg, Steve Silverman and Nelson Andrews) to discuss the hazardous waste combustor MACT proposal.

The discussion focused on ETC and Sierra Clubs' comments submitted on the proposal, and included topics such as the legal justification of the proposed floor methodologies, justification for issuing particulate matter standards as surrogate controls for metal HAPs, and EPA's proposed approach to not identify feed control of raw material HAPs ( and nonhazardous waste fuel HAPs) as a floor control technology.

ETC indicated that they would be submitting supplemental comments on the Hazardous Waste Combustor MACT proposal in the near future.


[Federal Register Volume 87, Number 235 (Thursday, December 8, 2022)]
[Notices]
[Pages 75248-75249]
[FR Doc No: 2022-26677]

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DEPARTMENT OF ENERGY

Federal Energy Regulatory Commission

Combined Notice of Filings #1

    Take notice that the Commission received the following electric
rate filings:

    Docket Numbers: ER23-542-000.
    Applicants: San Diego Gas & Electric Company.
    Description: Informational Filing [Cycle 5] of Fifth Transmission
Owner Rate Formula rate mechanism of San Diego Gas & Electric Company.
    Filed Date: 12/1/22.
    Accession Number: 20221201-5234.
     Comment Date: 5 p.m. ET 12/20/22.

    Docket Numbers: ER23-543-000.

     Applicants: EDF Renewables, Inc.
    Description: Petition for Limited Waiver and expedited Commission
action of EDF Renewables, Inc.
    Filed Date: 12/1/22.
    Accession Number: 20221201-5245.
     Comment Date: 12 p.m. (Noon) ET 12/5/22.

    Docket Numbers: ER23-544-000.
    Applicants: PJM Interconnection, L.L.C.
    Description: Sec.  205(d) Rate Filing: Original ISA, Service
Agreement No. 6708; Queue No. AF1-075 to be effective 11/2/2022.
    Filed Date: 12/2/22.
     Accession Number: 20221202-5008.
     Comment Date: 5 p.m. ET 12/23/22.

    Take notice that the Commission received the following foreign
utility company status filings:

    Docket Numbers: FC23-1-000.
    Applicants: I Squared Capital.
    Description: I Squared Capital submits Notice of Self-Certification
of Foreign Utility Company Status.
    Filed Date: 11/29/22.
    Accession Number: 20221129-5223.
     Comment Date: 5 p.m. ET 12/20/22.

    The filings are accessible in the Commission's eLibrary system
(https://elibrary.ferc.gov/idmws/search/fercgensearch.asp) by querying
the docket number.
    Any person desiring to intervene or protest in any of the above
proceedings must file in accordance with Rules 211 and 214 of the
Commission's Regulations (18 CFR 385.211 and 385.214) on or before 5:00
p.m. Eastern time on the specified comment date. Protests may be
considered, but intervention is necessary to become a party to the
proceeding.
    eFiling is encouraged. More detailed information relating to filing
requirements, interventions, protests, service, and qualifying
facilities filings can be found at: http://www.ferc.gov/docs-filing/efiling/filing-req.pdf. For other information, call<PHONE_NUMBER>
(toll free). For TTY, call<PHONE_NUMBER>.

    Dated: December 2, 2022.
Kimberly D. Bose,
Secretary.
[FR Doc. 2022-26677 Filed 12-7-22; 8:45 am]
BILLING CODE 6717-01-P