[Federal Register Volume 84, Number 48 (Tuesday, March 12, 2019)]
[Notices]
[Page 8943]
[FR Doc No: 2019-04446]

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DEPARTMENT OF TRANSPORTATION

Federal Railroad Administration

[Docket Number FRA-2019-0022]

Petition for Waiver of Compliance

    Under part 211 of Title 49 Code of Federal Regulations (CFR), this
document provides the public notice that on February 25, 2019, the
North Shore Railroad Company (NSHR) and its affiliates: Juniata Valley
Railroad (JVRR), Lycoming Valley Railroad (LVRR), Nittany & Bald Eagle
Railroad (UCIR), Shamokin Valley Railroad (SVRR), and Union County
Industrial Railroad (UCIR), petitioned the Federal Railroad
Administration (FRA) for a waiver of compliance from certain provisions
of the Federal railroad safety regulations contained at 49 CFR part
240, Qualification and Certification of Locomotive Engineers, and part
242, Qualification and Certification of Conductors. FRA assigned the
petition Docket Number FRA-2019-0022.
    The relief is requested as part of NSHR's proposed implementation
of and participation in FRA's Confidential Close Call Reporting System
(C \3\RS) Program. NSHR seeks to shield reporting employees and the
railroad from mandatory punitive sanctions that would otherwise arise
as provided in 49 CFR 240.117(e)(1)-(4); 240.305(a)(l)-(4) and (a)(6);
240.307; 242.403(b), (c), (e)(l)-(4), (e)(6)-(11), and (f)(l)-(2). The
C \3\RS Program encourages certified operating crew members to report
close calls and protect the employees and the railroad from discipline
or sanctions arising from the incidents reported per the C \3\RS
Implementing Memorandum of Understanding.
    A copy of the petition, as well as any written communications
concerning the petition, is available for review online at
www.regulations.gov and in person at the U.S. Department of
Transportation's (DOT) Docket Operations Facility, 1200 New Jersey
Avenue SE, W12-140, Washington, DC 20590. The Docket Operations
Facility is open from 9 a.m. to 5 p.m., Monday through Friday, except
Federal Holidays.
    Interested parties are invited to participate in these proceedings
by submitting written views, data, or comments. FRA does not anticipate
scheduling a public hearing in connection with these proceedings since
the facts do not appear to warrant a hearing. If any interested parties
desire an opportunity for oral comment and a public hearing, they
should notify FRA, in writing, before the end of the comment period and
specify the basis for their request.
    All communications concerning these proceedings should identify the
appropriate docket number and may be submitted by any of the following
methods:
     Website: http://www.regulations.gov. Follow the online
instructions for submitting comments.
     Fax:<PHONE_NUMBER>.
     Mail: Docket Operations Facility, U.S. Department of
Transportation, 1200 New Jersey Avenue SE, W12-140, Washington, DC
20590.
     Hand Delivery: 1200 New Jersey Avenue SE, Room W12-140,
Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday,
except Federal Holidays.
    Communications received by April 26, 2019 will be considered by FRA
before final action is taken. Comments received after that date will be
considered if practicable.
    Anyone can search the electronic form of any written communications
and comments received into any of our dockets by the name of the
individual submitting the comment (or signing the document, if
submitted on behalf of an association, business, labor union, etc.).
Under 5 U.S.C. 553(c), DOT solicits comments from the public to better
inform its processes. DOT posts these comments, without edit, including
any personal information the commenter provides, to
www.regulations.gov, as described in the system of records notice (DOT/
ALL-14 FDMS), which can be reviewed at https://www.transportation.gov/privacy. See also https://www.regulations.gov/privacyNotice for the
privacy notice of regulations.gov.

    Issued in Washington, DC.
Robert C. Lauby,
Associate Administrator for Railroad Safety, Chief Safety Officer.
[FR Doc. 2019-04446 Filed 3-11-19; 8:45 am]
BILLING CODE 4910-06-P


[Federal Register Volume 76, Number 2 (Tuesday, January 4, 2011)]
[Notices]
[Pages 409-410]
[FR Doc No: 2010-33223]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

Philadelphia International Airport, Capacity Enhancement Program,
Environmental Impact Statement, Record of Decision

AGENCY: Federal Aviation Administration (FAA) DOT.

ACTION: Notice of availability of record of decision (ROD).

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SUMMARY: The FAA has issued a ROD for the Philadelphia International
Airport (PHL), Capacity Enhancement Program (CEP), Environmental Impact
Statement (EIS). The City of Philadelphia, the airport sponsor, owns
and operates PHL and had requested FAA consider ways to accommodate
existing and forecasted aviation demands. The purpose of the CEP is to
enhance airport capacity in order to accommodate current and future
aviation demand in the Philadelphia Metropolitan Area during all
weather conditions. This ROD sets forth FAA's final determination and
environmental approvals for the federal actions necessary to implement
the CEP at the airport.

DATES: Effective upon publication in the Federal Register.

FOR FURTHER INFORMATION CONTACT: Susan L. McDonald, Environmental
Protection Specialist, Federal Aviation Administration, Harrisburg
Airports District Office, 3905 Hartzdale Drive, Suite 508, Harrisburg,
PA 17011.

SUPPLEMENTARY INFORMATION: In accordance with the National
Environmental Policy Act, the FAA has completed a Record of Decision
for the Environmental Impact Statement for the Philadelphia
International Airport Capacity Enhancement Program. The ROD sets forth
FAA's final determination and environmental approvals for the federal
actions necessary to implement the CEP at PHL. The ROD also identifies
Alternative A (the Project) as FAA's selected alternative for
implementation. The purpose of the CEP is to enhance airport capacity
in order to accommodate current and future aviation demand in the
Philadelphia Metropolitan Area during all weather conditions. The
Environmental Protection Agency (EPA) published a notice of
availability of the Final EIS in the Federal Register on August 27,
2010 (75 FR 52736). The Final EIS was prepared in compliance with the
National Environmental Policy Act of 1969 (NEPA), [42 U.S. C. 4321, et
seq.], the implementing regulations of the Council on Environmental
Quality (CEQ) [40 CFR parts 1500-1508], and FAA directives [Order
1050.1E and Order 505.4B]. The Final EIS presented three alternatives;
the No Action and two on-airport construction alternatives
(Alternatives A and B), and identified Alternative A the preferred
alternative. The FAA received comments on the Final EIS and these
comments, along with FAA's responses, are included in Attachment A of
the ROD.
    The Project will have five runways connected by a redesigned and
more efficient taxiway system than the No-Action Alternative. Runway
17-35 will remain as a 6,500-foot crosswind runway. Runway 8-26 will be
extended 2,000 feet to the east, for a total length of 7,000 feet. This
runway will continue to be unidirectional, serving westbound arrivals
and eastbound departures. The Runway 8-26 eastern arrival threshold
will be raised by approximately 55 feet in order to clear obstructions.
Runway 8-26 will have an Engineered Materials Arresting System (EMAS)
constructed at the east end of the runway. Runway 9L-27R will remain at
its current length (9,500 feet) and location. It will support westbound
departures in west flow, and eastbound arrivals in east flow. Runway
9R-27L will be extended to the east by 1,500 feet, to a total length of
12,000 feet. This runway will be renamed Runway 9C-27C. It will
function primarily as an arrival runway during west flow operations and
a departure runway during east flow. A new runway, Runway 9R-27L, 1,600
feet south of Runway 9C-27C will be constructed. This runway will be
9,103 feet long by 150 feet wide and will serve primarily as a
departure runway in west flow and an arrival runway in east flow.
Runway 9R-27L will have EMAS installed on its west end to reduce
impacts to the Delaware River. Constructing this runway will affect the
Delaware River. The approach lighting systems for proposed Runways 9R
and 9L will be upgraded to meet CAT II/III approach requirements. The
new approach light system for Runway 9R will be in the Delaware River,
extending 1,700 feet from the limit of fill, and will be a pile-
supported structure. The existing approach lighting systems for Runways
26 and 27C will be relocated based on the proposed threshold locations
for each runway. All existing navigational aids will be relocated as
necessary or new aids installed as required to meet the approach
criteria for the particular runway end. The Airport Surveillance Radar
(ASR-9) and the Precision Runway Monitor (PRM) south of Runway 9R-27L
will be relocated as necessary.
    The Project will upgrade and reconfigure the existing terminal
complex in its existing location. It will add a new commuter terminal
east of Runway 17-35. The total terminal complex will consist of eight
concourses with 145 to 150 gates and approximately 3.6 million square
feet. The existing terminal circulation, recirculation, and access will
remain as it is now with minor shifts in horizontal and vertical
alignments. An automated people mover (APM) will be constructed to
transport passengers between terminals and parking facilities. The
existing SEPTA rail line will continue to provide access to the
terminals from outside the Airport and will interface directly with the
APM system. The Project will enlarge the existing parking garages and
construct a new centralized ground transportation center. The Project
will also relocate or expand many of the other Airport facilities,
including cargo, general aviation (corporate), maintenance, fuel,
training facilities, and deicing facilities. The FAA's Air Traffic
Control Tower (ATCT) will also be relocated. Service roadways and
facilities will be reconstructed as needed.
    In order to accommodate the Airport reconfiguration, several off-
airport facilities and properties must be acquired and, in some cases,
relocated. The UPS facility south of the Airport will be relocated to a
new site in Tinicum. Hog Island Road will be closed and the freight
railroad serving the USACE Fort Mifflin Dredge Disposal Facility will
be relocated. Part of the Dredge Disposal Facility will be relocated
north. The Sunoco Hog Island Wharf will be closed and its functions
replaced by extending the existing Sunoco Fort Mifflin Pier to the
west.
    The Project will accommodate all forecasted operations with
annualized

average delays of 5.2 minutes in 2025 and 8.4 minutes in 2030. The
Project is estimated to cost $5.2 billion and take approximately 13
years to complete. With mitigation, significant environmental impacts
can be avoided or minimized.
    The FAA is granting approval to amend the airport layout plan (ALP)
with the conditions noted in Section 11 of the ROD, Conditions of
Project Approval, for the incorporation of all the physical elements
associated with selected alternative in the ROD, Alternative A, as
summarized in Section 2 of the ROD and approval to proceed with
processing an application for federal funding of those development
items qualifying for financial aid under the Airports Improvement
Program, [49 U.S.C. 47106] as well as applications to impose and use
Passenger Facility Charges, [49 U.S.C. 40117].
    A copy of the ROD can be found on the FAA Web site at: http://www.faa.gov/airports/environmental/records_decision/. The ROD and
information on the Project is available for electronic review and/or
download on the on the project Web site at: http://www.phl-cep-eis.com.
Hard copies of the ROD can be obtained by contacting FAA.

FOR FURTHER INFORMATION CONTACT: Susan McDonald, Environmental
Protection Specialist, Federal Aviation Administration, Harrisburg
Airports District Office, 3905 Hartzdale Drive, Suite 508, Camp Hill,
PA 17011, Telephone<PHONE_NUMBER>.

    Issued in Camp Hill, Pennsylvania, December 22, 2010.
Lori Pagnanelli,
Manager, Harrisburg Airports District Office.
[FR Doc. 2010-33223 Filed 1-3-11; 8:45 am]
BILLING CODE 4910-13-P


[Federal Register Volume 87, Number 211 (Wednesday, November 2, 2022)]
[Rules and Regulations]
[Pages 66084-66086]
[FR Doc No: 2022-23899]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

14 CFR Part 39

[Docket No. FAA-2022-1409; Project Identifier AD-2022-01396-A;
Amendment 39-22235; AD 2022-23-08]
RIN 2120-AA64

Airworthiness Directives; Viking Air Limited (Type Certificate
Previously Held by Bombardier Inc. and de Havilland, Inc.)

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Final rule; request for comments.

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SUMMARY: The FAA is adopting a new airworthiness directive (AD) for all
Viking Air Limited (Viking) (type certificate previously held by
Bombardier Inc. and de Havilland, Inc.) Model DHC-3 airplanes. This AD
was prompted by a recent investigation of a Viking Model DHC-3 airplane
where the lock ring of the stabilizer actuator was found missing. This
AD requires a visual inspection of the stabilizer actuator to confirm
that the stabilizer actuator lock ring is present, correctly seated in
the groove in the upper housing, and engaged in the clamp nut,
applicable corrective actions, and application of a torque seal. This
AD also requires sending the inspection results to the FAA. The FAA is
issuing this AD to address the unsafe condition on these products.

DATES: This AD is effective November 2, 2022.
    The FAA must receive comments on this AD by December 19, 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 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.
    AD Docket: You may examine the AD docket at regulations.gov by
searching for and locating Docket No. FAA-2022-1409; 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, any
comments received, and other information. The street address for Docket
Operations is listed above.

FOR FURTHER INFORMATION CONTACT: Elizabeth Dowling, Aviation Safety
Engineer, New York ACO Branch, FAA, 1600 Stewart Avenue, Westbury, NY
11590; phone:<PHONE_NUMBER>; email: [email protected].

SUPPLEMENTARY INFORMATION:

Background

    On September 4, 2022, a fatal accident of a Viking Model DHC-3
airplane in Mutiny Bay near Freeland, WA occurred. The National
Transportation Safety Board investigation showed that the lock ring of
the stabilizer actuator was found missing. The investigation revealed
that the clamp nut that attaches the top eye end and bearing assembly
of the horizontal stabilizer actuator to the actuator barrel had
unscrewed from the barrel. The investigation also found that the
circular wire lock ring, which was designed to prevent the clamp nut
from unscrewing, was not present. This condition, if not detected and
corrected, could result in a reduction or loss of pitch control during
flight with consequent loss of control of the airplane. The FAA is
issuing this AD to address the unsafe condition on these products.

FAA's Determination

    The FAA is issuing this AD because the agency has determined the
unsafe condition described previously is likely to exist or develop in
other products of the same type design.

AD Requirements

    This AD requires a visual inspection of the stabilizer actuator to
confirm that the stabilizer actuator lock ring is present, correctly
seated in the groove in the upper housing, and engaged in the clamp
nut, applicable corrective actions, and application of a torque seal.
This AD also requires sending the inspection results to the FAA.

Interim Action

    The FAA considers this AD to be an interim action. If final action
is later identified, the FAA might consider further rulemaking.

Justification for Immediate Adoption and Determination of the Effective
Date

    Section 553(b)(3)(B) of the Administrative Procedure Act (APA) (5
U.S.C. 551 et seq.) authorizes agencies to dispense with notice and
comment procedures for rules when the agency, for ``good cause,'' finds
that those procedures are ``impracticable, unnecessary, or contrary to
the public interest.'' Under this section, an agency, upon finding good
cause, may issue a final rule without providing notice and seeking
comment prior to issuance. Further, section 553(d) of the APA
authorizes agencies to make rules effective in less than thirty days,
upon a finding of good cause.
    An unsafe condition exists that requires the immediate adoption of
this AD without providing an opportunity for public comments prior to
adoption. The FAA has found that the risk to the flying public
justifies foregoing notice and comment prior to adoption of this rule
because loss of pitch control during flight with consequent loss of
control of the airplane could occur rapidly and without warning due to
a missing or incorrectly seated lock ring in the stabilizer actuator.
Given the significance of the risk presented by this unsafe condition,
it must be immediately addressed. Thus, the FAA has determined that
these airplanes must be inspected within 10 hours time-in-service.
Accordingly, notice and opportunity for prior public comment are
impracticable and contrary to the public interest pursuant to 5 U.S.C.
553(b)(3)(B).
    In addition, the FAA finds that good cause exists pursuant to 5
U.S.C. 553(d) for making this amendment effective in less than 30 days,
for the same reasons the FAA found good cause to forego notice and
comment.

Comments Invited

    The FAA invites you to send any written data, views, or arguments
about this final rule. Send your comments to an address listed under
ADDRESSES. Include ``Docket No. FAA-2022-1409 and Project Identifier
AD-2022-01396-A'' at the beginning of your comments. The most helpful
comments reference a specific portion of the final rule, 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 final rule 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
regulations.gov, including any personal information you provide. The
agency will also post a report summarizing each substantive verbal
contact received about this final rule.

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 AD 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 AD, 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 AD. Submissions containing CBI should be sent to
Elizabeth Dowling, Aviation Safety Engineer, New York ACO Branch, FAA,
1600 Stewart Avenue, Suite 410, Westbury, NY 11590. Any commentary that
the FAA receives which is not specifically designated as CBI will be
placed in the public docket for this rulemaking.

Regulatory Flexibility Act

    The requirements of the Regulatory Flexibility Act (RFA) do not
apply when an agency finds good cause pursuant to 5 U.S.C. 553 to adopt
a rule without prior notice and comment. Because FAA has determined
that it has good cause to adopt this rule without prior notice and
comment, RFA analysis is not required.

Costs of Compliance

    The FAA estimates that this AD affects 63 airplanes of U.S.
registry.
    The FAA estimates the following costs to comply with this AD:

                                                 Estimated Costs
----------------------------------------------------------------------------------------------------------------
                                                                                Cost per      Cost on U.S.
             Action                  Labor cost               Parts cost              product        operators
----------------------------------------------------------------------------------------------------------------
Inspection and Torque Seal       1 work-hour x $85   Not Applicable.............             $85          $5,355
 Application.                     per hour = $85.
Reporting Requirement..........  1 work-hour x $85   Not Applicable.............              85           5,355
                                  per hour = $85.
----------------------------------------------------------------------------------------------------------------

    The FAA has received no definitive data regarding the cost
estimates for the on-condition corrective actions required by this AD.

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

    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, and
    (2) Will not affect intrastate aviation in Alaska.

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

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:

2022-23-08 Viking Air Limited (type certificate previously held by
Bombardier Inc. and de Havilland, Inc.): Amendment 39-22235; Docket
No. FAA-2022-1409; Project Identifier AD-2022-01396-A.

(a) Effective Date

    This airworthiness directive (AD) is effective November 2, 2022.
    None.

(b) Affected ADs

    None.

(c) Applicability

    This AD applies to Viking Air Limited (Viking) (type certificate
previously held by Bombardier Inc. and de Havilland, Inc.) Model
DHC-3 airplanes, all serial numbers, certificated in any category.

(d) Subject

    Joint Aircraft System Component (JASC) Code 5520, Elevator
Structure.

(e) Unsafe Condition

    This AD was prompted by a recent investigation of a Viking Model
DHC-3 airplane where the lock ring of the stabilizer actuator was
found missing. The investigation revealed that the clamp nut that
attaches the top eye end and bearing

assembly of the horizontal stabilizer actuator to the actuator
barrel had unscrewed from the barrel. The investigation also found
that the circular wire lock ring, which was designed to prevent the
clamp nut from unscrewing, was not present. This condition, if not
detected and corrected, could result in a reduction or loss of pitch
control during flight with consequent loss of control of the
airplane.

(f) Compliance

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

(g) Inspection

    Within 10 hours time-in-service (TIS) after the effective date
of this AD, perform a visual inspection of the stabilizer actuator
to confirm that the stabilizer actuator lock ring is present,
correctly seated in the groove in the upper housing, and engaged in
the clamp nut. If the stabilizer actuator lock ring is missing or
not correctly installed, before further flight, repair using a
method approved by the Manager, New York ACO Branch, FAA, at the
address in paragraph (k) of this AD.
    Note to paragraph (g): Viking Service Letter DHC3-SL-27-001,
dated October 25, 2022, contains information related to this AD.

(h) Torque Seal

    Before further flight after the inspection required by paragraph
(g) of this AD, apply a torque seal to the clamp nut and lock ring.

(i) Reporting Requirement

    Within 10 days after the inspection required by paragraph (g) of
this AD or within 10 days after the effective date of this AD,
whichever occurs later, report the results of the inspection to the
FAA at [email protected]. Include the airplane serial number,
airplane hours TIS, hours TIS since last actuator overhaul (if
known), and whether the lock ring was present, missing, or
incorrectly installed.

(j) Alternative Methods of Compliance (AMOCs)

    (1) The Manager, New York ACO 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 certification office, mail it to ATTN: Program
Manager, Continuing Operational Safety, at the address identified in
paragraph (k) of this AD or email to: [email protected]. If
mailing information, also submit information by email.
    (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.
    (3) For service information identified in this AD that is not
incorporated by reference, contact Viking Air Ltd., 1959 de
Havilland Way, Sidney British Columbia, Canada V8L 5V5; phone: (800)
663-8444; email: vikingair.com">[email protected]vikingair.com; website:
vikingair.com.

(k) Related Information

    For more information about this AD, contact Elizabeth Dowling,
Aviation Safety Engineer, New York ACO Branch, FAA, 1600 Stewart
Avenue, Westbury, NY 11590; phone:<PHONE_NUMBER>; email: [email protected].

(l) Material Incorporated by Reference

    None.

    Issued on October 28, 2022.
Ross Landes,
Deputy Director for Regulatory Operations, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2022-23899 Filed 10-31-22; 8:45 am]
BILLING CODE 4910-13-P