Airworthiness Directives; Leonardo S.p.A. Helicopters, 37551-37555 [2020-13440]
Download as PDF
<![CDATA[
Federal Register / Vol. 85, No. 121 / Tuesday, June 23, 2020 / Rules and Regulations
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Definition of an Affected Part for the Reidentification and Validation of Rework/
Repair/Modification
An ‘‘affected part’’ is a TRB having P/N
350A333002.02 and a serial number specified
in Appendix 4.A. of Airbus Helicopters Alert
Service Bulletin EC130–04A007, Revision 0,
dated July 18, 2018 (‘‘ASB EC130–04A007’’).
(h) Part Replacement (Life Limit
Implementation)
Before exceeding 10,000 hours time-inservice (TIS) since first installation on a
helicopter: Remove from service each TRB
having P/N 350A333002.04.
(i) Part Re-Identification and Validation of
Rework/Repair/Modification
(1) Within 1,200 hours TIS after the
effective date of this AD: Re-identify each
affected part, in accordance with 3.B. of the
Accomplishment Instructions of Airbus
Helicopters ASB EC130–04A007.
(2) For each affected part which has been
subject to rework, repair, or modification
before the re-identification, as required by
paragraph (i)(1) of this AD, within 6 months
after the effective date of this AD, contact the
Manager, Rotorcraft Standards Branch, FAA,
for additional applicable maintenance
instructions and, within the compliance time
identified in those instructions, accomplish
those instructions accordingly.
jbell on DSKJLSW7X2PROD with RULES
(j) Parts Installation Prohibition and
Rework/Repair/Modification Limitation
(1) As of the effective date of this AD, no
person may install a TRB having P/N
350A333002.02 and a serial number specified
in Appendix 4.A. of ASB EC130–04A007 on
any helicopter.
(2) As of the effective date of this AD, no
person may accomplish any rework, repair,
or modification of an affected part, unless it
has been determined that the rework, repair,
or modification is FAA-approved for P/N
350A333002.04.
(k) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Rotorcraft Standards
Branch, FAA, may approve AMOCs for this
AD. Send your proposal to: Kristi Bradley,
Aviation Safety Engineer, Safety Management
Section, Rotorcraft Standards Branch, FAA,
10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone 817–222–5485; email 9ASW-FTW-AMOC-Requests@faa.gov.
(2) For operations conducted under a 14
CFR part 119 operating certificate or under
14 CFR part 91, subpart K, notify your
principal inspector or lacking a principal
inspector, the manager of the local flight
standards district office or certificate holding
district office, before operating any aircraft
complying with this AD through an AMOC.
(l) Related Information
(1) The subject of this AD is addressed in
European Aviation Safety Agency (now
European Union Aviation Safety Agency)
(EASA) AD 2018–0182, dated August 28,
VerDate Sep<11>2014
16:24 Jun 22, 2020
Jkt 250001
2018. This EASA AD may be found in the AD
docket on the internet at https://
www.regulations.gov by searching for and
locating Docket No. FAA–2020–0238.
(2) For more information about this AD,
contact Kristi Bradley, Aviation Safety
Engineer, Safety Management Section,
Rotorcraft Standards Branch, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177;
telephone 817–222–5485; email
Kristin.Bradley@faa.gov.
(m) Material Incorporated by Reference
(1) The Director of the Federal Register
approved the incorporation by reference
(IBR) 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) Airbus Helicopters Alert Service
Bulletin EC130–04A007, Revision 0, dated
July 18, 2018.
(ii) [Reserved]
(3) 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.
(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.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fedreg.legal@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on June 4, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020–13404 Filed 6–22–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2019–1020; Product
Identifier 2019–SW–076–AD; Amendment
39–21147; AD 2020–13–02]
RIN 2120–AA64
Airworthiness Directives; Leonardo
S.p.A. Helicopters
Federal Aviation
Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for
comments.
AGENCY:
PO 00000
Frm 00005
Fmt 4700
Sfmt 4700
37551
The FAA is adopting a new
airworthiness directive (AD) for certain
Leonardo S.p.A. Model A119 and
AW119 MKII helicopters. This AD
requires inspecting for movement and
the tightening torque of the tail rotor (T/
R) plug, the installation of the outboard
and inboard faces of the T/R duplex
bearing, and the condition of the T/R
plug threads, nut threads, and T/R
duplex bearing. Depending on the
inspection results, this AD requires
removing parts from service,
reassembling the T/R duplex assembly,
and reporting information. This AD also
prohibits installing a T/R duplex
bearing unless it has been inspected.
This AD was prompted by findings from
a preliminary investigation of a Model
AW119 MKII helicopter accident. The
actions of this AD are intended to
address an unsafe condition on these
products.
SUMMARY:
This AD becomes effective July
8, 2020.
The Director of the Federal Register
approved the incorporation by reference
of a certain document listed in this AD
as of July 8, 2020.
The FAA must receive comments on
this AD by August 7, 2020.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Docket: Go to
https://www.regulations.gov. Follow the
online instructions for sending your
comments electronically.
• Fax: 202–493–2251.
• Mail: Send comments to the U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE, Washington, DC
20590–0001.
• Hand Delivery: Deliver to the
‘‘Mail’’ address between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
DATES:
Examining the AD Docket
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
1020; 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 AD, the
European Union Aviation Safety Agency
(EASA) AD, any service information
that is incorporated by reference, any
comments received, and other
information. The street address for
Docket Operations is listed above.
Comments will be available in the AD
docket shortly after receipt.
For service information identified in
this final rule, contact Leonardo S.p.A.
E:\FR\FM\23JNR1.SGM
23JNR1
37552
Federal Register / Vol. 85, No. 121 / Tuesday, June 23, 2020 / Rules and Regulations
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://
www.leonardocompany.com/en/home.
You may view the referenced service
information at the FAA, Office of the
Regional Counsel, Southwest Region,
10101 Hillwood Pkwy., Room 6N–321,
Fort Worth, TX 76177. It is also
available on the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2019–
1020.
FOR FURTHER INFORMATION CONTACT:
David Hatfield, Aviation Safety
Engineer, Safety Management Section,
Rotorcraft Standards Branch, FAA,
10101 Hillwood Pkwy., Fort Worth, TX
76177; telephone 817–222–5110; email
david.hatfield@faa.gov.
SUPPLEMENTARY INFORMATION:
jbell on DSKJLSW7X2PROD with RULES
Comments Invited
This AD is a final rule that involves
requirements affecting flight safety, and
the FAA did not provide you with
notice and an opportunity to provide
your comments prior to it becoming
effective. However, the FAA invites you
to participate in this rulemaking by
submitting written comments, data, or
views. The FAA also invites comments
relating to the economic, environmental,
energy, or federalism impacts that
resulted from adopting this AD. The
most helpful comments reference a
specific portion of the AD, explain the
reason for any recommended change,
and include supporting data. To ensure
the docket does not contain duplicate
comments, commenters should send
only one copy of written comments, or
if comments are filed electronically,
commenters should submit them only
one time. The FAA will file in the
docket all comments received, as well as
a report summarizing each substantive
public contact with FAA personnel
concerning this rulemaking during the
comment period. The FAA will consider
all the comments received and may
conduct additional rulemaking based on
those comments.
Discussion
EASA, which is the Technical Agent
for the Member States of the European
Union, has issued EASA Emergency AD
No. 2019–0194–E, dated August 9, 2019,
to correct an unsafe condition for
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 A119 and
VerDate Sep<11>2014
16:24 Jun 22, 2020
Jkt 250001
AW119MKII helicopters with a serial
number (S/N) up to 14966 inclusive,
except S/N 14950, 14957, and 14961
through 14963 inclusive. According to
EASA, preliminary investigation of a
Model AW119 MKII helicopter accident
identified a disassembled connection
between the yaw control input lever and
the rotating input shaft, partial presence
of spalling on the T/R duplex bearing
inner races, and missing plug and
related lockwire. EASA states an
investigation to determine the root
cause of the occurrence is in progress.
EASA advises that this condition, if not
corrected, could lead to functional
failure of the T/R pitch change
mechanism, resulting in loss of control
of the helicopter.
As a precautionary measure and
pending further information from the
investigation, Leonardo S.p.A. issued
Leonardo Helicopters Emergency Alert
Service Bulletin No. 119–100, dated
August 7, 2019 (EASB 119–100), to
provide inspection instructions and
improved installation procedures for the
T/R duplex bearing.
Accordingly, the EASA AD requires
inspecting the T/R pitch change
mechanism and installation of
additional locking wire. The EASA AD
also requires repetitive inspections of
the duplex bearing and, depending on
findings, corrective actions. EASA states
its AD is considered an interim action
and further AD action may follow.
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 of the unsafe condition described
in its AD. The FAA is issuing this AD
after evaluating all information
provided by EASA and determining the
unsafe condition exists and is likely to
exist or develop on other helicopters of
these same type designs.
Related Service Information Under 1
CFR Part 51
The FAA has reviewed EASB 119–100
which specifies a one-time inspection of
the tightening torque of T/R plug part
number (P/N) 129–0160–45–103. This
service information also specifies a
repetitive inspection for correct
installation of the inboard and outboard
faces of T/R duplex bearing P/N 129–
0160–11–103, for damage to the threads
of the T/R plug and nut P/N MS17825–
7, and of the T/R duplex bearing for
roughness, ease of rotation, and
presence of brinelling, spalling,
chipping, and flaking or traces of
PO 00000
Frm 00006
Fmt 4700
Sfmt 4700
overheating of bearing balls, and general
damage to races.
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.
AD Requirements
• This AD requires, within 10 hours
time-in-service (TIS), inspecting for
movement and the tightening torque of
the T/R plug.
• If there is no movement and the
tightening torque is at least 30.5 Nm,
this AD requires installing lockwire
before further flight. Thereafter, within
50 hours TIS, this AD requires
inspecting for presence of the P/N and
S/N markings of the outboard and
inboard faces of T/R duplex bearing,
inspecting the T/R duplex bearing for
rough rotation, brinelling, spalling,
chipping, flaking, evidence of
overheated bearing balls, and damage to
the races, and inspecting for damaged
threads of the T/R plug and nut.
• If there is any movement or the
tightening torque is less than 30.5 Nm,
this AD requires inspecting for presence
of the P/N and S/N markings of the
outboard and inboard faces of T/R
duplex bearing, inspecting the T/R
duplex bearing for rough rotation,
brinelling, spalling, chipping, flaking,
evidence of overheated bearing balls,
and damage to the races, and inspecting
for damaged threads of the T/R plug and
nut before further flight.
• If the P/N and S/N markings are
visible on the outboard or inboard face
of the T/R duplex bearing; the T/R
duplex bearing has any rough rotation,
brinelling, spalling, chipping, flaking,
evidence of overheated bearing balls, or
damage to the races; or if the nut has
any damaged threads, this AD requires
removing the T/R duplex bearing,
internal spacer, external spacer, bearing
liner assembly, and T/R control rod
from service before further flight.
• If the T/R plug or nut has any
damaged threads, this AD requires
removing the affected part from service
before further flight.
• After inspecting, this AD requires
assembling and installing the T/R
duplex assembly by following related
service information procedures.
• This AD also requires reporting
inspection results to Leonardo
Helicopters if there is any T/R plug
movement or if its tightening torque is
not at least 30.5 Nm and any parts that
must be removed from service.
• This AD also prohibits installing a
T/R duplex bearing on any helicopter
unless it has been inspected.
E:\FR\FM\23JNR1.SGM
23JNR1
Federal Register / Vol. 85, No. 121 / Tuesday, June 23, 2020 / Rules and Regulations
Differences Between This AD and the
EASA AD
The EASA AD requires repeating the
inspection of the T/R duplex bearing
installation and the condition of the T/
R duplex bearing, plug threads, and nut
threads at any installation or
disassembly of the T/R duplex bearing,
whereas this AD does not because it
could be difficult to track. The EASA
AD requires inspecting the tightening
torque of the T/R plug in the range of
30.5–33.9 Nm, whereas this AD requires
inspecting the tightening torque of the
T/R plug to a minimum of 30.5 Nm
instead. The EASA AD requires
inspecting the threads of nut P/N
MS17825–7 for damage, but does not
state what to do if the threads have
damage. This AD requires inspecting for
damage to the threads of the nut
indicated by uneven threads, missing
threads, or cross-threading, and if the
nut has any damaged threads, removing
the nut from service. The EASA AD also
requires repeating the inspection of the
T/R duplex bearing installation and the
condition of the T/R duplex bearing,
plug threads, and nut threads every 200
hours TIS, whereas this AD does not.
The FAA plans to publish a notice of
proposed rulemaking to give the public
an opportunity to comment on this longterm requirement.
Interim Action
The FAA considers this AD to be an
interim action. If final action is later
identified, the FAA might consider
further 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 notice and
comment, RFA analysis is not required.
jbell on DSKJLSW7X2PROD with RULES
Costs of Compliance
The FAA estimates that this AD
affects 93 helicopters of U.S. Registry.
Labor costs 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 AD.
Inspecting the tightening torque of the
T/R plug takes about 0.5 work-hour for
an estimated cost of $43 per helicopter
and $3,999 for the U.S. fleet.
Inspecting for correct installation of
the outboard and inboard faces of the T/
R duplex bearing and the condition of
the T/R plug threads, nut threads, and
T/R duplex bearing takes about 2 work-
VerDate Sep<11>2014
16:24 Jun 22, 2020
Jkt 250001
hours for an estimated cost of $170 per
helicopter.
Assembling and installing the T/R
duplex bearing assembly takes about 2
work-hours for an estimated cost of
$170. If required, the parts for replacing
the T/R duplex bearing, internal spacer,
external spacer, bearing liner assembly,
and T/R control rod cost about $4,200,
and parts for replacing the T/R plug cost
about $171.
If required, reporting information
takes about 1 work-hour for an
estimated cost of $85 per instance.
According to Leonardo Helicopters’
service information, some of the costs of
this AD may be covered under warranty,
thereby reducing the cost impact on
affected individuals. The FAA does not
control warranty coverage by Leonardo
Helicopters. Accordingly, the FAA has
included all costs in this cost estimate.
Paperwork Reduction Act
FAA’s Justification and Determination
of the Effective Date
Section 553(b)(3)(B) of the
Administrative Procedure Act (5 U.S.C.)
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
seeking comment prior to the
rulemaking.
Frm 00007
Fmt 4700
Sfmt 4700
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 waiving notice
and comment prior to adoption of this
rule because there are required
corrective actions that must be
completed within 10 hours TIS and 50
hours TIS, a time period of up to 2
months based on the average flight-hour
utilization rate of these helicopters.
Therefore, notice and opportunity for
prior public comment are impracticable
and contrary to public interest pursuant
to 5 U.S.C. 553(b)(3)(B). In addition, for
the reasons stated above, 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.
Authority for This Rulemaking
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.
PO 00000
37553
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 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, 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.
E:\FR\FM\23JNR1.SGM
23JNR1
37554
Federal Register / Vol. 85, No. 121 / Tuesday, June 23, 2020 / Rules and Regulations
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
Adoption of 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.
§ 39.13
[Amended]
2. The FAA amends § 39.13 by adding
the following new airworthiness
directive (AD):
■
2020–13–02 Leonardo S.p.A.: Amendment
39–21147; Docket No. FAA–2019–1020;
Product Identifier 2019–SW–076–AD.
(a) Applicability
This AD applies to Leonardo S.p.A. Model
A119 and AW119 MKII helicopters,
certificated in any category, with a tail rotor
(T/R) duplex bearing part number (P/N) 129–
0160–11–103 (T/R duplex bearing).
(b) Unsafe Condition
This AD defines the unsafe condition as
structural failure of the T/R assembly,
possibly due to an incorrect installation. This
condition could result in loss of T/R pitch
change control and subsequent loss of control
of the helicopter.
(c) Effective Date
This AD becomes effective July 8, 2020.
jbell on DSKJLSW7X2PROD with RULES
(d) Compliance
You are responsible for performing each
action required by this AD within the
specified compliance time unless it has
already been accomplished prior to that time.
(e) Required Actions
(1) Within 10 hours time-in-service (TIS),
remove the lockwire that secures the T/R
plug P/N 129–0160–45–103 (T/R plug) to the
bearing liner assembly P/N 109–0135–16–101
(bearing liner assembly). Without loosening
the T/R plug first, inspect the tightening
torque of the T/R plug by increasing the
torque up to 30.5 Nm and inspect for any
movement the moment torque is applied.
(i) If there is no movement and the
tightening torque is at least 30.5 Nm, before
further flight, install lockwire by following
the Accomplishment Instructions, part I,
paragraph 4, of Leonardo Helicopters
Emergency Alert Service Bulletin No. 119–
100, dated August 7, 2019 (EASB 119–100).
(ii) If there is any movement or the
tightening torque is less than 30.5 Nm, before
further flight, comply with paragraph (e)(2) of
this AD.
(2) Within 50 hours TIS, unless required
before further flight by paragraph (e)(1)(ii) of
this AD, inspect to determine whether the P/
VerDate Sep<11>2014
16:24 Jun 22, 2020
Jkt 250001
N and serial number (S/N) are visible on the
outboard and inboard faces of the T/R duplex
bearing by following the Accomplishment
Instructions, part II, paragraphs 4 through 13
(except paragraphs 9.1, 13.1, and 13.2), of
EASB 119–100. Instead of the excluded steps,
do the following:
Note 1 to paragraph (e)(2) of this AD: You
are not required to discard parts and you may
use equivalent tooling to that identified in
EASB 119–100.
(i) If the P/N and S/N markings are visible
on the outboard or inboard face of the T/R
duplex bearing, before further flight, remove
from service the T/R duplex bearing, internal
spacer P/N 129–0160–43–101 (internal
spacer), external spacer P/N 129–0160–44–
101 (external spacer), bearing liner assembly,
and T/R control rod P/N 109–0135–02–101
(T/R control rod).
(ii) If the P/N and S/N markings are not
visible on the inboard face of the T/R duplex
bearing, before further flight, inspect the T/
R duplex bearing, T/R plug, and nut by
following the Accomplishment Instructions,
part II, paragraphs 14 and 15 (but not
paragraphs 15.1 through 15.2), of EASB 119–
100. For purposes of this inspection, damage
to the races may be indicated by nonmovement of the inner race, movement of the
outer race, deformation, roughness, or
incorrect installation; and damage to the
threads of the T/R plug and nut may be
indicated by uneven threads, missing
threads, or cross-threading.
(A) If the T/R duplex bearing has any rough
rotation, brinelling, spalling, chipping,
flaking, evidence of overheated bearing balls,
or damage to the races, before further flight,
remove from service the T/R duplex bearing,
the internal spacer, the external spacer, the
bearing liner assembly, and the T/R control
rod.
(B) If the T/R plug or nut has any damaged
threads, before further flight, remove from
service the affected part.
(C) Reassemble the T/R duplex bearing
assembly by following the Accomplishment
Instructions, part II, paragraphs 16 through
31, of EASB 119–100.
(3) If the T/R plug had any movement or
its tightening torque was not at least 30.5 Nm
in paragraph (e)(1)(ii) of this AD or if any
parts were required to be removed as a result
of the inspections required by paragraph
(e)(2) of this AD, within 10 days after
completing the inspection, report the
information in Appendix 1 to this AD by
email to aw109.mbx.aw@
leonardocompany.com.
(4) As of the effective date of this AD, do
not install a T/R duplex bearing P/N 129–
0160–11–103 on any helicopter unless you
have complied with the requirements in
paragraph (e)(2) of this AD.
(f) Special Flight Permits
Special flight permits are prohibited.
(g) Paperwork Reduction Act Burden
Statement
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
PO 00000
Frm 00008
Fmt 4700
Sfmt 4700
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.
(h) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Safety Management
Section, Rotorcraft Standards Branch, FAA,
may approve AMOCs for this AD. Send your
proposal to: David Hatfield, Aviation Safety
Engineer, Safety Management Section,
Rotorcraft Standards Branch, FAA, 10101
Hillwood Pkwy., Fort Worth, TX 76177;
telephone 817–222–5110; email 9-ASW-FTWAMOC-Requests@faa.gov.
(2) For operations conducted under a 14
CFR part 119 operating certificate or sunder
14 CFR part 91, subpart K, the FAA suggests
that you notify your principal inspector, or
lacking a principal inspector, the manager of
the local flight standards district office or
certificate holding district office, before
operating any aircraft complying with this
AD through an AMOC.
(i) Additional Information
The subject of this AD is addressed in
European Union Aviation Safety Agency
(EASA) Emergency AD No. 2019–0194–E,
dated August 9, 2019. You may view the
EASA AD on the Internet at https://
www.regulations.gov by searching for and
locating it in Docket No. FAA–2019–1020.
(j) Subject
Joint Aircraft Service Component (JASC)
Code: 6400, Tail Rotor System.
(k) 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 the AD specifies otherwise.
(i) Leonardo Helicopters Emergency Alert
Service Bulletin No. 119–100, dated August
7, 2019.
(ii) [Reserved]
(3) For Leonardo Helicopters 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://
www.leonardocompany.com/en/home.
E:\FR\FM\23JNR1.SGM
23JNR1
Federal Register / Vol. 85, No. 121 / Tuesday, June 23, 2020 / Rules and Regulations
(4) You may view this service information
at 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.
(5) You may view this service information
that is incorporated by reference at the
National Archives and Records
Administration (NARA). For information on
the availability of this material at NARA,
email fedreg.legal@nara.gov, or go to: https://
www.archives.gov/federal-register/cfr/ibrlocations.html.
Appendix 1 to AD 2020–13–02
Report the following information by email
to aw109.mbx.aw@leonardocompany.com.
(Leonardo Helicopters Emergency Alert
Service Bulletin No. 119–100, dated August
7, 2019.)
(1) Date of Inspection:
(2) Helicopter Model and Serial Number:
(3) Total hours time-in-service (TIS) on the
aircraft:
(4) Total hours TIS on the T/R duplex
bearing:
(5) Total hours TIS since last overhaul of
the T/R gearbox assembly:
(6) Describe in detail any information and
findings and, if possible, provide photos.
Issued on June 10, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
Authority for This Rulemaking
[FR Doc. 2020–13440 Filed 6–22–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2019–0474; Airspace
Docket No. 19–AEA–2]
RIN 2120–AA66
Amendment of Air Traffic Service
(ATS) Routes in the Vicinity of Glens
Falls, NY
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
jbell on DSKJLSW7X2PROD with RULES
VerDate Sep<11>2014
16:24 Jun 22, 2020
Jkt 250001
The FAA’s authority to issue rules
regarding aviation safety is found in
Title 49 of the United States Code.
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. This rulemaking is
promulgated under the authority
described in Subtitle VII, Part A,
Subpart I, Section 40103. Under that
section, the FAA is charged with
prescribing regulations to assign the use
of the airspace necessary to ensure the
safety of aircraft and the efficient use of
airspace. This regulation is within the
scope of that authority as it modifies the
route structure in the National Airspace
System as necessary to preserve the safe
and efficient flow of air traffic.
History
This action amends VHF
Omnidirectional Range (VOR) Federal
airways V–91, V–123, V–431, V–489,
and V–496 due to the planned
decommissioning of the Glens Falls,
NY, VORTAC navigation aid which
provides navigation guidance for
segments of the routes. The Glens Falls
VORTAC is being decommissioned as
part of the FAA’s VOR Minimum
Operational Network (MON) program.
DATES: Effective date 0901 UTC,
September 10, 2020. The Director of the
Federal Register approves this
incorporation by reference action under
SUMMARY:
Title 1 Code of Federal Regulations part
51, subject to the annual revision of
FAA Order 7400.11 and publication of
conforming amendments.
ADDRESSES: FAA Order 7400.11D,
Airspace Designations and Reporting
Points, and subsequent amendments can
be viewed online at https://
www.faa.gov/air_traffic/publications/.
For further information, you can contact
the Rules and Regulations Group,
Federal Aviation Administration, 800
Independence Avenue SW, Washington,
DC 20591; telephone: (202) 267–8783.
The Order is also available for
inspection at the National Archives and
Records Administration (NARA). For
information on the availability of FAA
Order 7400.11D at NARA, email:
fedreg.legal@nara.gov, or go to https://
www.archives.gov/federal-register/cfr/
ibr-locations.html.
FOR FURTHER INFORMATION CONTACT: Paul
Gallant, Rules and Regulations Group,
Office of Policy, Federal Aviation
Administration, 800 Independence
Avenue SW, Washington, DC 20591;
telephone: (202) 267–8783.
SUPPLEMENTARY INFORMATION:
The FAA published a notice of
proposed rulemaking in the Federal
Register for Docket No. FAA–2019–0474
(84 FR 34075; July 17, 2019) amending
VOR Federal airways V–91, V–123, V–
431, V–489, and V–496 due to the
planned decommissioning of the Glens
Falls, NY, VORTAC. Interested parties
were invited to participate in this
rulemaking effort by submitting written
comments on the proposal. No
comments were received.
VOR Federal airways are published in
paragraph 6010(a) of FAA Order
7400.11D dated August 8, 2019, and
PO 00000
Frm 00009
Fmt 4700
Sfmt 4700
37555
effective September 15, 2019, which is
incorporated by reference in 14 CFR
71.1. The VOR Federal airways listed in
this document will be subsequently
published in the Order.
Availability and Summary of
Documents for Incorporation by
Reference
This document amends FAA Order
7400.11D, Airspace Designations and
Reporting Points, dated August 8, 2019,
and effective September 15, 2019. FAA
Order 7400.11D is publicly available as
listed in the ADDRESSES section of this
document. FAA Order 7400.11D lists
Class A, B, C, D, and E airspace areas,
air traffic service routes, and reporting
points.
The Rule
The FAA is amending Title 14 Code
of Federal Regulations (14 CFR) part 71
by amending VOR Federal airways V–
91, V–123, V–431, V–489, and V–496
due to the planned decommissioning of
the Glens Falls, NY, VORTAC. The
airway changes are described below.
V–91: V–91 currently extends
between the intersection of the
Calverton, NY, VOR/DME 180° radial,
and the Hampton, NY, VORTAC 223°
radial; and the Burlington, VT, VOR/
DME. The FAA is removing the route
segments between the Albany, NY,
VORTAC, and Burlington, VT. As
amended, V–91 extends between the
intersection of the above Calverton and
Hampton radials; and Albany, NY.
Alternative routing between Albany and
Burlington, VT, is available via V–542
from Albany to Cambridge, NY, then V–
487 to Burlington.
V–123: V–123 currently extends
between the intersection of the
Washington, DC, VOR/DME 065° radial,
and the Baltimore, MD, VORTAC 197°
radial; and the Glens Falls, NY,
VORTAC. This action removes the
segment between the Cambridge, NY,
VOR/DME and Glens Falls. As
amended, V–123 extends between the
intersection of the above Washington,
DC, and the Baltimore, MD, radials; and
the Cambridge, NY, VOR/DME.
V–431: V–431 currently extends
between the intersection of the Boston,
MA, VOR/DME 015° radial, and the
Gardner, MA, VOR/DME 097° radial;
and the intersection of the Glens Falls,
NY, VORTAC 286° radial, and the
Albany, NY, VORTAC 350° radial. This
action removes the segments between
the Gardner, MA, VOR/DME, and the
intersection of the Glens Falls, NY 286°
and the Albany, NY 350° radials. The
amended route extends between the
intersection of the Boston, MA, VOR/
DME 015° radial, and the Gardner, MA,
E:\FR\FM\23JNR1.SGM
23JNR1
]]>Agencies
[Federal Register Volume 85, Number 121 (Tuesday, June 23, 2020)]
[Rules and Regulations]
[Pages 37551-37555]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-13440]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2019-1020; Product Identifier 2019-SW-076-AD; Amendment
39-21147; AD 2020-13-02]
RIN 2120-AA64
Airworthiness Directives; Leonardo S.p.A. Helicopters
AGENCY: Federal Aviation Administration (FAA), Department of
Transportation (DOT).
ACTION: Final rule; request for comments.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Leonardo S.p.A. Model A119 and AW119 MKII helicopters. This AD
requires inspecting for movement and the tightening torque of the tail
rotor (T/R) plug, the installation of the outboard and inboard faces of
the T/R duplex bearing, and the condition of the T/R plug threads, nut
threads, and T/R duplex bearing. Depending on the inspection results,
this AD requires removing parts from service, reassembling the T/R
duplex assembly, and reporting information. This AD also prohibits
installing a T/R duplex bearing unless it has been inspected. This AD
was prompted by findings from a preliminary investigation of a Model
AW119 MKII helicopter accident. The actions of this AD are intended to
address an unsafe condition on these products.
DATES: This AD becomes effective July 8, 2020.
The Director of the Federal Register approved the incorporation by
reference of a certain document listed in this AD as of July 8, 2020.
The FAA must receive comments on this AD by August 7, 2020.
ADDRESSES: You may send comments by any of the following methods:
Federal eRulemaking Docket: Go to https://www.regulations.gov. Follow the online instructions for sending your
comments electronically.
Fax: 202-493-2251.
Mail: Send comments to the U.S. Department of
Transportation, Docket Operations, M-30, West Building Ground Floor,
Room W12-140, 1200 New Jersey Avenue SE, Washington, DC 20590-0001.
Hand Delivery: Deliver to the ``Mail'' address between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
Examining the AD Docket
You may examine the AD docket on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
1020; 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 AD, the European Union Aviation Safety Agency (EASA) AD, any
service information that is incorporated by reference, any comments
received, and other information. The street address for Docket
Operations is listed above. Comments will be available in the AD docket
shortly after receipt.
For service information identified in this final rule, contact
Leonardo S.p.A.
[[Page 37552]]
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://www.leonardocompany.com/en/home. You
may view the referenced service information at the FAA, Office of the
Regional Counsel, Southwest Region, 10101 Hillwood Pkwy., Room 6N-321,
Fort Worth, TX 76177. It is also available on the internet at https://www.regulations.gov by searching for and locating Docket No. FAA-2019-
1020.
FOR FURTHER INFORMATION CONTACT: David Hatfield, Aviation Safety
Engineer, Safety Management Section, Rotorcraft Standards Branch, FAA,
10101 Hillwood Pkwy., Fort Worth, TX 76177; telephone 817-222-5110;
email [email protected].
SUPPLEMENTARY INFORMATION:
Comments Invited
This AD is a final rule that involves requirements affecting flight
safety, and the FAA did not provide you with notice and an opportunity
to provide your comments prior to it becoming effective. However, the
FAA invites you to participate in this rulemaking by submitting written
comments, data, or views. The FAA also invites comments relating to the
economic, environmental, energy, or federalism impacts that resulted
from adopting this AD. The most helpful comments reference a specific
portion of the AD, explain the reason for any recommended change, and
include supporting data. To ensure the docket does not contain
duplicate comments, commenters should send only one copy of written
comments, or if comments are filed electronically, commenters should
submit them only one time. The FAA will file in the docket all comments
received, as well as a report summarizing each substantive public
contact with FAA personnel concerning this rulemaking during the
comment period. The FAA will consider all the comments received and may
conduct additional rulemaking based on those comments.
Discussion
EASA, which is the Technical Agent for the Member States of the
European Union, has issued EASA Emergency AD No. 2019-0194-E, dated
August 9, 2019, to correct an unsafe condition for 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 A119 and AW119MKII helicopters with
a serial number (S/N) up to 14966 inclusive, except S/N 14950, 14957,
and 14961 through 14963 inclusive. According to EASA, preliminary
investigation of a Model AW119 MKII helicopter accident identified a
disassembled connection between the yaw control input lever and the
rotating input shaft, partial presence of spalling on the T/R duplex
bearing inner races, and missing plug and related lockwire. EASA states
an investigation to determine the root cause of the occurrence is in
progress. EASA advises that this condition, if not corrected, could
lead to functional failure of the T/R pitch change mechanism, resulting
in loss of control of the helicopter.
As a precautionary measure and pending further information from the
investigation, Leonardo S.p.A. issued Leonardo Helicopters Emergency
Alert Service Bulletin No. 119-100, dated August 7, 2019 (EASB 119-
100), to provide inspection instructions and improved installation
procedures for the T/R duplex bearing.
Accordingly, the EASA AD requires inspecting the T/R pitch change
mechanism and installation of additional locking wire. The EASA AD also
requires repetitive inspections of the duplex bearing and, depending on
findings, corrective actions. EASA states its AD is considered an
interim action and further AD action may follow.
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 of the
unsafe condition described in its AD. The FAA is issuing this AD after
evaluating all information provided by EASA and determining the unsafe
condition exists and is likely to exist or develop on other helicopters
of these same type designs.
Related Service Information Under 1 CFR Part 51
The FAA has reviewed EASB 119-100 which specifies a one-time
inspection of the tightening torque of T/R plug part number (P/N) 129-
0160-45-103. This service information also specifies a repetitive
inspection for correct installation of the inboard and outboard faces
of T/R duplex bearing P/N 129-0160-11-103, for damage to the threads of
the T/R plug and nut P/N MS17825-7, and of the T/R duplex bearing for
roughness, ease of rotation, and presence of brinelling, spalling,
chipping, and flaking or traces of overheating of bearing balls, and
general damage to races.
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.
AD Requirements
This AD requires, within 10 hours time-in-service (TIS),
inspecting for movement and the tightening torque of the T/R plug.
If there is no movement and the tightening torque is at
least 30.5 Nm, this AD requires installing lockwire before further
flight. Thereafter, within 50 hours TIS, this AD requires inspecting
for presence of the P/N and S/N markings of the outboard and inboard
faces of T/R duplex bearing, inspecting the T/R duplex bearing for
rough rotation, brinelling, spalling, chipping, flaking, evidence of
overheated bearing balls, and damage to the races, and inspecting for
damaged threads of the T/R plug and nut.
If there is any movement or the tightening torque is less
than 30.5 Nm, this AD requires inspecting for presence of the P/N and
S/N markings of the outboard and inboard faces of T/R duplex bearing,
inspecting the T/R duplex bearing for rough rotation, brinelling,
spalling, chipping, flaking, evidence of overheated bearing balls, and
damage to the races, and inspecting for damaged threads of the T/R plug
and nut before further flight.
If the P/N and S/N markings are visible on the outboard or
inboard face of the T/R duplex bearing; the T/R duplex bearing has any
rough rotation, brinelling, spalling, chipping, flaking, evidence of
overheated bearing balls, or damage to the races; or if the nut has any
damaged threads, this AD requires removing the T/R duplex bearing,
internal spacer, external spacer, bearing liner assembly, and T/R
control rod from service before further flight.
If the T/R plug or nut has any damaged threads, this AD
requires removing the affected part from service before further flight.
After inspecting, this AD requires assembling and
installing the T/R duplex assembly by following related service
information procedures.
This AD also requires reporting inspection results to
Leonardo Helicopters if there is any T/R plug movement or if its
tightening torque is not at least 30.5 Nm and any parts that must be
removed from service.
This AD also prohibits installing a T/R duplex bearing on
any helicopter unless it has been inspected.
[[Page 37553]]
Differences Between This AD and the EASA AD
The EASA AD requires repeating the inspection of the T/R duplex
bearing installation and the condition of the T/R duplex bearing, plug
threads, and nut threads at any installation or disassembly of the T/R
duplex bearing, whereas this AD does not because it could be difficult
to track. The EASA AD requires inspecting the tightening torque of the
T/R plug in the range of 30.5-33.9 Nm, whereas this AD requires
inspecting the tightening torque of the T/R plug to a minimum of 30.5
Nm instead. The EASA AD requires inspecting the threads of nut P/N
MS17825-7 for damage, but does not state what to do if the threads have
damage. This AD requires inspecting for damage to the threads of the
nut indicated by uneven threads, missing threads, or cross-threading,
and if the nut has any damaged threads, removing the nut from service.
The EASA AD also requires repeating the inspection of the T/R duplex
bearing installation and the condition of the T/R duplex bearing, plug
threads, and nut threads every 200 hours TIS, whereas this AD does not.
The FAA plans to publish a notice of proposed rulemaking to give the
public an opportunity to comment on this long-term requirement.
Interim Action
The FAA considers this AD to be an interim action. If final action
is later identified, the FAA might consider further 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 notice and comment,
RFA analysis is not required.
Costs of Compliance
The FAA estimates that this AD affects 93 helicopters of U.S.
Registry. Labor costs 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 AD.
Inspecting the tightening torque of the T/R plug takes about 0.5
work-hour for an estimated cost of $43 per helicopter and $3,999 for
the U.S. fleet.
Inspecting for correct installation of the outboard and inboard
faces of the T/R duplex bearing and the condition of the T/R plug
threads, nut threads, and T/R duplex bearing takes about 2 work-hours
for an estimated cost of $170 per helicopter.
Assembling and installing the T/R duplex bearing assembly takes
about 2 work-hours for an estimated cost of $170. If required, the
parts for replacing the T/R duplex bearing, internal spacer, external
spacer, bearing liner assembly, and T/R control rod cost about $4,200,
and parts for replacing the T/R plug cost about $171.
If required, reporting information takes about 1 work-hour for an
estimated cost of $85 per instance.
According to Leonardo Helicopters' service information, some of the
costs of this AD may be covered under warranty, thereby reducing the
cost impact on affected individuals. The FAA does not control warranty
coverage by Leonardo Helicopters. Accordingly, the FAA has included all
costs in this cost estimate.
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.
FAA's Justification and Determination of the Effective Date
Section 553(b)(3)(B) of the Administrative Procedure Act (5 U.S.C.)
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 seeking comment prior to the rulemaking.
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 waiving notice and comment prior to adoption of this rule
because there are required corrective actions that must be completed
within 10 hours TIS and 50 hours TIS, a time period of up to 2 months
based on the average flight-hour utilization rate of these helicopters.
Therefore, notice and opportunity for prior public comment are
impracticable and contrary to public interest pursuant to 5 U.S.C.
553(b)(3)(B). In addition, for the reasons stated above, 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.
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 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, 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.
[[Page 37554]]
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
Adoption of 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 (AD):
2020-13-02 Leonardo S.p.A.: Amendment 39-21147; Docket No. FAA-2019-
1020; Product Identifier 2019-SW-076-AD.
(a) Applicability
This AD applies to Leonardo S.p.A. Model A119 and AW119 MKII
helicopters, certificated in any category, with a tail rotor (T/R)
duplex bearing part number (P/N) 129-0160-11-103 (T/R duplex
bearing).
(b) Unsafe Condition
This AD defines the unsafe condition as structural failure of
the T/R assembly, possibly due to an incorrect installation. This
condition could result in loss of T/R pitch change control and
subsequent loss of control of the helicopter.
(c) Effective Date
This AD becomes effective July 8, 2020.
(d) Compliance
You are responsible for performing each action required by this
AD within the specified compliance time unless it has already been
accomplished prior to that time.
(e) Required Actions
(1) Within 10 hours time-in-service (TIS), remove the lockwire
that secures the T/R plug P/N 129-0160-45-103 (T/R plug) to the
bearing liner assembly P/N 109-0135-16-101 (bearing liner assembly).
Without loosening the T/R plug first, inspect the tightening torque
of the T/R plug by increasing the torque up to 30.5 Nm and inspect
for any movement the moment torque is applied.
(i) If there is no movement and the tightening torque is at
least 30.5 Nm, before further flight, install lockwire by following
the Accomplishment Instructions, part I, paragraph 4, of Leonardo
Helicopters Emergency Alert Service Bulletin No. 119-100, dated
August 7, 2019 (EASB 119-100).
(ii) If there is any movement or the tightening torque is less
than 30.5 Nm, before further flight, comply with paragraph (e)(2) of
this AD.
(2) Within 50 hours TIS, unless required before further flight
by paragraph (e)(1)(ii) of this AD, inspect to determine whether the
P/N and serial number (S/N) are visible on the outboard and inboard
faces of the T/R duplex bearing by following the Accomplishment
Instructions, part II, paragraphs 4 through 13 (except paragraphs
9.1, 13.1, and 13.2), of EASB 119-100. Instead of the excluded
steps, do the following:
Note 1 to paragraph (e)(2) of this AD: You are not required to
discard parts and you may use equivalent tooling to that identified
in EASB 119-100.
(i) If the P/N and S/N markings are visible on the outboard or
inboard face of the T/R duplex bearing, before further flight,
remove from service the T/R duplex bearing, internal spacer P/N 129-
0160-43-101 (internal spacer), external spacer P/N 129-0160-44-101
(external spacer), bearing liner assembly, and T/R control rod P/N
109-0135-02-101 (T/R control rod).
(ii) If the P/N and S/N markings are not visible on the inboard
face of the T/R duplex bearing, before further flight, inspect the
T/R duplex bearing, T/R plug, and nut by following the
Accomplishment Instructions, part II, paragraphs 14 and 15 (but not
paragraphs 15.1 through 15.2), of EASB 119-100. For purposes of this
inspection, damage to the races may be indicated by non-movement of
the inner race, movement of the outer race, deformation, roughness,
or incorrect installation; and damage to the threads of the T/R plug
and nut may be indicated by uneven threads, missing threads, or
cross-threading.
(A) If the T/R duplex bearing has any rough rotation,
brinelling, spalling, chipping, flaking, evidence of overheated
bearing balls, or damage to the races, before further flight, remove
from service the T/R duplex bearing, the internal spacer, the
external spacer, the bearing liner assembly, and the T/R control
rod.
(B) If the T/R plug or nut has any damaged threads, before
further flight, remove from service the affected part.
(C) Reassemble the T/R duplex bearing assembly by following the
Accomplishment Instructions, part II, paragraphs 16 through 31, of
EASB 119-100.
(3) If the T/R plug had any movement or its tightening torque
was not at least 30.5 Nm in paragraph (e)(1)(ii) of this AD or if
any parts were required to be removed as a result of the inspections
required by paragraph (e)(2) of this AD, within 10 days after
completing the inspection, report the information in Appendix 1 to
this AD by email to [email protected].
(4) As of the effective date of this AD, do not install a T/R
duplex bearing P/N 129-0160-11-103 on any helicopter unless you have
complied with the requirements in paragraph (e)(2) of this AD.
(f) Special Flight Permits
Special flight permits are prohibited.
(g) Paperwork Reduction Act Burden Statement
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.
(h) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Safety Management Section, Rotorcraft Standards
Branch, FAA, may approve AMOCs for this AD. Send your proposal to:
David Hatfield, Aviation Safety Engineer, Safety Management Section,
Rotorcraft Standards Branch, FAA, 10101 Hillwood Pkwy., Fort Worth,
TX 76177; telephone 817-222-5110; email [email protected].
(2) For operations conducted under a 14 CFR part 119 operating
certificate or sunder 14 CFR part 91, subpart K, the FAA suggests
that you notify your principal inspector, or lacking a principal
inspector, the manager of the local flight standards district office
or certificate holding district office, before operating any
aircraft complying with this AD through an AMOC.
(i) Additional Information
The subject of this AD is addressed in European Union Aviation
Safety Agency (EASA) Emergency AD No. 2019-0194-E, dated August 9,
2019. You may view the EASA AD on the Internet at https://www.regulations.gov by searching for and locating it in Docket No.
FAA-2019-1020.
(j) Subject
Joint Aircraft Service Component (JASC) Code: 6400, Tail Rotor
System.
(k) 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 the AD specifies otherwise.
(i) Leonardo Helicopters Emergency Alert Service Bulletin No.
119-100, dated August 7, 2019.
(ii) [Reserved]
(3) For Leonardo Helicopters 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://www.leonardocompany.com/en/home.
[[Page 37555]]
(4) You may view this service information at 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.
(5) You may view this service information that is incorporated
by reference at the National Archives and Records Administration
(NARA). For information on the availability of this material at
NARA, email [email protected], or go to: https://www.archives.gov/federal-register/cfr/ibr-locations.html.
Appendix 1 to AD 2020-13-02
Report the following information by email to
[email protected]. (Leonardo Helicopters Emergency
Alert Service Bulletin No. 119-100, dated August 7, 2019.)
(1) Date of Inspection:
(2) Helicopter Model and Serial Number:
(3) Total hours time-in-service (TIS) on the aircraft:
(4) Total hours TIS on the T/R duplex bearing:
(5) Total hours TIS since last overhaul of the T/R gearbox
assembly:
(6) Describe in detail any information and findings and, if
possible, provide photos.
Issued on June 10, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2020-13440 Filed 6-22-20; 8:45 am]
BILLING CODE 4910-13-P
