Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop Engines, 9387-9389 [2023-03069]
Download as PDF
9387
Rules and Regulations
Federal Register
Vol. 88, No. 30
Tuesday, February 14, 2023
This section of the FEDERAL REGISTER
contains regulatory documents having general
applicability and legal effect, most of which
are keyed to and codified in the Code of
Federal Regulations, which is published under
50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by
the Superintendent of Documents.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2022–1477; Project
Identifier MCAI–2022–00632–E; Amendment
39–22327; AD 2023–03–02]
RIN 2120–AA64
Airworthiness Directives; Pratt &
Whitney Canada Corp. Turboprop
Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
The FAA is adopting a new
airworthiness directive (AD) for certain
Pratt & Whitney Canada Corp. (P&WC)
PT6E–67XP model turboprop engines
with serial number HP0194 and earlier.
This AD is prompted by multiple
reports of engines failing to achieve
required power (torque) during high
power applications due to internal leaks
in the bleed-off valves (BOVs). This AD
requires replacement of the compressor
BOV assembly, replacement of the BOV
orifice feed air tube assembly, and
installation of a redesigned P3 probe
snorkel, as specified in a Transport
Canada AD, which is incorporated by
reference (IBR). The FAA is issuing this
AD to address the unsafe condition on
these products.
DATES: This AD is effective March 21,
2023.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in this AD
as of March 21, 2023.
ADDRESSES:
AD Docket: You may examine the AD
docket at regulations.gov under Docket
No. FAA–2022–1477; or in person at
Docket Operations between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. The AD docket
contains this final rule, the mandatory
ddrumheller on DSK120RN23PROD with RULES
SUMMARY:
VerDate Sep<11>2014
16:49 Feb 13, 2023
Jkt 259001
continuing airworthiness information
(MCAI), any comments received, and
other information. The address for
Docket Operations is U.S. Department of
Transportation, Docket Operations, M–
30, West Building Ground Floor, Room
W12–140, 1200 New Jersey Avenue SE,
Washington, DC 20590.
Material Incorporated by Reference:
• For material that is IBR in this final
rule, contact Transport Canada,
Transport Canada National Aircraft
Certification, 159 Cleopatra Drive,
Nepean, Ontario K1A 0N5, Canada;
phone: (888) 663–3639; email: AD-CN@
tc.gc.ca; website: tc.canada.ca/en/
aviation.
• You may view this service
information at the FAA, Airworthiness
Products Section, Operational Safety
Branch, 1200 District Avenue,
Burlington, MA 01803. For information
on the availability of this material at the
FAA, call (817) 222–5110. It is also
available at regulations.gov under
Docket No. FAA–2022–1477.
FOR FURTHER INFORMATION CONTACT:
Barbara Caufield, Aviation Safety
Engineer, ECO Branch, FAA, 1200
District Avenue, Burlington, MA 01803;
phone: (781) 238–7146; email:
barbara.caufield@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 by adding an AD that would
apply to certain P&WC PT6E–67XP
model turboprop engines with serial
number HP0194 and earlier. The NPRM
published in the Federal Register on
November 18, 2022 (87 FR 69218). The
NPRM was prompted by Transport
Canada AD CF–2022–26–E, dated May
12, 2022 (Transport Canada AD CF–
2022–26–E) (referred to after this as the
MCAI). The MCAI states that there have
been reports of multiple incidents in
which engines were unable to achieve
the required power (torque) during high
power applications. A manufacturer
investigation found that contamination
from the glass beads used in the
manufacturing process during the gas
generator casing (GGC) production
caused internal leaks in the BOVs,
preventing the BOVs from fully closing
at high power settings.
In the NPRM, the FAA proposed to
require replacement of the compressor
PO 00000
Frm 00001
Fmt 4700
Sfmt 4700
BOV assembly, replacement of the BOV
orifice feed air tube assembly, and
installation of a redesigned P3 probe
snorkel, as specified in Transport
Canada AD CF–2022–26. The FAA is
issuing this AD to address the unsafe
condition on these products.
You may examine the MCAI in the
AD docket at regulations.gov under
Docket No. FAA–2022–1477.
Discussion of Final Airworthiness
Directive
Comments
The FAA received no comments on
the NPRM or on the determination of
the cost to the public.
Conclusion
This product has been approved by
the aviation authority of another
country and is approved for operation in
the United States. Pursuant to the FAA’s
bilateral agreement with this State of
Design Authority, it has notified the
FAA of the unsafe condition described
in the MCAI referenced above. The FAA
reviewed the relevant data and
determined that air safety requires
adopting this AD as proposed.
Accordingly, the FAA is issuing this AD
to address the unsafe condition on this
product. Except for minor editorial
changes, this AD is adopted as proposed
in the NPRM. None of the changes will
increase the economic burden on any
operator.
Related Service Information Under 1
CFR Part 51
The FAA reviewed Transport Canada
AD CF–2022–26, which specifies
procedures for the replacement of the
compressor BOV assembly, replacement
of the BOV orifice feed air tube
assembly, and installation of a
redesigned P3 probe snorkel.
This material is reasonably available
because the interested parties have
access to it through their normal course
of business or by the means identified
in ADDRESSES.
Costs of Compliance
The FAA estimates that this AD
affects 100 engines installed on
airplanes of U.S. registry.
The FAA estimates the following
costs to comply with this AD:
E:\FR\FM\14FER1.SGM
14FER1
9388
Federal Register / Vol. 88, No. 30 / Tuesday, February 14, 2023 / Rules and Regulations
ESTIMATED COSTS
Action
Labor cost
Replace compressor BOV assembly ......................................
Replace BOV orifice feed air tube assembly with P3 probe
snorkel and BOV orifice feed air tube assembly.
Authority for This Rulemaking
Title 49 of the United States Code
specifies the FAA’s authority to issue
rules on aviation safety. Subtitle I,
section 106, describes the authority of
the FAA Administrator. Subtitle VII:
Aviation Programs, describes in more
detail the scope of the Agency’s
authority.
The FAA is issuing this rulemaking
under the authority described in
Subtitle VII, Part A, Subpart III, Section
44701: General requirements. Under
that section, Congress charges the FAA
with promoting safe flight of civil
aircraft in air commerce by prescribing
regulations for practices, methods, and
procedures the Administrator finds
necessary for safety in air commerce.
This regulation is within the scope of
that authority because it addresses an
unsafe condition that is likely to exist or
develop on products identified in this
rulemaking action.
Regulatory Findings
This AD will not have federalism
implications under Executive Order
13132. This AD will not have a
substantial direct effect on the States, on
the relationship between the national
government and the States, or on the
distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify that this AD:
(1) Is not a ‘‘significant regulatory
action’’ under Executive Order 12866,
(2) Will not affect intrastate aviation
in Alaska, and
(3) Will not have a significant
economic impact, positive or negative,
on a substantial number of small entities
under the criteria of the Regulatory
Flexibility Act.
ddrumheller on DSK120RN23PROD with RULES
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:
VerDate Sep<11>2014
16:49 Feb 13, 2023
Jkt 259001
Parts cost
5 work-hours × $85 per hour
= $425.
6 work-hours × $85 per hour
= $510.
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:
■
2023–03–02 Pratt & Whitney Canada Corp.:
Amendment 39–22327; Docket No.
FAA–2022–1477; Project Identifier
MCAI–2022–00632–E.
(a) Effective Date
This airworthiness directive (AD) is
effective March 21, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Pratt & Whitney Canada
Corp. (P&WC) PT6E–67XP model turboprop
engines with serial number HP0194 and
earlier, as identified in Transport Canada AD
CF–2022–26, dated May 12, 2022 (Transport
Canada AD CF–2022–26).
(d) Subject
Joint Aircraft Service Component (JASC)
Code 7230, Turbine Engine Compressor
Section.
(e) Unsafe Condition
This AD was prompted by reports of
multiple incidents in which engines were
unable to achieve the required power (torque)
during high power applications due to
internal leaks in the bleed-off valves (BOVs)
caused by glass bead contamination. The
FAA is issuing this AD to prevent internal
leaks in the BOVs, and to prevent the failure
of the engine to achieve the required power
(torque) during high power applications. The
unsafe condition, if not addressed, could
result in loss of thrust control and loss of the
airplane.
(f) Compliance
Comply with this AD within the
compliance times specified, unless already
done.
(g) Required Actions
Except as specified in paragraphs (h) and
(i) of this AD: Perform all required actions
within the compliance times specified in,
and in accordance with, Transport Canada
AD CF–2022–26.
PO 00000
Frm 00002
Fmt 4700
Sfmt 4700
Cost per
product
Cost on U.S.
operators
$13,102
$13,527
$1,352,700
22,000
22,510
2,251,000
(h) Exceptions to Transport Canada AD CF–
2022–26
(1) Where Transport Canada AD CF–2022–
26 refers to hours air time, this AD requires
using flight hours.
(2) Where Transport Canada AD CF–2022–
26 specifies compliance from its effective
date, this AD requires using the effective date
of this AD.
(i) No Reporting Requirement
Although the service information
referenced in Transport Canada AD CF–
2022–26 specifies to submit certain
information to the manufacturer, this AD
does not include that requirement.
(j) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, ECO Branch, FAA, has
the authority to approve AMOCs for this AD,
if requested using the procedures found in
§ 39.19. In accordance with § 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,
send it to the attention of the person
identified in paragraph (k) of this AD or
email to: ANE-AD-AMOC@faa.gov.
(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.
(k) Additional Information
For more information about this AD,
contact Barbara Caufield, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District
Avenue, Burlington, MA 01803; phone: (781)
238–7146; email: barbara.caufield@faa.gov.
(l) 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) Transport Canada AD CF–2022–26,
dated May 12, 2022.
(ii) [Reserved]
(3) For Transport Canada AD CF–2022–26–
E, contact Transport Canada, Transport
Canada National Aircraft Certification, 159
Cleopatra Drive, Nepean, Ontario K1A 0N5,
Canada; phone: (888) 663–3639; email: ADCN@tc.gc.ca; website: tc.canada.ca/en/
aviation.
(4) You may view this service information
at the FAA, Airworthiness Products Section,
Operational Safety Branch, 1200 District
E:\FR\FM\14FER1.SGM
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Federal Register / Vol. 88, No. 30 / Tuesday, February 14, 2023 / Rules and Regulations
Avenue, Burlington, MA 01803. 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: fr.inspection@nara.gov, or go to:
www.archives.gov/federal-register/cfr/ibrlocations.html.
Issued on February 1, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2023–03069 Filed 2–13–23; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF COMMERCE
Bureau of Industry and Security
15 CFR Part 744
[Docket No. 230209–0041]
RIN 0694–AJ14
Additions to the Entity List
Bureau of Industry and
Security, Department of Commerce.
ACTION: Final rule.
AGENCY:
Entity List Decisions
In this rule, the Bureau of
Industry and Security (BIS) amends the
Export Administration Regulations
(EAR) by adding six entities to the
Entity List, under the destination of the
People’s Republic of China (China).
These six entities have been determined
by the U.S. Government to be acting
contrary to the national security or
foreign policy interests of the United
States.
SUMMARY:
This rule is effective on February
10, 2023.
FOR FURTHER INFORMATION CONTACT:
Chair, End-User Review Committee,
Office of the Assistant Secretary for
Export Administration, Bureau of
Industry and Security, Department of
Commerce, Phone: (202) 482–5991,
Email: ERC@bis.doc.gov.
SUPPLEMENTARY INFORMATION:
DATES:
ddrumheller on DSK120RN23PROD with RULES
Background
The Entity List (supplement no. 4 to
part 744 of the EAR (15 CFR parts 730–
774)) identifies entities for which there
is reasonable cause to believe, based on
specific and articulable facts, that the
entities have been involved, are
involved, or pose a significant risk of
being or becoming involved in activities
contrary to the national security or
foreign policy interests of the United
States, pursuant to § 744.11(b). The EAR
impose additional license requirements
VerDate Sep<11>2014
16:49 Feb 13, 2023
Jkt 259001
on, and limit the availability of, most
license exceptions for exports,
reexports, and transfers (in-country)
when a listed entity is a party to the
transaction. The license review policy
for each listed entity is identified in the
‘‘License Review Policy’’ column on the
Entity List, and the impact on the
availability of license exceptions is
described in the relevant Federal
Register document that added the entity
to the Entity List. The Bureau of
Industry and Security (BIS) places
entities on the Entity List pursuant to
part 744 (Control Policy: End-User and
End-Use Based) and part 746
(Embargoes and Other Special Controls)
of the EAR.
The End-User Review Committee
(ERC), composed of representatives of
the Departments of Commerce (Chair),
State, Defense, Energy and, where
appropriate, the Treasury, makes all
decisions regarding additions to,
removals from, or other modifications to
the Entity List. The ERC makes all
decisions to add an entry to the Entity
List by majority vote and makes all
decisions to remove or modify an entry
by unanimous vote.
A. Additions to the Entity List
The ERC determined to add Beijing
Nanjiang Aerospace Technology Co.,
Ltd.; China Electronics Technology
Group Corporation 48th Research
Institute; Dongguan Lingkong Remote
Sensing Technology Co., Ltd.; Eagles
Men Aviation Science and Technology
Group Co., Ltd. (EMAST); Guangzhou
Tian-Hai-Xiang Aviation Technology
Co., Ltd.; and Shanxi Eagles Men
Aviation Science and Technology Group
Co., Ltd. all under the destination of
China, to the Entity List. These entities
are being added for their support to
China’s military modernization efforts,
specifically the People’s Liberation
Army’s (PLA) aerospace programs
including airships and balloons and
related materials and components. The
PLA is utilizing High Altitude Balloons
(HAB) for intelligence and
reconnaissance activities. This activity
is contrary to U.S. national security and
foreign policy interests under § 744.11
of the EAR. For these six entities, BIS
imposes a license requirement for all
items subject to the EAR and will
review license applications under a
presumption of denial.
For the reasons described above, this
final rule adds the following six entities
to the Entity List and includes, where
appropriate, aliases:
PO 00000
Frm 00003
Fmt 4700
Sfmt 4700
9389
China
• Beijing Nanjiang Aerospace
Technology Co., Ltd.;
• China Electronics Technology
Group Corporation 48th Research
Institute;
• Dongguan Lingkong Remote
Sensing Technology Co., Ltd.;
• Eagles Men Aviation Science and
Technology Group Co., Ltd. (EMAST);
• Guangzhou Tian-Hai-Xiang
Aviation Technology Co., Ltd.; and
• Shanxi Eagles Men Aviation
Science and Technology Group Co., Ltd.
Savings Clause
For the changes being made in this
final rule, shipments of items removed
from eligibility for a License Exception
or export, reexport, or transfer (incountry) without a license (NLR) as a
result of this regulatory action that were
en route aboard a carrier to a port of
export, reexport, or transfer (in-country),
on February 10, 2023, pursuant to actual
orders for export, reexport, or transfer
(in-country) to or within a foreign
destination, may proceed to that
destination under the previous
eligibility for a License Exception or
export, reexport, or transfer (in-country)
without a license (NLR) before March
13, 2023. Any such items not actually
exported, reexported or transferred (incountry) before midnight, on March 13,
2023, require a license in accordance
with this final rule.
Export Control Reform Act of 2018
On August 13, 2018, the President
signed into law the John S. McCain
National Defense Authorization Act for
Fiscal Year 2019, which included the
Export Control Reform Act of 2018
(ECRA) (50 U.S.C. 4801–4852). ECRA
provides the legal basis for BIS’s
principal authorities and serves as the
authority under which BIS issues this
rule.
Rulemaking Requirements
1. This rule has been determined to be
not significant for purposes of Executive
Order 12866.
2. Notwithstanding any other
provision of law, no person is required
to respond to or be subject to a penalty
for failure to comply with a collection
of information, subject to the
requirements of the Paperwork
Reduction Act of 1995 (44 U.S.C. 3501
et seq.) (PRA), unless that collection of
information displays a currently valid
Office of Management and Budget
(OMB) Control Number. This regulation
involves an information collection
approved by OMB under control
number 0694–0088, Simplified Network
Application Processing System. BIS
E:\FR\FM\14FER1.SGM
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Agencies
[Federal Register Volume 88, Number 30 (Tuesday, February 14, 2023)]
[Rules and Regulations]
[Pages 9387-9389]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2023-03069]
========================================================================
Rules and Regulations
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains regulatory documents
having general applicability and legal effect, most of which are keyed
to and codified in the Code of Federal Regulations, which is published
under 50 titles pursuant to 44 U.S.C. 1510.
The Code of Federal Regulations is sold by the Superintendent of Documents.
========================================================================
Federal Register / Vol. 88 , No. 30 / Tuesday, February 14, 2023 /
Rules and Regulations
[[Page 9387]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2022-1477; Project Identifier MCAI-2022-00632-E;
Amendment 39-22327; AD 2023-03-02]
RIN 2120-AA64
Airworthiness Directives; Pratt & Whitney Canada Corp. Turboprop
Engines
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule.
-----------------------------------------------------------------------
SUMMARY: The FAA is adopting a new airworthiness directive (AD) for
certain Pratt & Whitney Canada Corp. (P&WC) PT6E-67XP model turboprop
engines with serial number HP0194 and earlier. This AD is prompted by
multiple reports of engines failing to achieve required power (torque)
during high power applications due to internal leaks in the bleed-off
valves (BOVs). This AD requires replacement of the compressor BOV
assembly, replacement of the BOV orifice feed air tube assembly, and
installation of a redesigned P3 probe snorkel, as specified in a
Transport Canada AD, which is incorporated by reference (IBR). The FAA
is issuing this AD to address the unsafe condition on these products.
DATES: This AD is effective March 21, 2023.
The Director of the Federal Register approved the incorporation by
reference of a certain publication listed in this AD as of March 21,
2023.
ADDRESSES:
AD Docket: You may examine the AD docket at regulations.gov under
Docket No. FAA-2022-1477; or in person at Docket Operations between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays. The AD
docket contains this final rule, the mandatory continuing airworthiness
information (MCAI), any comments received, and other information. The
address for Docket Operations is U.S. Department of Transportation,
Docket Operations, M-30, West Building Ground Floor, Room W12-140, 1200
New Jersey Avenue SE, Washington, DC 20590.
Material Incorporated by Reference:
For material that is IBR in this final rule, contact
Transport Canada, Transport Canada National Aircraft Certification, 159
Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; phone: (888) 663-
3639; email: [email protected]; website: tc.canada.ca/en/aviation.
You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District Avenue, Burlington, MA 01803. For information on the
availability of this material at the FAA, call (817) 222-5110. It is
also available at regulations.gov under Docket No. FAA-2022-1477.
FOR FURTHER INFORMATION CONTACT: Barbara Caufield, Aviation Safety
Engineer, ECO Branch, FAA, 1200 District Avenue, Burlington, MA 01803;
phone: (781) 238-7146; email: [email protected].
SUPPLEMENTARY INFORMATION:
Background
The FAA issued a notice of proposed rulemaking (NPRM) to amend 14
CFR part 39 by adding an AD that would apply to certain P&WC PT6E-67XP
model turboprop engines with serial number HP0194 and earlier. The NPRM
published in the Federal Register on November 18, 2022 (87 FR 69218).
The NPRM was prompted by Transport Canada AD CF-2022-26-E, dated May
12, 2022 (Transport Canada AD CF-2022-26-E) (referred to after this as
the MCAI). The MCAI states that there have been reports of multiple
incidents in which engines were unable to achieve the required power
(torque) during high power applications. A manufacturer investigation
found that contamination from the glass beads used in the manufacturing
process during the gas generator casing (GGC) production caused
internal leaks in the BOVs, preventing the BOVs from fully closing at
high power settings.
In the NPRM, the FAA proposed to require replacement of the
compressor BOV assembly, replacement of the BOV orifice feed air tube
assembly, and installation of a redesigned P3 probe snorkel, as
specified in Transport Canada AD CF-2022-26. The FAA is issuing this AD
to address the unsafe condition on these products.
You may examine the MCAI in the AD docket at regulations.gov under
Docket No. FAA-2022-1477.
Discussion of Final Airworthiness Directive
Comments
The FAA received no comments on the NPRM or on the determination of
the cost to the public.
Conclusion
This product has been approved by the aviation authority of another
country and is approved for operation in the United States. Pursuant to
the FAA's bilateral agreement with this State of Design Authority, it
has notified the FAA of the unsafe condition described in the MCAI
referenced above. The FAA reviewed the relevant data and determined
that air safety requires adopting this AD as proposed. Accordingly, the
FAA is issuing this AD to address the unsafe condition on this product.
Except for minor editorial changes, this AD is adopted as proposed in
the NPRM. None of the changes will increase the economic burden on any
operator.
Related Service Information Under 1 CFR Part 51
The FAA reviewed Transport Canada AD CF-2022-26, which specifies
procedures for the replacement of the compressor BOV assembly,
replacement of the BOV orifice feed air tube assembly, and installation
of a redesigned P3 probe snorkel.
This material is reasonably available because the interested
parties have access to it through their normal course of business or by
the means identified in ADDRESSES.
Costs of Compliance
The FAA estimates that this AD affects 100 engines installed on
airplanes of U.S. registry.
The FAA estimates the following costs to comply with this AD:
[[Page 9388]]
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost per Cost on U.S.
Action Labor cost Parts cost product operators
----------------------------------------------------------------------------------------------------------------
Replace compressor BOV assembly....... 5 work-hours x $85 per $13,102 $13,527 $1,352,700
hour = $425.
Replace BOV orifice feed air tube 6 work-hours x $85 per 22,000 22,510 2,251,000
assembly with P3 probe snorkel and hour = $510.
BOV orifice feed air tube assembly.
----------------------------------------------------------------------------------------------------------------
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, Section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
This AD will not have federalism implications under Executive Order
13132. This AD will not have a substantial direct effect on the States,
on the relationship between the national government and the States, or
on the distribution of power and responsibilities among the various
levels of government.
For the reasons discussed above, I certify that this AD:
(1) Is not a ``significant regulatory action'' under Executive
Order 12866,
(2) Will not affect intrastate aviation in Alaska, and
(3) Will not have a significant economic impact, positive or
negative, on a substantial number of small entities under the criteria
of the Regulatory Flexibility Act.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA amends 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
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:
2023-03-02 Pratt & Whitney Canada Corp.: Amendment 39-22327; Docket
No. FAA-2022-1477; Project Identifier MCAI-2022-00632-E.
(a) Effective Date
This airworthiness directive (AD) is effective March 21, 2023.
(b) Affected ADs
None.
(c) Applicability
This AD applies to Pratt & Whitney Canada Corp. (P&WC) PT6E-67XP
model turboprop engines with serial number HP0194 and earlier, as
identified in Transport Canada AD CF-2022-26, dated May 12, 2022
(Transport Canada AD CF-2022-26).
(d) Subject
Joint Aircraft Service Component (JASC) Code 7230, Turbine
Engine Compressor Section.
(e) Unsafe Condition
This AD was prompted by reports of multiple incidents in which
engines were unable to achieve the required power (torque) during
high power applications due to internal leaks in the bleed-off
valves (BOVs) caused by glass bead contamination. The FAA is issuing
this AD to prevent internal leaks in the BOVs, and to prevent the
failure of the engine to achieve the required power (torque) during
high power applications. The unsafe condition, if not addressed,
could result in loss of thrust control and loss of the airplane.
(f) Compliance
Comply with this AD within the compliance times specified,
unless already done.
(g) Required Actions
Except as specified in paragraphs (h) and (i) of this AD:
Perform all required actions within the compliance times specified
in, and in accordance with, Transport Canada AD CF-2022-26.
(h) Exceptions to Transport Canada AD CF-2022-26
(1) Where Transport Canada AD CF-2022-26 refers to hours air
time, this AD requires using flight hours.
(2) Where Transport Canada AD CF-2022-26 specifies compliance
from its effective date, this AD requires using the effective date
of this AD.
(i) No Reporting Requirement
Although the service information referenced in Transport Canada
AD CF-2022-26 specifies to submit certain information to the
manufacturer, this AD does not include that requirement.
(j) Alternative Methods of Compliance (AMOCs)
(1) The Manager, ECO Branch, FAA, has the authority to approve
AMOCs for this AD, if requested using the procedures found in Sec.
39.19. In accordance with Sec. 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, send it to the attention of the person
identified in paragraph (k) of this AD or email 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.
(k) Additional Information
For more information about this AD, contact Barbara Caufield,
Aviation Safety Engineer, ECO Branch, FAA, 1200 District Avenue,
Burlington, MA 01803; phone: (781) 238-7146; email:
[email protected].
(l) 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) Transport Canada AD CF-2022-26, dated May 12, 2022.
(ii) [Reserved]
(3) For Transport Canada AD CF-2022-26-E, contact Transport
Canada, Transport Canada National Aircraft Certification, 159
Cleopatra Drive, Nepean, Ontario K1A 0N5, Canada; phone: (888) 663-
3639; email: [email protected]; website: tc.canada.ca/en/aviation.
(4) You may view this service information at the FAA,
Airworthiness Products Section, Operational Safety Branch, 1200
District
[[Page 9389]]
Avenue, Burlington, MA 01803. 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: www.archives.gov/federal-register/cfr/ibr-locations.html.
Issued on February 1, 2023.
Christina Underwood,
Acting Director, Compliance & Airworthiness Division, Aircraft
Certification Service.
[FR Doc. 2023-03069 Filed 2-13-23; 8:45 am]
BILLING CODE 4910-13-P