Airworthiness Directives; AlliedSignal Inc. and Rajay Inc. Oil Scavenge Pumps, 35260 [2015-14993]
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35260
Proposed Rules
Federal Register
Vol. 80, No. 118
Friday, June 19, 2015
This section of the FEDERAL REGISTER
contains notices to the public of the proposed
issuance of rules and regulations. The
purpose of these notices is to give interested
persons an opportunity to participate in the
rule making prior to the adoption of the final
rules.
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2015–0909; Directorate
Identifier 96–ANE–24–AD]
RIN 2120–AA64
Airworthiness Directives; AlliedSignal
Inc. and Rajay Inc. Oil Scavenge
Pumps
Federal Aviation
Administration (FAA), DOT.
ACTION: Proposed rule; withdrawal.
AGENCY:
The FAA is withdrawing a
notice of proposed rulemaking (NPRM).
The NPRM proposed a new
airworthiness directive (AD) that had
applied to AlliedSignal oil scavenge
pumps, part numbers (P/Ns) 101633–01
and –02 and Rajay Inc. oil scavenge
pumps, P/Ns 1025–1 and –2 installed on
Continental Motors, Inc. (CMI) IO–470
and TSIO–520 reciprocating engines
and on Lycoming Engines, Inc.,
(Lycoming) IO–360, IO–540, and O–360
reciprocating engines. We have found
no service difficulties with these model
oil scavenge pumps when installed on
the affected engines. Accordingly, we
withdraw the proposed rule.
DATES: As of June 19, 2015, the
proposed rule published February 20,
1997 at 62 FR 7730 is withdrawn.
FOR FURTHER INFORMATION CONTACT:
Richard McCauley, Aerospace Engineer,
Seattle Aircraft Certification Office,
FAA, Transport Directorate, 1601 Lind
Avenue SW., Renton, WA 98055–4056;
phone: 425–917–6502; fax: 425–917–
6590; email: richard.mccauley@faa.gov.
SUPPLEMENTARY INFORMATION: The FAA
proposed to amend 14 CFR part 39 with
a proposed AD (62 FR 7730, February
20, 1997). The proposed AD had applied
to AlliedSignal oil scavenge pumps,
P/Ns 101633–01 and –02 and Rajay Inc.
oil scavenge pumps, P/Ns 1025–1 and
–2 installed on CMI IO–470 and TSIO–
520 reciprocating engines and on
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SUMMARY:
VerDate Sep<11>2014
15:19 Jun 18, 2015
Jkt 235001
Lycoming IO–360, IO–540, and O–360
reciprocating engines. The NPRM
proposed to require initial and
repetitive inspections of the oil
scavenge pump for the security of the
snap ring installation, snap ring and
washer wear, and shaft groove wear, and
their replacement, if necessary, with
serviceable parts. The proposed action
was prompted by reports of severe wear
on the end plate of the oil scavenge
pump. The proposed actions were
intended to prevent oil scavenge pump
snap ring failure causing severe wear on
the pump end plate, which could result
in loss of engine oil and subsequent
engine shutdown.
Since we issued the NPRM (62 FR
7730, February 20, 1997), additional
information became available after the
public comment period closed on April
21, 1997.
Upon further consideration, we
hereby withdraw the proposed rule for
the following reason:
• We reviewed service difficulty
reports, AD databases, and airplane
manufacturer’s data and found no
unsafe condition in the last 19 years of
service history associated with these oil
scavenge pumps installed on the
affected engines.
Withdrawal of the NPRM (62 FR 7730,
February 20, 1997) constitutes only such
action, and does not preclude the
agency from issuing another notice in
the future, nor does it commit the
agency to any course of action in the
future.
Since this action only withdraws a
notice of proposed rulemaking, it is
neither a proposed nor a final rule.
Therefore, Executive Order 12866, the
Regulatory Flexibility Act, or DOT
Regulatory Policies and Procedures (44
FR 11034, February 26, 1979) do not
cover this withdrawal.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation
safety, Incorporation by reference,
Safety.
The Withdrawal
Accordingly, the notice of proposed
rulemaking, Docket No. FAA–2015–
0909; Directorate Identifier 96–ANE–
24–AD, published in the Federal
Register on February 20, 1997 (62 FR
7730), is withdrawn.
PO 00000
Frm 00001
Fmt 4702
Sfmt 4702
Issued in Burlington, Massachusetts, on
June 10, 2015.
Ann C. Mollica,
Acting Directorate Manager, Engine &
Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2015–14993 Filed 6–18–15; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2015–0486; Directorate
Identifier 2015–NE–07–AD]
RIN 2120–AA64
Airworthiness Directives; Pratt &
Whitney Canada Corp. Turboshaft
Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for certain
Pratt & Whitney Canada Corp. (P&WC)
PT6B–37A turboshaft engines. This
proposed AD was prompted by reports
of incorrect engine torque for PT6B–37A
engines. This proposed AD would
require initial and repetitive inspections
until replacement of the No. 10 bearing,
and eventual replacement of the No. 9
bearing, both located in the engine
reduction gearbox (RGB) assembly. We
are proposing this AD to prevent axial
migration of the No. 10 bearing in the
engine RGB assembly, which could lead
to engine overtorque, failure of the
engine, in-flight shutdown, and loss of
the rotorcraft.
DATES: We must receive comments on
this proposed AD by August 18, 2015.
ADDRESSES: You may send comments by
any of the following methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Mail: Docket Management Facility,
U.S. Department of Transportation, 1200
New Jersey Avenue SE., West Building
Ground Floor, Room W12–140,
Washington, DC 20590–0001.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
SUMMARY:
E:\FR\FM\19JNP1.SGM
19JNP1
Agencies
[Federal Register Volume 80, Number 118 (Friday, June 19, 2015)]
[Proposed Rules]
[Page 35260]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2015-14993]
========================================================================
Proposed Rules
Federal Register
________________________________________________________________________
This section of the FEDERAL REGISTER contains notices to the public of
the proposed issuance of rules and regulations. The purpose of these
notices is to give interested persons an opportunity to participate in
the rule making prior to the adoption of the final rules.
========================================================================
Federal Register / Vol. 80, No. 118 / Friday, June 19, 2015 /
Proposed Rules
[[Page 35260]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2015-0909; Directorate Identifier 96-ANE-24-AD]
RIN 2120-AA64
Airworthiness Directives; AlliedSignal Inc. and Rajay Inc. Oil
Scavenge Pumps
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Proposed rule; withdrawal.
-----------------------------------------------------------------------
SUMMARY: The FAA is withdrawing a notice of proposed rulemaking (NPRM).
The NPRM proposed a new airworthiness directive (AD) that had applied
to AlliedSignal oil scavenge pumps, part numbers (P/Ns) 101633-01 and -
02 and Rajay Inc. oil scavenge pumps, P/Ns 1025-1 and -2 installed on
Continental Motors, Inc. (CMI) IO-470 and TSIO-520 reciprocating
engines and on Lycoming Engines, Inc., (Lycoming) IO-360, IO-540, and
O-360 reciprocating engines. We have found no service difficulties with
these model oil scavenge pumps when installed on the affected engines.
Accordingly, we withdraw the proposed rule.
DATES: As of June 19, 2015, the proposed rule published February 20,
1997 at 62 FR 7730 is withdrawn.
FOR FURTHER INFORMATION CONTACT: Richard McCauley, Aerospace Engineer,
Seattle Aircraft Certification Office, FAA, Transport Directorate, 1601
Lind Avenue SW., Renton, WA 98055-4056; phone: 425-917-6502; fax: 425-
917-6590; email: richard.mccauley@faa.gov.
SUPPLEMENTARY INFORMATION: The FAA proposed to amend 14 CFR part 39
with a proposed AD (62 FR 7730, February 20, 1997). The proposed AD had
applied to AlliedSignal oil scavenge pumps, P/Ns 101633-01 and -02 and
Rajay Inc. oil scavenge pumps, P/Ns 1025-1 and -2 installed on CMI IO-
470 and TSIO-520 reciprocating engines and on Lycoming IO-360, IO-540,
and O-360 reciprocating engines. The NPRM proposed to require initial
and repetitive inspections of the oil scavenge pump for the security of
the snap ring installation, snap ring and washer wear, and shaft groove
wear, and their replacement, if necessary, with serviceable parts. The
proposed action was prompted by reports of severe wear on the end plate
of the oil scavenge pump. The proposed actions were intended to prevent
oil scavenge pump snap ring failure causing severe wear on the pump end
plate, which could result in loss of engine oil and subsequent engine
shutdown.
Since we issued the NPRM (62 FR 7730, February 20, 1997),
additional information became available after the public comment period
closed on April 21, 1997.
Upon further consideration, we hereby withdraw the proposed rule
for the following reason:
We reviewed service difficulty reports, AD databases, and
airplane manufacturer's data and found no unsafe condition in the last
19 years of service history associated with these oil scavenge pumps
installed on the affected engines.
Withdrawal of the NPRM (62 FR 7730, February 20, 1997) constitutes
only such action, and does not preclude the agency from issuing another
notice in the future, nor does it commit the agency to any course of
action in the future.
Since this action only withdraws a notice of proposed rulemaking,
it is neither a proposed nor a final rule. Therefore, Executive Order
12866, the Regulatory Flexibility Act, or DOT Regulatory Policies and
Procedures (44 FR 11034, February 26, 1979) do not cover this
withdrawal.
List of Subjects in 14 CFR Part 39
Air transportation, Aircraft, Aviation safety, Incorporation by
reference, Safety.
The Withdrawal
Accordingly, the notice of proposed rulemaking, Docket No. FAA-
2015-0909; Directorate Identifier 96-ANE-24-AD, published in the
Federal Register on February 20, 1997 (62 FR 7730), is withdrawn.
Issued in Burlington, Massachusetts, on June 10, 2015.
Ann C. Mollica,
Acting Directorate Manager, Engine & Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2015-14993 Filed 6-18-15; 8:45 am]
BILLING CODE 4910-13-P