Airworthiness Directives; McCauley Propeller Systems Governors, 19399-19401 [2020-07168]
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19399
Proposed Rules
Federal Register
Vol. 85, No. 67
Tuesday, April 7, 2020
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
Examining the AD Docket
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2020–0320; Product
Identifier 2019–CE–011–AD]
RIN 2120–AA64
Airworthiness Directives; McCauley
Propeller Systems Governors
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
The FAA proposes to adopt a
new airworthiness directive (AD) for
certain model McCauley Propeller
Systems (McCauley) governors installed
on airplanes. This proposed AD was
prompted by reports of an unapproved
variant McCauley idler gear bearing,
part number (P/N) A–20028, that could
be installed in the affected governors.
This proposed AD would require
replacing the governor with a governor
that is eligible for installation. The FAA
is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments
on this proposed AD by May 22, 2020.
ADDRESSES: You may send comments,
using the procedures found in 14 CFR
11.43 and 11.45, by any of the following
methods:
• Federal eRulemaking Portal: Go to
https://www.regulations.gov. Follow the
instructions for submitting comments.
• Fax: 202–493–2251.
• Mail: U.S. Department of
Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue SE, Washington, DC 20590.
• Hand Delivery: Deliver to Mail
address above between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
For service information identified in
this NPRM, contact McCauley Propeller
Systems, One Cessna Boulevard, P.O.
Box 7704, Wichita, Kansas 67277;
khammond on DSKJM1Z7X2PROD with PROPOSALS
SUMMARY:
VerDate Sep<11>2014
17:06 Apr 06, 2020
Jkt 250001
telephone: (800) 621–7767 or (316) 831–
4021; email: productsupport@txtav.com;
internet: https://mccauley.txtav.com.
You may view this service information
at the FAA, Policy and Innovation
Division, 901 Locust, Kansas City,
Missouri 64106. For information on the
availability of this material at the FAA,
call (816) 329–4148.
You may examine the AD docket on
the internet at https://
www.regulations.gov by searching for
and locating Docket No. FAA–2020–
0320 or in person at Docket Operations
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
The AD docket contains this NPRM, the
regulatory evaluation, 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 FURTHER INFORMATION CONTACT:
Thomas Teplik, Aerospace Engineer,
Wichita ACO Branch, 1801 Airport
Road, Room 100, Wichita, Kansas
67209; telephone: (316) 946–4196; fax:
(316) 946–4107; email: thomas.teplik@
faa.gov or Wichita-COS@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any
written relevant data, views, or
arguments about this proposal. Send
your comments to an address listed
under the ADDRESSES section. Include
‘‘Docket No. FAA–2020–0320; Product
Identifier 2019–CE–011–AD’’ at the
beginning of your comments. The FAA
specifically invites comments on the
overall regulatory, economic,
environmental, and energy aspects of
this NPRM. The FAA will consider all
comments received by the closing date
and may amend this NPRM because of
those comments.
The FAA will post all comments
received, without change, to https://
www.regulations.gov, including any
personal information you provide. The
FAA will also post a report
summarizing each substantive verbal
contact received about this NPRM.
Discussion
The FAA has received reports from
McCauley that an unapproved variant
idler gear bearing, part number (P/N) A–
PO 00000
Frm 00001
Fmt 4702
Sfmt 4702
20028, was installed on certain
governors during production between
January 31, 2017, and September 27,
2018, and may have been installed on
governors in service after January 31,
2017. The unapproved variant of the
idler gear bearing does not conform to
McCauley drawing requirements.
All models of McCauley governors
have an idler gear bearing with P/N A–
20028 installed; however, the
unapproved variant of the bearing can
be identified by part marking ‘‘BA–59.’’
The non-conforming idler gear bearing
could have also been included in the
idler gear assembly (idler gear and
bearing), P/N A–20107, or the governor
overhaul kit, P/N PL–20233 or PL–
20234.
The non-conformity of the bearing
may cause premature failure of the idler
gear bearing. Early symptoms that the
idler gear bearing may fail include
inability of the governor to hold the
selected RPM, hunting, surging, etc. An
investigation identified 23 occurrences
of airplane operation problems related
to erratic governor behavior that may
have resulted from the unapproved idler
gear bearing.
This condition, if not addressed,
could cause the idler gear bearing to fail.
This failure could result in failure of the
governor, loss of propeller pitch control,
engine and propeller over speed, engine
oil contamination, and loss of control.
Related Service Information Under 1
CFR Part 51
The FAA reviewed McCauley Alert
Service Bulletin ASB273C, dated
January 30, 2019. The service bulletin
contains model and serial number
information to identify the affected
governors. The service bulletin also
contains procedures for removing the
governor from the engine, inspecting the
governor for the unapproved variant
idler gear bearing, replacing the idler
gear bearing or idler gear assembly if
necessary, overhauling the governor if
necessary, and installing a governor on
the engine. 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.
FAA’s Determination
The FAA is proposing this AD
because it evaluated all relevant
information and determined the unsafe
E:\FR\FM\07APP1.SGM
07APP1
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Federal Register / Vol. 85, No. 67 / Tuesday, April 7, 2020 / Proposed Rules
condition described previously is likely
to exist or develop in other products of
the same type design.
Proposed AD Requirements
This proposed AD would require
replacing an affected governor with a
governor eligible for installation.
Differences Between This Proposed AD
and the Service Information
The service bulletin contains
maintenance procedures for inspecting
an affected governor and any
subsequent corrective actions required
to ensure the governor is eligible for
continued service and installation. The
service bulletin also references other
McCauley service documents for
additional maintenance actions to
include overhaul of the governor.
However, this NPRM only proposes
replacing the affected governor with a
governor eligible for installation.
Costs of Compliance
The FAA estimates that this proposed
AD affects 2,500 governors as installed
in airplanes of U.S. registry.
The FAA estimates the following
costs to comply with this proposed AD:
ESTIMATED COSTS
Action
Labor cost
Parts cost
Remove affected governor ..
Install an governor ...............
1 work-hour × $85 per hour = $85 ..................
1 work-hour × $85 per hour = $85 ..................
Not Applicable ............
See table below ..........
An operator has the option to pay a
service center to inspect their existing
governor and replace the idler gear
bearing if necessary or pay to have their
existing governor overhauled. An
operator has the option to purchase a
factory new governor or an overhauled
governor, a feathering/syncing governor
or a non-feathering/syncing governor.
The FAA has no way of knowing what
option an operator may take to obtain a
governor eligible for installation.
Cost per product
Cost on U.S.
operators
$85
Variable
$212,500
Unknown
Therefore, the FAA has no way of
determining the parts cost on U.S.
operators. The following represents the
estimated parts cost associated with
obtaining a governor.
COST FOR AN ELIGIBLE GOVERNOR
Type of governor
Cost of governor
Factory new non-feathering/non-syncing governor .......................................................................................................................
Factory new feathering/syncing governor .....................................................................................................................................
Overhaul of existing non-feathering/non-syncing governor ...........................................................................................................
Overhaul of existing feathering/syncing governor .........................................................................................................................
According to the manufacturer, some
of the costs of this proposed AD may be
covered under warranty, thereby
reducing the cost impact on affected
individuals. The FAA does not control
warranty coverage for affected
individuals. As a result, the FAA has
included all costs in our cost estimate.
khammond on DSKJM1Z7X2PROD with PROPOSALS
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
VerDate Sep<11>2014
17:06 Apr 06, 2020
Jkt 250001
develop on products identified in this
rulemaking action.
Regulatory Findings
The FAA determined that this
proposed AD would not have federalism
implications under Executive Order
13132. This proposed AD would not
have a substantial direct effect on the
States, on the relationship between the
national government and the States, or
on the distribution of power and
responsibilities among the various
levels of government.
For the reasons discussed above, I
certify this proposed regulation:
(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.
PO 00000
Frm 00002
Fmt 4702
Sfmt 4702
$2,000
9,000
1,000
3,000
The Proposed Amendment
Accordingly, under the authority
delegated to me by the Administrator,
the FAA proposes to amend 14 CFR part
39 as follows:
PART 39—AIRWORTHINESS
DIRECTIVES
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):
■
McCauley Propeller Systems: Docket No.
FAA–2020–0320; Product Identifier
2019–CE–011–AD.
(a) Comments Due Date
The FAA must receive comments by May
22, 2020.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the McCauley Propeller
Systems (McCauley) governors specified in
paragraphs (c)(1) or (2) of this AD and
E:\FR\FM\07APP1.SGM
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Federal Register / Vol. 85, No. 67 / Tuesday, April 7, 2020 / Proposed Rules
installed on airplanes, certificated in any
category.
(1) Models listed in table 2 of McCauley
Alert Service Bulletin No. ASB273C, dated
January 30, 2019 (McCauley ASB273C) with
a serial number from 170061 through 180501,
excluding the serial numbers listed in table
1 of McCauley ASB273C.
(2) Models listed in table 2 of McCauley
ASB273C, with any serial number, that have
an installation date after January 31, 2017, or
an installation date that cannot be
determined.
(d) Subject
Joint Aircraft System Component (JASC)/
Air Transport Association (ATA) of America
Code 61, Propellers.
(e) Unsafe Condition
This AD was prompted by reports of an
unapproved variant idler gear bearing,
McCauley part number (P/N) A–20028,
installed on governors. All models of
McCauley governors have a bearing with
P/N A–20028 installed; however, the
unapproved variant can be identified with
the part marking ‘‘BA–59.’’ The FAA is
issuing this AD to prevent failure of the idler
gear bearing. This failure could result in
failure of the governor, loss of propeller pitch
control, engine and propeller over speed,
engine oil contamination, and loss of control
of the airplane.
(f) Compliance
Unless already done, within 50 hours timein-service after the effective date of this AD
or within 24 months after the effective date
of this AD, whichever occurs first, replace
the governor with a governor eligible for
installation.
Note 1 to paragraph (f) of this AD: Any
model McCauley governor that is stamped
with the letter B, as specified in the
Accomplishment Instructions in McCauley
ASB273C, has already complied with the
requirements of this AD.
(g) Definition
For the purposes of this AD, a governor
eligible for installation is defined as a
governor that does not have an idler gear
bearing with a part marking ‘‘BA–59’’
installed.
khammond on DSKJM1Z7X2PROD with PROPOSALS
(i) Alternative Methods of Compliance
(AMOCs)
(1) The Manager, Wichita ACO Branch,
FAA, has the authority to approve AMOCs
for this AD, if requested using the procedures
found in 14 CFR 39.19. In accordance with
14 CFR 39.19, send your request to your
principal inspector or local Flight Standards
District Office, as appropriate. If sending
information directly to the manager of the
certification office, send it to the attention of
the person identified in paragraph (l)(1) of
this AD.
(2) Before using any approved AMOC,
notify your appropriate principal inspector,
17:06 Apr 06, 2020
Jkt 250001
(j) Related Information
(1) For more information about this AD,
contact Thomas Teplik, Aerospace Engineer,
Wichita ACO Branch, 1801 Airport Road,
Room 100, Wichita, Kansas 67209; telephone:
(316) 946–4196; fax: (316) 946–4107; email:
thomas.teplik@faa.gov or Wichita-COS@
faa.gov.
(2) For service information identified in
this AD, contact McCauley Propeller
Systems, One Cessna Boulevard, P.O. Box
7704, Wichita, Kansas 67277; telephone:
(800) 621–7767 or (316) 831–4021; email:
productsupport@txtav.com; internet: https://
mccauley.txtav.com. You may view this
service information at the FAA, Policy and
Innovation Division, 901 Locust, Kansas City,
Missouri 64106. For information on the
availability of this material at the FAA, call
(816) 329–4148.
Issued on April 1, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness
Division, Aircraft Certification Service.
[FR Doc. 2020–07168 Filed 4–6–20; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF JUSTICE
Drug Enforcement Administration
21 CFR Part 1308
[Docket No. DEA–498]
Schedules of Controlled Substances:
Placement of 4,4′-DMAR in Schedule I
Drug Enforcement
Administration, Department of Justice.
ACTION: Notice of proposed rulemaking.
AGENCY:
The Drug Enforcement
Administration proposes placing the
substance 4,4′-DMAR (Chemical name:
4,4′-dimethylaminorex), including its
salts, isomers, and salts of isomers, in
schedule I of the Controlled Substances
Act. This action is being taken to enable
the United States to meet its obligations
under the 1971 Convention on
Psychotropic Substances. If finalized,
this action would impose the regulatory
controls and administrative, civil, and
criminal sanctions applicable to
schedule I controlled substances on
persons who handle (manufacture,
distribute, reverse distribute, import,
export, engage in research, conduct
instructional activities or chemical
analysis with, or possess), or propose to
handle 4,4′-DMAR.
DATES: Comments must be submitted
electronically or postmarked on or
before June 8, 2020.
Interested persons may file a request
for hearing or waiver of hearing
SUMMARY:
(h) Parts Installation Prohibition
As of the effective date of this AD, do not
install on any airplane a McCauley governor
unless it is a governor eligible for
installation.
VerDate Sep<11>2014
or lacking a principal inspector, the manager
of the local flight standards district office/
certificate holding district office.
PO 00000
Frm 00003
Fmt 4702
Sfmt 4702
19401
pursuant to 21 CFR 1308.44 and in
accordance with 21 CFR 1316.45 and/or
1316.47, as applicable. Requests for
hearing and waivers of an opportunity
for a hearing or to participate in a
hearing must be received on or before
May 7, 2020.
ADDRESSES: Interested persons may file
written comments on this proposal in
accordance with 21 CFR 1308.43(g).
Commenters should be aware that the
electronic Federal Docket Management
System will not accept comments after
11:59 p.m. Eastern Time on the last day
of the comment period. To ensure
proper handling of comments, please
reference ‘‘Docket No. DEA–498’’ on all
electronic and written correspondence,
including any attachments.
• Electronic comments: The Drug
Enforcement Administration encourages
that all comments be submitted
electronically through the Federal
eRulemaking Portal, which provides the
ability to type short comments directly
into the comment field on the web page
or attach a file for lengthier comments.
Please go to https://www.regulations.gov
and follow the on-line instructions at
that site for submitting comments. Upon
completion of your submission you will
receive a Comment Tracking Number for
your comment. Please be aware that
submitted comments are not
instantaneously available for public
view on regulations.gov. If you have
received a Comment Tracking Number,
your comment has been successfully
submitted and there is no need to
resubmit the same comment.
• Paper comments: Paper comments
that duplicate electronic submissions
are not necessary and are discouraged.
Should you wish to mail a paper
comment in lieu of an electronic
comment, it should be sent via regular
or express mail to: Drug Enforcement
Administration, Attn: DEA Federal
Register Representative/DPW, 8701
Morrissette Drive, Springfield, Virginia
22152.
• Hearing requests: All requests for a
hearing and waivers of participation
must be sent to: Drug Enforcement
Administration, Attn: Administrator,
8701 Morrissette Drive, Springfield,
Virginia 22152. All requests for hearing
and waivers of participation should also
be sent to: (1) Drug Enforcement
Administration, Attn: Hearing Clerk/LJ,
8701 Morrissette Drive, Springfield,
Virginia 22152; and (2) Drug
Enforcement Administration, Attn: DEA
Federal Register Representative/DPW,
8701 Morrissette Drive, Springfield,
Virginia 22152.
FOR FURTHER INFORMATION CONTACT:
Scott A. Brinks, Regulatory Drafting and
E:\FR\FM\07APP1.SGM
07APP1
Agencies
[Federal Register Volume 85, Number 67 (Tuesday, April 7, 2020)]
[Proposed Rules]
[Pages 19399-19401]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2020-07168]
========================================================================
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. 85, No. 67 / Tuesday, April 7, 2020 /
Proposed Rules
[[Page 19399]]
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2020-0320; Product Identifier 2019-CE-011-AD]
RIN 2120-AA64
Airworthiness Directives; McCauley Propeller Systems Governors
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM).
-----------------------------------------------------------------------
SUMMARY: The FAA proposes to adopt a new airworthiness directive (AD)
for certain model McCauley Propeller Systems (McCauley) governors
installed on airplanes. This proposed AD was prompted by reports of an
unapproved variant McCauley idler gear bearing, part number (P/N) A-
20028, that could be installed in the affected governors. This proposed
AD would require replacing the governor with a governor that is
eligible for installation. The FAA is proposing this AD to address the
unsafe condition on these products.
DATES: The FAA must receive comments on this proposed AD by May 22,
2020.
ADDRESSES: You may send comments, using the procedures found in 14 CFR
11.43 and 11.45, by any of the following methods:
Federal eRulemaking Portal: Go to https://www.regulations.gov. Follow the instructions for submitting comments.
Fax: 202-493-2251.
Mail: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue SE, Washington, DC 20590.
Hand Delivery: Deliver to Mail address above between 9
a.m. and 5 p.m., Monday through Friday, except Federal holidays.
For service information identified in this NPRM, contact McCauley
Propeller Systems, One Cessna Boulevard, P.O. Box 7704, Wichita, Kansas
67277; telephone: (800) 621-7767 or (316) 831-4021; email:
[email protected]; internet: https://mccauley.txtav.com. You may
view this service information at the FAA, Policy and Innovation
Division, 901 Locust, Kansas City, Missouri 64106. For information on
the availability of this material at the FAA, call (816) 329-4148.
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-2020-
0320 or in person at Docket Operations between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays. The AD docket contains
this NPRM, the regulatory evaluation, 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 FURTHER INFORMATION CONTACT: Thomas Teplik, Aerospace Engineer,
Wichita ACO Branch, 1801 Airport Road, Room 100, Wichita, Kansas 67209;
telephone: (316) 946-4196; fax: (316) 946-4107; email:
[email protected] or [email protected].gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
The FAA invites you to send any written relevant data, views, or
arguments about this proposal. Send your comments to an address listed
under the ADDRESSES section. Include ``Docket No. FAA-2020-0320;
Product Identifier 2019-CE-011-AD'' at the beginning of your comments.
The FAA specifically invites comments on the overall regulatory,
economic, environmental, and energy aspects of this NPRM. The FAA will
consider all comments received by the closing date and may amend this
NPRM because of those comments.
The FAA will post all comments received, without change, to https://www.regulations.gov, including any personal information you provide.
The FAA will also post a report summarizing each substantive verbal
contact received about this NPRM.
Discussion
The FAA has received reports from McCauley that an unapproved
variant idler gear bearing, part number (P/N) A-20028, was installed on
certain governors during production between January 31, 2017, and
September 27, 2018, and may have been installed on governors in service
after January 31, 2017. The unapproved variant of the idler gear
bearing does not conform to McCauley drawing requirements.
All models of McCauley governors have an idler gear bearing with P/
N A-20028 installed; however, the unapproved variant of the bearing can
be identified by part marking ``BA-59.'' The non-conforming idler gear
bearing could have also been included in the idler gear assembly (idler
gear and bearing), P/N A-20107, or the governor overhaul kit, P/N PL-
20233 or PL-20234.
The non-conformity of the bearing may cause premature failure of
the idler gear bearing. Early symptoms that the idler gear bearing may
fail include inability of the governor to hold the selected RPM,
hunting, surging, etc. An investigation identified 23 occurrences of
airplane operation problems related to erratic governor behavior that
may have resulted from the unapproved idler gear bearing.
This condition, if not addressed, could cause the idler gear
bearing to fail. This failure could result in failure of the governor,
loss of propeller pitch control, engine and propeller over speed,
engine oil contamination, and loss of control.
Related Service Information Under 1 CFR Part 51
The FAA reviewed McCauley Alert Service Bulletin ASB273C, dated
January 30, 2019. The service bulletin contains model and serial number
information to identify the affected governors. The service bulletin
also contains procedures for removing the governor from the engine,
inspecting the governor for the unapproved variant idler gear bearing,
replacing the idler gear bearing or idler gear assembly if necessary,
overhauling the governor if necessary, and installing a governor on the
engine. 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.
FAA's Determination
The FAA is proposing this AD because it evaluated all relevant
information and determined the unsafe
[[Page 19400]]
condition described previously is likely to exist or develop in other
products of the same type design.
Proposed AD Requirements
This proposed AD would require replacing an affected governor with
a governor eligible for installation.
Differences Between This Proposed AD and the Service Information
The service bulletin contains maintenance procedures for inspecting
an affected governor and any subsequent corrective actions required to
ensure the governor is eligible for continued service and installation.
The service bulletin also references other McCauley service documents
for additional maintenance actions to include overhaul of the governor.
However, this NPRM only proposes replacing the affected governor with a
governor eligible for installation.
Costs of Compliance
The FAA estimates that this proposed AD affects 2,500 governors as
installed in airplanes of U.S. registry.
The FAA estimates the following costs to comply with this proposed
AD:
Estimated Costs
----------------------------------------------------------------------------------------------------------------
Cost on U.S.
Action Labor cost Parts cost Cost per product operators
----------------------------------------------------------------------------------------------------------------
Remove affected governor....... 1 work-hour x $85 per Not Applicable... $85 $212,500
hour = $85.
Install an governor............ 1 work-hour x $85 per See table below.. Variable Unknown
hour = $85.
----------------------------------------------------------------------------------------------------------------
An operator has the option to pay a service center to inspect their
existing governor and replace the idler gear bearing if necessary or
pay to have their existing governor overhauled. An operator has the
option to purchase a factory new governor or an overhauled governor, a
feathering/syncing governor or a non-feathering/syncing governor. The
FAA has no way of knowing what option an operator may take to obtain a
governor eligible for installation. Therefore, the FAA has no way of
determining the parts cost on U.S. operators. The following represents
the estimated parts cost associated with obtaining a governor.
Cost for an Eligible Governor
------------------------------------------------------------------------
Type of governor Cost of governor
------------------------------------------------------------------------
Factory new non-feathering/non-syncing governor...... $2,000
Factory new feathering/syncing governor.............. 9,000
Overhaul of existing non-feathering/non-syncing 1,000
governor............................................
Overhaul of existing feathering/syncing governor..... 3,000
------------------------------------------------------------------------
According to the manufacturer, some of the costs of this proposed
AD may be covered under warranty, thereby reducing the cost impact on
affected individuals. The FAA does not control warranty coverage for
affected individuals. As a result, the FAA has included all costs in
our cost estimate.
Authority for This Rulemaking
Title 49 of the United States Code specifies the FAA's authority to
issue rules on aviation safety. Subtitle I, section 106, describes the
authority of the FAA Administrator. Subtitle VII: Aviation Programs,
describes in more detail the scope of the Agency's authority.
The FAA is issuing this rulemaking under the authority described in
Subtitle VII, Part A, Subpart III, section 44701: General requirements.
Under that section, Congress charges the FAA with promoting safe flight
of civil aircraft in air commerce by prescribing regulations for
practices, methods, and procedures the Administrator finds necessary
for safety in air commerce. This regulation is within the scope of that
authority because it addresses an unsafe condition that is likely to
exist or develop on products identified in this rulemaking action.
Regulatory Findings
The FAA determined that this proposed AD would not have federalism
implications under Executive Order 13132. This proposed AD would not
have a substantial direct effect on the States, on the relationship
between the national government and the States, or on the distribution
of power and responsibilities among the various levels of government.
For the reasons discussed above, I certify this proposed
regulation:
(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 Proposed Amendment
Accordingly, under the authority delegated to me by the
Administrator, the FAA proposes to amend 14 CFR part 39 as follows:
PART 39--AIRWORTHINESS DIRECTIVES
0
1. The authority citation for part 39 continues to read as follows:
Authority: 49 U.S.C. 106(g), 40113, 44701.
Sec. 39.13 [Amended]
0
2. The FAA amends Sec. 39.13 by adding the following new airworthiness
directive (AD):
McCauley Propeller Systems: Docket No. FAA-2020-0320; Product
Identifier 2019-CE-011-AD.
(a) Comments Due Date
The FAA must receive comments by May 22, 2020.
(b) Affected ADs
None.
(c) Applicability
This AD applies to the McCauley Propeller Systems (McCauley)
governors specified in paragraphs (c)(1) or (2) of this AD and
[[Page 19401]]
installed on airplanes, certificated in any category.
(1) Models listed in table 2 of McCauley Alert Service Bulletin
No. ASB273C, dated January 30, 2019 (McCauley ASB273C) with a serial
number from 170061 through 180501, excluding the serial numbers
listed in table 1 of McCauley ASB273C.
(2) Models listed in table 2 of McCauley ASB273C, with any
serial number, that have an installation date after January 31,
2017, or an installation date that cannot be determined.
(d) Subject
Joint Aircraft System Component (JASC)/Air Transport Association
(ATA) of America Code 61, Propellers.
(e) Unsafe Condition
This AD was prompted by reports of an unapproved variant idler
gear bearing, McCauley part number (P/N) A-20028, installed on
governors. All models of McCauley governors have a bearing with P/N
A-20028 installed; however, the unapproved variant can be identified
with the part marking ``BA-59.'' The FAA is issuing this AD to
prevent failure of the idler gear bearing. This failure could result
in failure of the governor, loss of propeller pitch control, engine
and propeller over speed, engine oil contamination, and loss of
control of the airplane.
(f) Compliance
Unless already done, within 50 hours time-in-service after the
effective date of this AD or within 24 months after the effective
date of this AD, whichever occurs first, replace the governor with a
governor eligible for installation.
Note 1 to paragraph (f) of this AD: Any model McCauley governor
that is stamped with the letter B, as specified in the
Accomplishment Instructions in McCauley ASB273C, has already
complied with the requirements of this AD.
(g) Definition
For the purposes of this AD, a governor eligible for
installation is defined as a governor that does not have an idler
gear bearing with a part marking ``BA-59'' installed.
(h) Parts Installation Prohibition
As of the effective date of this AD, do not install on any
airplane a McCauley governor unless it is a governor eligible for
installation.
(i) Alternative Methods of Compliance (AMOCs)
(1) The Manager, Wichita ACO Branch, FAA, has the authority to
approve AMOCs for this AD, if requested using the procedures found
in 14 CFR 39.19. In accordance with 14 CFR 39.19, send your request
to your principal inspector or local Flight Standards District
Office, as appropriate. If sending information directly to the
manager of the certification office, send it to the attention of the
person identified in paragraph (l)(1) of this AD.
(2) Before using any approved AMOC, notify your appropriate
principal inspector, or lacking a principal inspector, the manager
of the local flight standards district office/certificate holding
district office.
(j) Related Information
(1) For more information about this AD, contact Thomas Teplik,
Aerospace Engineer, Wichita ACO Branch, 1801 Airport Road, Room 100,
Wichita, Kansas 67209; telephone: (316) 946-4196; fax: (316) 946-
4107; email: [email protected] or [email protected].
(2) For service information identified in this AD, contact
McCauley Propeller Systems, One Cessna Boulevard, P.O. Box 7704,
Wichita, Kansas 67277; telephone: (800) 621-7767 or (316) 831-4021;
email: [email protected]; internet: https://mccauley.txtav.com. You may view this service information at the
FAA, Policy and Innovation Division, 901 Locust, Kansas City,
Missouri 64106. For information on the availability of this material
at the FAA, call (816) 329-4148.
Issued on April 1, 2020.
Lance T. Gant,
Director, Compliance & Airworthiness Division, Aircraft Certification
Service.
[FR Doc. 2020-07168 Filed 4-6-20; 8:45 am]
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