Special Conditions: SNECMA, Silvercrest-2 SC-2D; Rated 10-Minute One Engine Inoperative Takeoff Thrust at High Ambient Temperature; Withdrawal, 28993-28994 [2017-12937]
Download as PDF
Federal Register / Vol. 82, No. 122 / Tuesday, June 27, 2017 / Rules and Regulations
2. Amend § 457.8, in the Common
Crop Insurance Policy, as follows:
■ a. In section 1 by revising the
definition of ‘‘practical to replant’’ and
‘‘replanted crop;’’ and
■ b. In section 15 by revising paragraph
(h).
The revisions read as follows:
■
§ 457.8
*
*
The application and policy.
*
*
*
Common Crop Insurance Policy
*
*
*
*
*
1. Definitions
pmangrum on DSK3GDR082PROD with RULES
*
*
*
*
*
Practical to replant. Our
determination, after loss or damage to
the insured crop, that you are able to
replant to the same crop in such areas
and under such circumstances as it is
customary to replant and that replanting
the insured crop will allow the crop to
attain maturity prior to the calendar
date for the end of the insurance period.
We may consider circumstances as to
whether: (1) It is physically possible to
replant the acreage; (2) seed
germination, emergence, and formation
of a healthy plant is likely; (3) field, soil,
and growing conditions allow for proper
planting and growth of the replanted
crop to reach maturity; or (4) other
conditions exist, as provided by the
Crop Provisions or Special Provisions.
Unless we determine it is not practical
to replant, based on the circumstances
listed above, it will be considered
practical to replant through: (1) The
final planting date if no late planting
period is applicable; (2) the end of the
late planting period if the late planting
period is less than 10 days; or (3) the
10th day after the final planting date if
the crop has a late planting period of 10
days or more. We will consider it
practical to replant regardless of the
availability of seed or plants, or the
input costs necessary to produce the
insured crop such as seed or plants,
irrigation water, etc.
*
*
*
*
*
Replanted crop. The same agricultural
commodity replanted on the same
acreage as the insured crop for harvest
in the same crop year if: (1) The
replanting is specifically made optional
by the policy and you elect to replant
the crop and insure it under the policy
covering the insured crop; or (2)
Replanting is required by the policy.
The crop will be considered a replanted
insured crop and no replanting payment
will be paid if we have determined it is
not practical to replant the insured crop
and you choose to plant the acreage to
the same insured crop.
*
*
*
*
*
VerDate Sep<11>2014
15:07 Jun 26, 2017
Jkt 241001
15. Production Included in Determining
an Indemnity and Payment Reductions
*
*
*
*
*
(h) You may receive a full indemnity,
or a full prevented planting payment for
a first insured crop when a second crop
is planted on the same acreage in the
same crop year, if each of the following
conditions are met, regardless of
whether or not the second crop is
insured or sustains an insurable loss:
(1) Planting two or more crops for
harvest in the same crop year in the area
is generally recognized by agricultural
experts or organic agricultural experts;
(2) The second or more crops are
customarily planted after the first
insured crop for harvest on the same
acreage in the same crop year in the
area;
(3) Additional coverage insurance
offered under the authority of the Act is
available in the county on the two or
more crops that are double cropped;
(4) In the case of prevented planting,
the second crop is not planted on or
prior to the final planting date or, if
applicable, prior to the end of the late
planting period for the first insured
crop;
(5) You provide records, acceptable to
us, of acreage and production specific to
the double cropped acreage proving
that:
(i) You have double cropped acreage
in at least two of the last four crop years
in which the first insured crop was
planted and incur an insurable loss or
the first insured crop is prevented from
being planted and a second crop is
planted. If you acquired additional land
for the current crop year you may apply
the percentage of acres that you have
previously double cropped to the total
cropland acres that you are farming this
year (if greater) using the following
calculation:
(A) Determine the number of acres of
the first insured crop that were double
cropped in each of the years for which
double cropping records are provided
(For example, records are provided
showing: 100 acres of wheat planted in
2016 and 50 of those acres were double
cropped with soybeans; and 100 acres of
wheat planted in 2017 and 70 of those
acres were double cropped with
soybeans);
(B) Divide each result of section
15(h)(5)(i)(A) by the number of acres of
the first insured crop that were planted
in each respective year (In the example
above, 50 divided by 100 equals 50
percent of the first insured crop acres
that were double cropped in 2016 and
70 divided by 100 equals 70 percent of
the first insured crop acres that were
double cropped in 2017);
PO 00000
Frm 00011
Fmt 4700
Sfmt 4700
28993
(C) Add the results of section
15(h)(5)(i)(B) and divide by the number
of years the first insured crop was
double cropped (In the example above,
50 plus 70 equals 120 divided by 2
equals 60 percent); and
(D) Multiply the result of
15(h)(5)(i)(C) by the number of insured
acres of the first insured crop (In the
example above, 60 percent multiplied
by the number of wheat acres insured in
2018); or
(ii) The applicable acreage was double
cropped (by one or more other
producers, and the producer(s) will
allow you to use their records) for at
least two of the last four crop years in
which the first insured crop was grown
on it; and
(6) If you do not have records of
acreage and production specific to the
double cropped acreage, as required in
section 15(h)(5), but instead have
records that combine production from
acreage you double cropped with
records of production from acreage you
did not double crop, we will allocate the
first and second crop production to the
specific acreage in proportion to the
liability for the acreage that was and
was not double cropped.
*
*
*
*
*
Dated: June 20, 2017.
Robert Ibarra,
Acting Administrator.
[FR Doc. 2017–13242 Filed 6–26–17; 8:45 am]
BILLING CODE 3410–08–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 33
[Docket No. FAA–2014–0376; Notice No. 33–
014–01–SC]
Special Conditions: SNECMA,
Silvercrest-2 SC–2D; Rated 10-Minute
One Engine Inoperative Takeoff Thrust
at High Ambient Temperature;
Withdrawal
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions;
withdrawal.
AGENCY:
The FAA is withdrawing
previously published special conditions
for the Silvercrest-2 SC–2D engine
model. We are requesting the
withdrawal because the ‘‘Rated 10Minute One Engine Inoperative Takeoff
Thrust at High Ambient Temperature
(Rated 10-Minute OEI TOTHAT) is not
needed.
SUMMARY:
E:\FR\FM\27JNR1.SGM
27JNR1
28994
Federal Register / Vol. 82, No. 122 / Tuesday, June 27, 2017 / Rules and Regulations
As of June 27, 2017, the special
conditions published on October 31,
2014, at 79 FR 64666, are withdrawn.
FOR FURTHER INFORMATION CONTACT: Tara
Fitzgerald, ANE–112, Engine and
Propeller Directorate, Aircraft
Certification Service, 1200 District
Avenue, Burlington, Massachusetts,
01803–5213; telephone (781) 238–7130;
facsimile (781) 238–7199; email
Tara.Fitzgerald@faa.gov.
SUPPLEMENTARY INFORMATION:
DATES:
Background
On April 19, 2011, SNECMA, now
known as Safran Aircraft Engines (SAE)
applied for a new type certificate for the
Silvercrest-2 SC–2D engine model. At
that time, the Silvercrest-2 SC–2D
engine model was to have a novel or
unusual design feature when compared
to the state of technology described in
the airworthiness standards for aircraft
engines. The design feature included an
additional takeoff rating for the
Silvercrest-2 SC–2D engine model,
named ‘‘Rated 10-Minute One Engine
Inoperative Takeoff Thrust at High
Ambient Temperature’’ (Rated 10Minute OEI TOTHAT). It was intended
to maintain the takeoff thrust in certain
high ambient temperature conditions for
a maximum of 10 minutes with one
engine inoperative (OEI).
Reason for Withdrawal
The FAA is withdrawing Notice No.
33–014–01–SC because of concerns
raised over the sufficiency of the ‘‘Rated
10-Minute OEI TOTHAT’’ special
condition to meet the Automatic Takeoff
Thrust Control System (ATTCS) design
requirement specified in Title 14, Code
of Federal Regulations (14 CFR) part 25,
section I25.5(b)(2).
The proposed takeoff rating was for
use during OEI events that occur during
takeoff in high ambient temperature
conditions, up to 5 degrees Celsius
hotter than the rated takeoff corner
point. The assumptions for this rating
are no longer valid and the ‘‘Rated 10Minute OEI TOTHAT’’ is not needed.
pmangrum on DSK3GDR082PROD with RULES
Conclusion
This withdrawal does not preclude
the FAA from issuing another notice on
the subject matter in the future or
committing the agency to any future
course of action.
Issued in Burlington, Massachusetts, on
June 13, 2017.
Carlos A. Pestana,
Acting Assistant Manager, Engine and
Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2017–12937 Filed 6–26–17; 8:45 am]
BILLING CODE 4910–13–P
VerDate Sep<11>2014
15:07 Jun 26, 2017
Jkt 241001
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 33
[Docket No. FAA–2014–0376; Notice No. 33–
014–01–SC]
Special Conditions: SNECMA,
Silvercrest-2 SC–2D; Rated 10-Minute
One Engine Inoperative Takeoff Thrust
at High Ambient Temperature;
Withdrawal
Federal Aviation
Administration (FAA), DOT.
ACTION: Final special conditions,
withdrawal.
AGENCY:
The FAA is withdrawing
previously published special conditions
for the Silvercrest-2 SC–2D engine
model. We are requesting the
withdrawal because the ‘‘Rated 10Minute One Engine Inoperative Takeoff
Thrust at High Ambient Temperature
(Rated 10-Minute OEI TOTHAT) is not
needed.
DATES: As of June 27, 2017, the special
conditions published on October 31,
2014 at 79 FR 64666, are withdrawn.
FOR FURTHER INFORMATION CONTACT: Tara
Fitzgerald, ANE–112, Engine and
Propeller Directorate, Aircraft
Certification Service, 1200 District
Avenue, Burlington, Massachusetts,
01803–5213; telephone (781) 238–7130;
facsimile (781) 238–7199; email
Tara.Fitzgerald@faa.gov.
SUPPLEMENTARY INFORMATION:
SUMMARY:
Background
On April 19, 2011, SNECMA, now
known as Safran Aircraft Engines (SAE)
applied for a new type certificate for the
Silvercrest-2 SC–2D engine model. At
that time, the Silvercrest-2 SC–2D
engine model was to have a novel or
unusual design feature when compared
to the state of technology described in
the airworthiness standards for aircraft
engines. The design feature included an
additional takeoff rating for the
Silvercrest-2 SC–2D engine model,
named ‘‘Rated 10-Minute One Engine
Inoperative Takeoff Thrust at High
Ambient Temperature’’ (Rated 10Minute OEI TOTHAT). It was intended
to maintain the takeoff thrust in certain
high ambient temperature conditions for
a maximum of 10 minutes with one
engine inoperative (OEI).
Reason for Withdrawal
The FAA is withdrawing Notice No.
33–014–01–SC because of concerns
raised over the sufficiency of the ‘‘Rated
10-Minute OEI TOTHAT’’ special
condition to meet the Automatic Takeoff
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
Thrust Control System (ATTCS) design
requirement specified in Title 14, Code
of Federal Regulations (14 CFR) part 25,
section I25.5(b)(2).
The proposed takeoff rating was for
use during OEI events that occur during
takeoff in high ambient temperature
conditions, up to 5 degrees Celsius
hotter than the rated takeoff corner
point. The assumptions for this rating
are no longer valid and the ‘‘Rated 10Minute OEI TOTHAT’’ is not needed.
Conclusion
This withdrawal does not preclude
the FAA from issuing another notice on
the subject matter in the future or
committing the agency to any future
course of action.
Issued in Burlington, Massachusetts, on
June 13, 2017.
Carlos A. Pestana,
Acting Assistant Manager, Engine and
Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 2017–12939 Filed 6–26–17; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF COMMERCE
National Institutes of Standards and
Technology
15 CFR Part 290
[Docket No.: 170526519–7519–01]
RIN 0693–AB64
Hollings Manufacturing Extension
Partnership—Amendments to the
Terms and Schedule of Financial
Assistance
National Institute of Standards
and Technology (NIST), United States
Department of Commerce.
ACTION: Final rule.
AGENCY:
NIST is issuing a final rule to
amend the regulations governing the
Hollings Manufacturing Extension
Partnership (MEP) program to reflect the
current cost sharing requirements for
cooperative agreements for the
establishment and operation of MEP
Centers, consistent with recent
amendments to the MEP authorizing
statute. Under the revised statute, NIST
may provide up to 50 percent of the
capital and annual operating and
maintenance funds required to establish
and support an MEP Center. The
regulations are also being amended to
remove other cost sharing rules that are
not required by the MEP authorizing
statute or current program policies.
DATES: This rule is effective June 27,
2017.
SUMMARY:
E:\FR\FM\27JNR1.SGM
27JNR1
Agencies
[Federal Register Volume 82, Number 122 (Tuesday, June 27, 2017)]
[Rules and Regulations]
[Pages 28993-28994]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 2017-12937]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 33
[Docket No. FAA-2014-0376; Notice No. 33-014-01-SC]
Special Conditions: SNECMA, Silvercrest-2 SC-2D; Rated 10-Minute
One Engine Inoperative Takeoff Thrust at High Ambient Temperature;
Withdrawal
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; withdrawal.
-----------------------------------------------------------------------
SUMMARY: The FAA is withdrawing previously published special conditions
for the Silvercrest-2 SC-2D engine model. We are requesting the
withdrawal because the ``Rated 10-Minute One Engine Inoperative Takeoff
Thrust at High Ambient Temperature (Rated 10-Minute OEI TOTHAT) is not
needed.
[[Page 28994]]
DATES: As of June 27, 2017, the special conditions published on October
31, 2014, at 79 FR 64666, are withdrawn.
FOR FURTHER INFORMATION CONTACT: Tara Fitzgerald, ANE-112, Engine and
Propeller Directorate, Aircraft Certification Service, 1200 District
Avenue, Burlington, Massachusetts, 01803-5213; telephone (781) 238-
7130; facsimile (781) 238-7199; email Tara.Fitzgerald@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
On April 19, 2011, SNECMA, now known as Safran Aircraft Engines
(SAE) applied for a new type certificate for the Silvercrest-2 SC-2D
engine model. At that time, the Silvercrest-2 SC-2D engine model was to
have a novel or unusual design feature when compared to the state of
technology described in the airworthiness standards for aircraft
engines. The design feature included an additional takeoff rating for
the Silvercrest-2 SC-2D engine model, named ``Rated 10-Minute One
Engine Inoperative Takeoff Thrust at High Ambient Temperature'' (Rated
10-Minute OEI TOTHAT). It was intended to maintain the takeoff thrust
in certain high ambient temperature conditions for a maximum of 10
minutes with one engine inoperative (OEI).
Reason for Withdrawal
The FAA is withdrawing Notice No. 33-014-01-SC because of concerns
raised over the sufficiency of the ``Rated 10-Minute OEI TOTHAT''
special condition to meet the Automatic Takeoff Thrust Control System
(ATTCS) design requirement specified in Title 14, Code of Federal
Regulations (14 CFR) part 25, section I25.5(b)(2).
The proposed takeoff rating was for use during OEI events that
occur during takeoff in high ambient temperature conditions, up to 5
degrees Celsius hotter than the rated takeoff corner point. The
assumptions for this rating are no longer valid and the ``Rated 10-
Minute OEI TOTHAT'' is not needed.
Conclusion
This withdrawal does not preclude the FAA from issuing another
notice on the subject matter in the future or committing the agency to
any future course of action.
Issued in Burlington, Massachusetts, on June 13, 2017.
Carlos A. Pestana,
Acting Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 2017-12937 Filed 6-26-17; 8:45 am]
BILLING CODE 4910-13-P