Special Conditions: Cirrus Design Corporation, Model SF50; Fire Extinguishing for Upper Aft Fuselage Mounted Engine; Withdrawal, 35747 [2013-14151]
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Federal Register / Vol. 78, No. 115 / Friday, June 14, 2013 / Rules and Regulations
of the Interior acknowledges to exist as
an Indian tribe pursuant to the Federally
Recognized Indian Tribe List Act of
1994. Tribal participation is voluntary.
Tribes may express interest in
participating in the advance
notifications and may discontinue their
participation at any time. Currently, 27
Tribes have expressed interest in
receiving the advance notifications.
Tribes meeting the criteria may receive
advance notifications after certifying
that the Safeguards Information
associated with the shipments of these
materials will be adequately protected
by complying with the requirements in
10 CFR 73.21 and 73.22.
After the NRC receives this
certification and the contact information
for the Tribal official or Tribal official’s
designee, the NRC will add the Tribe to
the list of advance notification contacts
and the Tribal reservation information
to the interactive map of Tribal
boundaries at https://www.nrc.gov/
about-nrc/state-tribal/tribal-advancenotification.html. Current contact
information can also be accessed
throughout the year at https://nrcstp.ornl.gov/special/designee.pdf. The
list is published annually in the Federal
Register on or about June 30 to reflect
any changes in information. Licensees
should check these sites to determine
whether they need to provide advance
notification when they have any
shipments meeting the criteria in 10
CFR 71.97 or 73.37 that will pass within
or across a participating Tribe’s
reservation.
Dated at Rockville, Maryland, this 10th day
of June 2013.
For the U.S. Nuclear Regulatory
Commission.
Melanie A. Galloway,
Acting Director, Division of
Intergovernmental Liaison and Rulemaking,
Office of Federal and State Materials and
Environmental Management Programs.
[FR Doc. 2013–14159 Filed 6–13–13; 8:45 am]
BILLING CODE 7590–01–P
Final special conditions;
withdrawal.
ACTION:
SUMMARY: The FAA is withdrawing a
previously published notice granting
special conditions for the Cirrus Design
Corporation model SF50 airplane. We
are withdrawing Special Condition No.
23–245–SC through mutual agreement
with Cirrus Design Corporation.
DATES: This special condition published
on April 20, 2010 at 75 FR 20518 is
withdrawn, effective June 14, 2013.
FOR FURTHER INFORMATION CONTACT:
Leslie B. Taylor, Federal Aviation
Administration, Small Airplane
Directorate, Aircraft Certification
Service, 901 Locust, Room 301, Kansas
City, MO 64106; telephone (816) 329–
4134; facsimile (816) 329–4090, email
leslie.b.taylor@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
On April 20, 2010, the FAA published
Special Condition No. 23–245–SC for
the Cirrus Design Corporation new
model SF50. The model SF50 is a 7-seat
(5 adults and 2 children), pressurized,
retractable gear, carbon composite,
airplane with one turbofan engine
mounted partially in the upper aft
fuselage.
The single turbofan engine is
mounted on the upper aft fuselage, not
in the pilot’s line of site. Upper aft
fuselage mounted engine installations,
along with the need to protect such
installed engines from fires, were not
envisioned in the development of the
part 23 normal category regulations.
The model SF50 certification project
was granted an extension on September
19, 2011. Amendment 23–62 (76 FR
75736), published December 2, 2011,
incorporated Special Condition No. 23–
245–SC. On December 11, 2012, Cirrus
Design Corporation elected to adjust the
model SF50 certification basis to 14 CFR
part 23, Amendment 62.
Reason for Withdrawal
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 23
mstockstill on DSK4VPTVN1PROD with RULES
[Docket No. CE305; Special Conditions No.
23–245–SC]
Special Conditions: Cirrus Design
Corporation, Model SF50; Fire
Extinguishing for Upper Aft Fuselage
Mounted Engine; Withdrawal
Federal Aviation
Administration (FAA), DOT.
AGENCY:
VerDate Mar<15>2010
15:51 Jun 13, 2013
Jkt 229001
The FAA is withdrawing Special
Condition No. 23–245–SC because
Cirrus elected to revise the model SF50
certification basis to Amendment 23–62.
The authority citation for this Special
Condition withdrawal is 49 U.S.C.
106(g), 40113 and 44701; 14 CFR 21.16
and 21.17; and 14 CFR 11.38 and 11.19.
Conclusion
Withdrawal of this special condition
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.
PO 00000
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Fmt 4700
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35747
Issued in Kansas City, Missouri on June 5,
2013.
Earl Lawrence,
Small Airplane Directorate, Aircraft
Certification Service.
[FR Doc. 2013–14151 Filed 6–13–13; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2012–1329; Directorate
Identifier 2012–NE–46–AD; Amendment
39–17479; AD 2013–12–02]
RIN 2120–AA64
Airworthiness Directives; Engine
Alliance Turbofan Engines
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: We are adopting a new
airworthiness directive (AD) for certain
Engine Alliance GP7270 and GP7277
turbofan engines. This AD was
prompted by damage to the highpressure compressor (HPC) stage 7–9
spool caused by failure of the baffle
plate feature on affected HPC stage 6
disks. This AD requires initial and
repetitive borescope inspections of the
baffle plate feature and removal from
service of the HPC stage 6 disk if the
plate is missing material. This AD also
requires mandatory removal from
service of these HPC stage 6 disks at the
next HPC module exposure. We are
issuing this AD to prevent failure of the
HPC stage 7–9 spool, uncontained
engine failure, and damage to the
airplane.
DATES:
This AD is effective July 19,
2013.
Examining the AD Docket
You may examine the AD docket on
the Internet at https://
www.regulations.gov; or in person at the
Docket Management Facility between 9
a.m. and 5 p.m., Monday through
Friday, except Federal holidays. The AD
docket contains this AD, the regulatory
evaluation, any comments received, and
other information. The address for the
Docket Office (phone: 800–647–5527) is
Document Management Facility, U.S.
Department of Transportation, Docket
Operations, M–30, West Building
Ground Floor, Room W12–140, 1200
New Jersey Avenue SE., Washington,
DC 20590.
FOR FURTHER INFORMATION CONTACT:
Martin Adler, Aerospace Engineer,
E:\FR\FM\14JNR1.SGM
14JNR1
]]>Agencies
[Federal Register Volume 78, Number 115 (Friday, June 14, 2013)]
[Rules and Regulations]
[Page 35747]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2013-14151]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 23
[Docket No. CE305; Special Conditions No. 23-245-SC]
Special Conditions: Cirrus Design Corporation, Model SF50; Fire
Extinguishing for Upper Aft Fuselage Mounted Engine; Withdrawal
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final special conditions; withdrawal.
-----------------------------------------------------------------------
SUMMARY: The FAA is withdrawing a previously published notice granting
special conditions for the Cirrus Design Corporation model SF50
airplane. We are withdrawing Special Condition No. 23-245-SC through
mutual agreement with Cirrus Design Corporation.
DATES: This special condition published on April 20, 2010 at 75 FR
20518 is withdrawn, effective June 14, 2013.
FOR FURTHER INFORMATION CONTACT: Leslie B. Taylor, Federal Aviation
Administration, Small Airplane Directorate, Aircraft Certification
Service, 901 Locust, Room 301, Kansas City, MO 64106; telephone (816)
329-4134; facsimile (816) 329-4090, email leslie.b.taylor@faa.gov.
SUPPLEMENTARY INFORMATION:
Background
On April 20, 2010, the FAA published Special Condition No. 23-245-
SC for the Cirrus Design Corporation new model SF50. The model SF50 is
a 7-seat (5 adults and 2 children), pressurized, retractable gear,
carbon composite, airplane with one turbofan engine mounted partially
in the upper aft fuselage.
The single turbofan engine is mounted on the upper aft fuselage,
not in the pilot's line of site. Upper aft fuselage mounted engine
installations, along with the need to protect such installed engines
from fires, were not envisioned in the development of the part 23
normal category regulations.
The model SF50 certification project was granted an extension on
September 19, 2011. Amendment 23-62 (76 FR 75736), published December
2, 2011, incorporated Special Condition No. 23-245-SC. On December 11,
2012, Cirrus Design Corporation elected to adjust the model SF50
certification basis to 14 CFR part 23, Amendment 62.
Reason for Withdrawal
The FAA is withdrawing Special Condition No. 23-245-SC because
Cirrus elected to revise the model SF50 certification basis to
Amendment 23-62.
The authority citation for this Special Condition withdrawal is 49
U.S.C. 106(g), 40113 and 44701; 14 CFR 21.16 and 21.17; and 14 CFR
11.38 and 11.19.
Conclusion
Withdrawal of this special condition 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 Kansas City, Missouri on June 5, 2013.
Earl Lawrence,
Small Airplane Directorate, Aircraft Certification Service.
[FR Doc. 2013-14151 Filed 6-13-13; 8:45 am]
BILLING CODE 4910-13-P
