Airworthiness Directives; Burl A. Rogers (Type Certificate Previously Held by William Brad Mitchell and Aeronca, Inc.) Models 15AC and S15AC Airplanes, 23920-23921 [2011-10383]
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23920
Federal Register / Vol. 76, No. 83 / Friday, April 29, 2011 / Proposed Rules
Archives and records, Imports, Labeling,
Organically produced products, Plants,
Reporting and recordkeeping
requirements, Seals and insignia, Soil
conservation.
For the reasons set forth in the
preamble, 7 CFR part 205, subpart G is
proposed to be amended as follows:
PART 205—NATIONAL ORGANIC
PROGRAM
1. The authority citation for 7 CFR
part 205 continues to read as follows:
Authority: 7 U.S.C. 6501–6522.
2. Section 205.670 is revised to read
as follows:
emcdonald on DSK2BSOYB1PROD with PROPOSALS
§ 205.670 Inspection and testing of
agricultural product to be sold or labeled as
‘‘100 percent organic,’’ ‘‘organic,’’ or ‘‘made
with organic (specified ingredients or food
group(s)).’’
(a) All agricultural products that are
to be sold, labeled, or represented as
‘‘100 percent organic,’’ ‘‘organic,’’ or
‘‘made with organic (specified
ingredients or food group(s))’’ must be
made accessible by certified organic
production or handling operations for
examination by the Administrator, the
applicable State organic program’s
governing State official, or the certifying
agent.
(b) The Administrator, applicable
State organic program’s governing State
official, or the certifying agent may
require preharvest or postharvest testing
of any agricultural input used or
agricultural product to be sold, labeled,
or represented as ‘‘100 percent organic,’’
‘‘organic,’’ or ‘‘made with organic
(specified ingredients or food group(s))’’
when there is reason to believe that the
agricultural input or product has come
into contact with a prohibited substance
or has been produced using excluded
methods. Such tests must be conducted
by the applicable State organic
program’s governing State official or the
certifying agent at the official’s or
certifying agent’s own expense.
(c) A certifying agent must conduct
periodic residue testing of agricultural
products to be sold, labeled, or
represented as ‘‘100 percent organic,’’
‘‘organic,’’ or ‘‘made with organic
(specified ingredients or food group(s)).’’
Such tests must be conducted by the
certifying agent at the certifying agent’s
own expense. A certifying agent must,
on an annual basis, sample and test
from a minimum of five percent of the
operations it certifies, rounded to the
nearest whole number. A certifying
agent that certifies fewer than thirty
operations on an annual basis must
sample and test from at least one
operation annually.
VerDate Mar<15>2010
17:59 Apr 28, 2011
Jkt 223001
(d) Sample collection pursuant to
paragraphs (b) and (c) of this section
must be performed by an inspector
representing the Administrator,
applicable State organic program’s
governing State official, or certifying
agent. Sample integrity must be
maintained throughout the chain of
custody, and residue testing must be
performed in an accredited laboratory.
Chemical analysis must be made in
accordance with the methods described
in the most current edition of the
Official Methods of Analysis of the
AOAC International or other current
applicable validated methodology for
determining the presence of
contaminants in agricultural products.
(e) Results of all analyses and tests
performed under this section:
(1) Must be promptly provided to the
Administrator; Except, That, where a
State organic program exists, all test
results and analyses shall be provided to
the State organic program’s governing
State official by the applicable certifying
party that requested testing; and
(2) Will be available for public access,
unless the testing is part of an ongoing
compliance investigation.
(f) If test results indicate a specific
agricultural product contains pesticide
residues or environmental contaminants
that exceed the Food and Drug
Administration’s or the Environmental
Protection Agency’s regulatory
tolerances, the certifying agent must
promptly report such data to the Federal
health agency whose regulatory
tolerance or action level has been
exceeded. Test results that exceed
federal regulatory tolerances must also
be reported to the appropriate State
health agency or foreign equivalent.
*
*
*
*
*
Dated: April 25, 2011.
David R. Shipman,
Associate Administrator, Agricultural
Marketing Service.
[FR Doc. 2011–10415 Filed 4–28–11; 8:45 am]
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Sfmt 4702
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2011–0318; Directorate
Identifier 2010–CE–033–AD]
RIN 2120–AA64
Airworthiness Directives; Burl A.
Rogers (Type Certificate Previously
Held by William Brad Mitchell and
Aeronca, Inc.) Models 15AC and
S15AC Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM); Extension of the comment
period.
AGENCY:
This document extends the
period for public comment on the
above-referenced NPRM. The proposed
AD would require repetitive inspections
of the upper and lower main wing spar
cap angles for cracks and/or corrosion
and installing inspection access panels.
The proposed AD would also require
replacing the wing spar cap angles if
moderate or severe corrosion is found
and applying corrosion inhibitor. The
proposed AD was prompted by reports
of intergranular exfoliation and
corrosion of the upper and/or lower
wing main spar cap angles found on the
affected airplanes. We are proposing
this AD to detect and correct cracks,
intergranular exfoliation and corrosion
in the wing main spar cap angles, which
could result in reduced strength of the
wing spar and the load carrying capacity
of the wing. This could lead to wing
failure and consequent loss of control.
This extension of the comment period is
necessary to assure that all interested
persons have ample opportunity to
present their views on the proposed
requirements of the NPRM.
DATES: We must receive comments on
this proposed AD by July 3, 2011. The
comment due date is being extended
from May 19, 2011.
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.
• 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: U.S. Department of
Transportation, Docket Operations,
M–30, West Building Ground Floor,
Room W12–140, 1200 New Jersey
Avenue, SE., Washington, DC 20590,
SUMMARY:
E:\FR\FM\29APP1.SGM
29APP1
Federal Register / Vol. 76, No. 83 / Friday, April 29, 2011 / Proposed Rules
between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays.
For service information identified in
this proposed AD, contact Burl’s
Aircraft, LLC, P.O. Box 671487,
Chugiak, Alaska 99567–1487; phone:
(907) 688–3715; fax (907) 688–5031;
e-mail burl@biginalaska.com; Internet:
https://www.burlac.com. You may
review copies of the referenced service
information at the FAA, Small Airplane
Directorate, 901 Locust, Room 301,
Kansas City, MO 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; 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 proposed AD, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Office
(phone: 800–647–5527) is in the
ADDRESSES section. Comments will be
available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Eric
Wright, Aerospace Engineer, FAA,
Anchorage Aircraft Certification Office,
222 W. 7th Ave., #14, Anchorage,
Alaska 99513; telephone: (907) 271–
2648; fax: (907) 271–6365; e-mail:
eric.wright@faa.gov.
SUPPLEMENTARY INFORMATION:
emcdonald on DSK2BSOYB1PROD with PROPOSALS
Comments Invited
We invite you to send any written
relevant data, views, or arguments about
this proposed AD. Send your comments
to an address listed under the
ADDRESSES section. Include ‘‘Docket No.
FAA–2011–0318; Directorate Identifier
2010–CE–033–AD’’ at the beginning of
your comments. We specifically invite
comments on the overall regulatory,
economic, environmental, and energy
aspects of this proposed AD. We will
consider all comments received by the
closing date and may amend this
proposed AD because of those
comments.
We will post all comments we
receive, without change, to https://
www.regulations.gov, including any
personal information you provide. We
will also post a report summarizing each
substantive verbal contact we receive
about this proposed AD.
Discussion
FAA’s Determination
We have considered the request and
find it appropriate to extend the
comment period to give all interested
persons additional time to examine all
data and the proposed requirements of
the NPRM and submit comments. We
determined that extending the comment
period to 90 days will not compromise
the safety of these airplanes.
The comment period for Docket No.
FAA–2011–0318; Directorate Identifier
2010–CE–033–AD is hereby extended to
July 3, 2011.
Since no portion of the NPRM or
other regulatory information has been
changed, the entire NPRM is not being
republished.
Issued in Kansas City, Missouri, on April
22, 2011.
John Colomy,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2011–10383 Filed 4–28–11; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2011–0436; Directorate
Identifier 2011–CE–009–AD]
RIN 2120–AA64
Airworthiness Directives; Hawker
Beechcraft Corporation Models B300
and B300C (C–12W) Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking
(NPRM).
AGENCY:
We propose to adopt a new
airworthiness directive (AD) for the
products listed above. This proposed
AD would require inserting an update to
SUMMARY:
We issued an NPRM to amend 14 CFR
part 39 to include an airworthiness
directive (AD) that would apply to all
VerDate Mar<15>2010
Burl A. Rogers (type certificate
previously held by William Brad
Mitchell and Aeronca, Inc.) Models
15AC and S15AC airplanes. The NPRM
published in the Federal Register on
April 4, 2011 (76 FR 18454). The NPRM
proposed to require repetitive
inspections of the upper and lower main
wing spar cap angles for cracks and/or
corrosion and installing inspection
access panels. The NPRM also proposed
to require replacing the wing spar cap
angles if moderate or severe corrosion is
found and applying corrosion inhibitor.
Since we issued the NPRM, we
received a request to extend the
comment period of the NPRM to 90
days.
17:59 Apr 28, 2011
Jkt 223001
PO 00000
Frm 00008
Fmt 4702
Sfmt 4702
23921
the performance charts in the FAAapproved airplane flight manual and the
pilot’s operating handbook, part number
(P/N) 130–590031–245. This proposed
AD was prompted by an error found in
the take-off speeds and field lengths
published in the FAA-approved
airplane flight manual. We are
proposing this AD to correct the
published data in the airplane flight
manual and the pilot’s operating
handbook and ensure it corresponds
with the published data in the pilot’s
checklist. This condition, if not
corrected, could result in a pilot taking
off from shorter runways than required
by the airplane if the airplane loses an
engine after takeoff decision speed (V1).
This could result in the airplane
running out of runway before take-off
can be accomplished.
DATES: We must receive comments on
this proposed AD by June 13, 2011.
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.
• 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 proposed AD, contact Hawker
Beechcraft Corporation, 9709 East
Central, Wichita, Kansas 67201;
telephone: (316) 676–5034; fax: (316)
676–6614; Internet: https://
www.hawkerbeechcraft.com/
service_support/pubs/. You may review
copies of the referenced service
information at the FAA, Small Airplane
Directorate, 901 Locust, Kansas City,
MO 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; 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 proposed AD, the
regulatory evaluation, any comments
received, and other information. The
street address for the Docket Office
(phone: 800–647–5527) is in the
ADDRESSES section. Comments will be
available in the AD docket shortly after
receipt.
E:\FR\FM\29APP1.SGM
29APP1
Agencies
[Federal Register Volume 76, Number 83 (Friday, April 29, 2011)]
[Proposed Rules]
[Pages 23920-23921]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2011-10383]
=======================================================================
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2011-0318; Directorate Identifier 2010-CE-033-AD]
RIN 2120-AA64
Airworthiness Directives; Burl A. Rogers (Type Certificate
Previously Held by William Brad Mitchell and Aeronca, Inc.) Models 15AC
and S15AC Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of proposed rulemaking (NPRM); Extension of the comment
period.
-----------------------------------------------------------------------
SUMMARY: This document extends the period for public comment on the
above-referenced NPRM. The proposed AD would require repetitive
inspections of the upper and lower main wing spar cap angles for cracks
and/or corrosion and installing inspection access panels. The proposed
AD would also require replacing the wing spar cap angles if moderate or
severe corrosion is found and applying corrosion inhibitor. The
proposed AD was prompted by reports of intergranular exfoliation and
corrosion of the upper and/or lower wing main spar cap angles found on
the affected airplanes. We are proposing this AD to detect and correct
cracks, intergranular exfoliation and corrosion in the wing main spar
cap angles, which could result in reduced strength of the wing spar and
the load carrying capacity of the wing. This could lead to wing failure
and consequent loss of control. This extension of the comment period is
necessary to assure that all interested persons have ample opportunity
to present their views on the proposed requirements of the NPRM.
DATES: We must receive comments on this proposed AD by July 3, 2011.
The comment due date is being extended from May 19, 2011.
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.
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: U.S. Department of Transportation, Docket
Operations, M-30, West Building Ground Floor, Room W12-140, 1200 New
Jersey Avenue, SE., Washington, DC 20590,
[[Page 23921]]
between 9 a.m. and 5 p.m., Monday through Friday, except Federal
holidays.
For service information identified in this proposed AD, contact
Burl's Aircraft, LLC, P.O. Box 671487, Chugiak, Alaska 99567-1487;
phone: (907) 688-3715; fax (907) 688-5031; e-mail burl@biginalaska.com;
Internet: https://www.burlac.com. You may review copies of the
referenced service information at the FAA, Small Airplane Directorate,
901 Locust, Room 301, Kansas City, MO 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; 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 proposed AD, the regulatory
evaluation, any comments received, and other information. The street
address for the Docket Office (phone: 800-647-5527) is in the ADDRESSES
section. Comments will be available in the AD docket shortly after
receipt.
FOR FURTHER INFORMATION CONTACT: Eric Wright, Aerospace Engineer, FAA,
Anchorage Aircraft Certification Office, 222 W. 7th Ave., 14,
Anchorage, Alaska 99513; telephone: (907) 271-2648; fax: (907) 271-
6365; e-mail: eric.wright@faa.gov.
SUPPLEMENTARY INFORMATION:
Comments Invited
We invite you to send any written relevant data, views, or
arguments about this proposed AD. Send your comments to an address
listed under the ADDRESSES section. Include ``Docket No. FAA-2011-0318;
Directorate Identifier 2010-CE-033-AD'' at the beginning of your
comments. We specifically invite comments on the overall regulatory,
economic, environmental, and energy aspects of this proposed AD. We
will consider all comments received by the closing date and may amend
this proposed AD because of those comments.
We will post all comments we receive, without change, to https://www.regulations.gov, including any personal information you provide. We
will also post a report summarizing each substantive verbal contact we
receive about this proposed AD.
Discussion
We issued an NPRM to amend 14 CFR part 39 to include an
airworthiness directive (AD) that would apply to all Burl A. Rogers
(type certificate previously held by William Brad Mitchell and Aeronca,
Inc.) Models 15AC and S15AC airplanes. The NPRM published in the
Federal Register on April 4, 2011 (76 FR 18454). The NPRM proposed to
require repetitive inspections of the upper and lower main wing spar
cap angles for cracks and/or corrosion and installing inspection access
panels. The NPRM also proposed to require replacing the wing spar cap
angles if moderate or severe corrosion is found and applying corrosion
inhibitor.
Since we issued the NPRM, we received a request to extend the
comment period of the NPRM to 90 days.
FAA's Determination
We have considered the request and find it appropriate to extend
the comment period to give all interested persons additional time to
examine all data and the proposed requirements of the NPRM and submit
comments. We determined that extending the comment period to 90 days
will not compromise the safety of these airplanes.
The comment period for Docket No. FAA-2011-0318; Directorate
Identifier 2010-CE-033-AD is hereby extended to July 3, 2011.
Since no portion of the NPRM or other regulatory information has
been changed, the entire NPRM is not being republished.
Issued in Kansas City, Missouri, on April 22, 2011.
John Colomy,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2011-10383 Filed 4-28-11; 8:45 am]
BILLING CODE 4910-13-P