Interest Rate Risk Policy and Program, 57990 [C1-2012-2091]
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57990
Federal Register / Vol. 77, No. 182 / Wednesday, September 19, 2012 / Rules and Regulations
pounds; turkeys and all other poultry—
3 pounds.
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Dated: September 13, 2012.
David R. Shipman,
Administrator, Agricultural Marketing
Service.
[FR Doc. 2012–23083 Filed 9–18–12; 8:45 am]
BILLING CODE 3410–02–P
NATIONAL CREDIT UNION
ADMINISTRATION
12 CFR Part 741
RIN 3133–AD66
Interest Rate Risk Policy and Program
Correction
In rule document 2012–02091,
appearing on pages 55155–5167 in the
issue of Thursday, February 2, 2012,
make the following corrections:
1. On page 5157, in the second
column, in the first line, the text entry
‘‘by asset size cohort at year-end 2010,
as depicted in Table 1:’’ is deleted.
2. On page 5164, in the second
column, under the heading ‘‘Account
Attributes’’ on the second line,
‘‘P\principal’’ should read ‘‘Principal’’.
[FR Doc. C1–2012–2091 Filed 9–18–12; 8:45 am]
BILLING CODE 1505–01–D
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2012–0645; Directorate
Identifier 2011–NM–052–AD; Amendment
39–17190; AD 2012–18–13]
Examining the AD Docket
RIN 2120–AA64
Airworthiness Directives; The Boeing
Company Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
We are superseding an
existing airworthiness directive (AD) for
all The Boeing Company Model 737–
100, –200, –200C, –300, –400, and –500
SUMMARY:
series airplanes. That AD currently
requires repetitive inspections to detect
cracking in the web of the aft pressure
bulkhead at body station 1016 at the aft
fastener row attachment to the ‘‘Y’’
chord, and corrective actions if
necessary. This new AD adds various
inspections for discrepancies at the aft
pressure bulkhead, and related
investigative and corrective actions if
necessary. This AD was prompted by
several reports of fatigue cracking at that
location. We are issuing this AD to
detect and correct such fatigue cracking,
which could result in rapid
decompression of the fuselage.
DATES: This AD is effective October 24,
2012.
The Director of the Federal Register
approved the incorporation by reference
of a certain publication listed in the AD
as of October 24, 2012.
The Director of the Federal Register
approved the incorporation by reference
of certain other publications listed in
this AD as of May 10, 1999 (64 FR
19879, April 23, 1999).
ADDRESSES: For service information
identified in this AD, contact Boeing
Commercial Airplanes, Attention: Data
& Services Management, P.O. Box 3707,
MC 2H–65, Seattle, Washington 98124–
2207; telephone 206–544–5000,
extension 1; fax 206–766–5680; Internet
https://www.myboeingfleet.com. You
may review copies of the referenced
service information at the FAA,
Transport Airplane Directorate, 1601
Lind Avenue SW., Renton, Washington.
For information on the availability of
this material at the FAA, call 425–227–
1221.
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:
Alan Pohl, Aerospace Engineer,
Airframe Branch, ANM–120S, FAA,
Seattle Aircraft Certification Office,
1601 Lind Avenue SW., Renton,
Washington 98057–3356; phone: (425)
917–6450; fax: (425) 917–6590; email:
alan.pohl@faa.gov.
SUPPLEMENTARY INFORMATION:
Discussion
We issued a notice of proposed
rulemaking (NPRM) to amend 14 CFR
part 39 to supersede AD 99–08–23,
Amendment 39–11132 (64 FR 19879,
April 23, 1999). That AD applies to the
specified products. The NPRM
published in the Federal Register on
June 28, 2012 (77 FR 38547). That
NPRM proposed to continue to require
repetitive inspections to detect cracking
in the web of the aft pressure bulkhead
at body station 1016 at the aft fastener
row attachment to the ‘‘Y’’ chord, and
corrective actions if necessary. That
NPRM also proposed to require adding
various inspections for discrepancies at
the aft pressure bulkhead, and related
investigative and corrective actions if
necessary.
Comments
We gave the public the opportunity to
participate in developing this AD. We
have considered the comments received.
Boeing supports the NPRM (77 FR
38547, June 28, 2012). Aviation Partners
Boeing stated that it has reviewed the
NPRM and has determined that the
installation of winglets per
supplemental type certificate
ST01219SE does not affect the NPRM.
Conclusion
We reviewed the relevant data,
considered the comments received, and
determined that air safety and the
public interest require adopting the AD
as proposed.
Costs of Compliance
We estimate that this AD affects 566
airplanes of U.S. registry.
We estimate the following costs to
comply with this AD:
srobinson on DSK4SPTVN1PROD with RULES
ESTIMATED COSTS
Action
Labor cost
Low frequency eddy current (LFEC) inspection [retained actions from AD
99-08–23, Amendment 39–11132 (64
FR 19879, April 23, 1999)].
8 work-hours × $85 per hour = $680 .....
VerDate Mar<15>2010
19:23 Sep 18, 2012
Jkt 226001
PO 00000
Frm 00006
Fmt 4700
Parts cost
Sfmt 4700
Cost per product
$0
$680 .......................
E:\FR\FM\19SER1.SGM
19SER1
Cost on U.S.
operators
$384,880.
Agencies
[Federal Register Volume 77, Number 182 (Wednesday, September 19, 2012)]
[Rules and Regulations]
[Page 57990]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: C1-2012-2091]
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NATIONAL CREDIT UNION ADMINISTRATION
12 CFR Part 741
RIN 3133-AD66
Interest Rate Risk Policy and Program
Correction
In rule document 2012-02091, appearing on pages 55155-5167 in the
issue of Thursday, February 2, 2012, make the following corrections:
1. On page 5157, in the second column, in the first line, the text
entry ``by asset size cohort at year-end 2010, as depicted in Table
1:'' is deleted.
2. On page 5164, in the second column, under the heading ``Account
Attributes'' on the second line, ``P\principal'' should read
``Principal''.
[FR Doc. C1-2012-2091 Filed 9-18-12; 8:45 am]
BILLING CODE 1505-01-D