Airworthiness Directives; Mitsubishi Heavy Industries, Ltd. Various Models MU-2B Airplanes, 71353 [2010-29463]
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Federal Register / Vol. 75, No. 225 / Tuesday, November 23, 2010 / Rules and Regulations
effective date of this AD, unless the actions
have already been done.
Federal Aviation Administration
One-Time Visual Inspection of the No. 3
Bearing Oil Pressure Tube
(f) Perform a one-time visual inspection of
the exterior of the No. 3 bearing oil pressure
tube for cracks and evidence of being
repaired.
(1) Remove the tube from service if any
cracks are found.
(2) Remove the tube from service if found
repaired, or if suspected that the tube was
repaired.
(g) After the effective date of this AD, do
not install any repaired No. 3 bearing oil
pressure tube into any engine.
(h) Guidance on the No. 3 bearing oil
pressure tube visual inspection can be found
in:
(1) Pratt & Whitney Clean, Inspect, Repair
Manual PN 51A357, 72–41–20 for PW4000–
94’’ and PW4000–100’’ series engines; or
(2) Pratt & Whitney Clean, Inspect, Repair
Manual PN 51A750, 72–41–20 for PW4000–
112’’ series engines.
Definitions
(i) For the purpose of this AD, piece part
condition means that the part is completely
disassembled from the engine as specified in
the disassembly instructions in the
manufacturer’s engine manual.
Alternative Methods of Compliance
(j) The Manager, Engine Certification
Office, FAA, may approve alternative
methods of compliance for this AD, if
requested using the procedures found in 14
CFR 39.19.
Related Information
(k) For more information about this AD,
contact James Gray, Aerospace Engineer,
Engine Certification Office, FAA, Engine and
Propeller Directorate, 12 New England
Executive Park, Burlington, MA 01803;
telephone (781) 238–7742; fax (781) 238–
7199; e-mail: james.e.gray@faa.gov.
Material Incorporated by Reference
(l) None.
Issued in Burlington, Massachusetts, on
November 16, 2010.
Robert G. Mann,
Acting Manager, Engine & Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 2010–29451 Filed 11–22–10; 8:45 am]
mstockstill on DSKH9S0YB1PROD with RULES
BILLING CODE 4910–13–P
DEPARTMENT OF TRANSPORTATION
14 CFR Part 39
[Docket No. FAA–2009–1076; Directorate
Identifier 2009–CE–019–AD; Amendment
39–16296; AD 2010–10–17]
RIN 2120–AA64
Airworthiness Directives; Mitsubishi
Heavy Industries, Ltd. Various Models
MU–2B Airplanes
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule; correction.
AGENCY:
The FAA is correcting an
airworthiness directive (AD) that has
published in the Federal Register. That
AD applies to the products listed above.
The reissue date of September 24, 1986,
of the MU–2B–60 airplane flight manual
(AFM) in table 3 of the Compliance
section (e)(1)(i) is incorrect, in that it is
‘‘September 24, 1985,’’ instead of
‘‘September 24, 1986.’’ This document
corrects this error. In all other respects,
the original document remains the
same.
SUMMARY:
This final rule; correction is
effective November 23, 2010. The
effective date for AD 2010–10–17
remains July 22, 2010.
ADDRESSES: 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: Matt
Bryant, Propulsion Engineer, FAA, Fort
Worth ACO, 2601 Meacham Blvd., Fort
Worth, Texas 76137; telephone: (817)
222–5146; fax: (817) 222–5960; e-mail:
matthew.a.bryant@faa.gov.
DATES:
SUPPLEMENTARY INFORMATION:
Airworthiness Directive 2010–10–17,
amendment 39–16296 (75 FR 34349),
which supersedes Airworthiness
Directive (AD) 2006–17–01, AD 2006–
15–07, AD 2000–02–25, and AD 97–25–
02, currently retains from AD 2006–17–
01 the inspection of the engine torque
indication system and possible
recalibration of the torque pressure
VerDate Mar<15>2010
19:35 Nov 22, 2010
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71353
transducers and requires incorporating
all revisions up to and including the
latest revisions of the AFM for certain
MHI various Models MU–2B airplanes.
As published, table 3 specific to the
MHI MU–2B–60 airplane stating that the
MU–2B–60 AFM has a reissued date of
September 24, 1986, in the Compliance
section (e) is incorrect, in that it is
‘‘September 24, 1985,’’ instead of
‘‘September 24, 1986.’’
No other part of the preamble or
regulatory information has been
changed; therefore, only the changed
portion of the final rule is being
published in the Federal Register.
The effective date of this AD remains
July 22, 2010.
Correction of Regulatory Text
§ 39.13
[Corrected]
In the Federal Register of June 17,
2010, AD 2010–10–17; Amendment
39–16296 is corrected as follows:
On page 34352, in the Compliance
section paragraph (e)(1)(i) in table 3,
under the third column ‘‘Date and
version of AFM,’’ change the AFM,
Section 6, Reissued date ‘‘September 24,
1986,’’ to ‘‘September 24, 1985.’’
■
Issued in Kansas City, Missouri, on
November 17, 2010.
Patrick R. Mullen,
Acting Manager, Small Airplane Directorate,
Aircraft Certification Service.
[FR Doc. 2010–29463 Filed 11–22–10; 8:45 am]
BILLING CODE 4910–13–P
DEPARTMENT OF JUSTICE
28 CFR Part 26
[Docket No. OJP 1464; AG Order No.]
RIN 1121–AA76
Office of the Attorney General;
Certification Process for State Capital
Counsel Systems; Removal of Final
Rule
Department of Justice.
Final rule.
AGENCY:
ACTION:
Pursuant to the USA
PATRIOT Improvement and
Reauthorization Act of 2005, the
Department of Justice promulgated a
final rule to implement certification
procedures for States seeking to qualify
for the special federal habeas corpus
review procedures in capital cases. A
Federal district court issued an
injunction requiring the Department to
provide an additional public comment
period and publish a response to any
comments received during that period.
The Department then solicited further
SUMMARY:
E:\FR\FM\23NOR1.SGM
23NOR1
]]>Agencies
[Federal Register Volume 75, Number 225 (Tuesday, November 23, 2010)]
[Rules and Regulations]
[Page 71353]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 2010-29463]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2009-1076; Directorate Identifier 2009-CE-019-AD;
Amendment 39-16296; AD 2010-10-17]
RIN 2120-AA64
Airworthiness Directives; Mitsubishi Heavy Industries, Ltd.
Various Models MU-2B Airplanes
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: The FAA is correcting an airworthiness directive (AD) that has
published in the Federal Register. That AD applies to the products
listed above. The reissue date of September 24, 1986, of the MU-2B-60
airplane flight manual (AFM) in table 3 of the Compliance section
(e)(1)(i) is incorrect, in that it is ``September 24, 1985,'' instead
of ``September 24, 1986.'' This document corrects this error. In all
other respects, the original document remains the same.
DATES: This final rule; correction is effective November 23, 2010. The
effective date for AD 2010-10-17 remains July 22, 2010.
ADDRESSES: 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: Matt Bryant, Propulsion Engineer, FAA,
Fort Worth ACO, 2601 Meacham Blvd., Fort Worth, Texas 76137; telephone:
(817) 222-5146; fax: (817) 222-5960; e-mail: matthew.a.bryant@faa.gov.
SUPPLEMENTARY INFORMATION: Airworthiness Directive 2010-10-17,
amendment 39-16296 (75 FR 34349), which supersedes Airworthiness
Directive (AD) 2006-17-01, AD 2006-15-07, AD 2000-02-25, and AD 97-25-
02, currently retains from AD 2006-17-01 the inspection of the engine
torque indication system and possible recalibration of the torque
pressure transducers and requires incorporating all revisions up to and
including the latest revisions of the AFM for certain MHI various
Models MU-2B airplanes.
As published, table 3 specific to the MHI MU-2B-60 airplane stating
that the MU-2B-60 AFM has a reissued date of September 24, 1986, in the
Compliance section (e) is incorrect, in that it is ``September 24,
1985,'' instead of ``September 24, 1986.''
No other part of the preamble or regulatory information has been
changed; therefore, only the changed portion of the final rule is being
published in the Federal Register.
The effective date of this AD remains July 22, 2010.
Correction of Regulatory Text
Sec. 39.13 [Corrected]
0
In the Federal Register of June 17, 2010, AD 2010-10-17; Amendment 39-
16296 is corrected as follows:
On page 34352, in the Compliance section paragraph (e)(1)(i) in
table 3, under the third column ``Date and version of AFM,'' change the
AFM, Section 6, Reissued date ``September 24, 1986,'' to ``September
24, 1985.''
Issued in Kansas City, Missouri, on November 17, 2010.
Patrick R. Mullen,
Acting Manager, Small Airplane Directorate, Aircraft Certification
Service.
[FR Doc. 2010-29463 Filed 11-22-10; 8:45 am]
BILLING CODE 4910-13-P
