Airworthiness Directives; Rolls-Royce Corporation (formerly Allison Engine Company, Allison Gas Turbine Division, and Detroit Diesel Allison) Models 250-C28, -C28B, and -C28C Turboshaft Engines; Correction, 46754 [05-15896]
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46754
Federal Register / Vol. 70, No. 154 / Thursday, August 11, 2005 / Rules and Regulations
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA–2004–18538; Directorate
Identifier 2004–NE–29–AD; Amendment 39–
13711; AD 2004–14–02]
RIN 2120–AA64
corrected to read ‘‘manufactured and
inadvertently accepted with a blueprint
variance’’.
Issued in Burlington, MA, on August 4,
2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate,
Aircraft Certification Service.
[FR Doc. 05–15896 Filed 8–10–05; 8:45 am]
BILLING CODE 4910–13–P
Airworthiness Directives; Rolls-Royce
Corporation (formerly Allison Engine
Company, Allison Gas Turbine
Division, and Detroit Diesel Allison)
Models 250–C28, –C28B, and –C28C
Turboshaft Engines; Correction
Federal Aviation
Administration, DOT.
ACTION: Final rule; correction.
AGENCY:
13:55 Aug 10, 2005
Jkt 205001
Federal Aviation Administration
14 CFR Part 71
[Docket No. FAA–2004–18612; Airspace
Docket No. 04–AWA–05]
SUMMARY: This document makes a
correction to Airworthiness Directive
(AD) 2004–14–02. That AD applies to
Rolls-Royce Corporation (formerly
Allison Engine Company, Allison Gas
Turbine Division, and Detroit Diesel
Allison) models 250–C28, –C28B, and
–C28C turboshaft engines with certain
serial number (SN) third-stage turbine
wheels, part number (P/N) 6899383. We
published AD 2004–14–02 in the
Federal Register on July 9, 2004 (69 FR
41389). The SUMMARY and the
SUPPLEMENTAL INFORMATION paragraphs
each have a sentence that is not clear.
This document corrects these two
sentences. In all other respects, the
original document remains the same.
DATES: Effective August 11, 2005.
FOR FURTHER INFORMATION CONTACT: John
Tallarovic, Aerospace Engineer, Chicago
Aircraft Certification Office, FAA, 2300
East Devon Avenue, Des Plaines, IL
60018–4696; telephone (847) 294–8180;
fax (847) 294–7834.
SUPPLEMENTARY INFORMATION: A final
rule; request for comments AD, FR Doc.
04–15508, that applies to Rolls-Royce
Corporation (formerly Allison Engine
Company, Allison Gas Turbine Division,
and Detroit Diesel Allison) models 250–
C28, –C28B, and –C28C turboshaft
engines with certain SN third-stage
turbine wheels, P/N 6899383, was
published in the Federal Register on
July 9, 2004, (69 FR 41389). The
following corrections are needed:
I On page 41390, in the first column, in
the SUMMARY, in the twelfth line, ‘‘before
reaching new reduced life limits’’ is
corrected to read ‘‘before the new
reduced life limits for these turbine
wheels are reached’’.
I On page 41390, in the first column, in
the SUPPLEMENTARY INFORMATION, in the
twelfth line, ‘‘manufactured and
accepted with a blueprint variance’’ is
VerDate jul<14>2003
DEPARTMENT OF TRANSPORTATION
RIN 2120–AA66
Modification of the Los Angeles Class
B Airspace Area; CA
Federal Aviation
Administration (FAA), DOT.
ACTION: Final rule.
AGENCY:
SUMMARY: This action modifies the Los
Angeles (LAX), CA, Class B airspace.
Specifically, this action expands the
eastern boundary of the airspace to
ensure containment of the LAX
Standard Terminal Arrival Routes
(STAR), and correct the inefficiencies of
several existing areas identified during
public meetings and Southern California
TRACON (SCT) reviews of the airspace.
The FAA is taking this action to
improve the flow of air traffic, enhance
safety, and reduce the potential for
midair collision in the LAX Class B
airspace, while accommodating the
concerns of airspace users. Further, this
effort supports the FAA’s national
airspace redesign goal of optimizing
terminal and en route airspace to reduce
aircraft delays and improve system
capacity.
EFFECTIVE DATE:
0901 UTC, December
22, 2005.
Ken
McElroy, Airspace and Rules, Office of
System Operations and Safety, Federal
Aviation Administration, 800
Independence Avenue, SW.,
Washington, DC 20591; telephone: (202)
267–8783.
SUPPLEMENTARY INFORMATION:
FOR FURTHER INFORMATION CONTACT:
Background
On March 24, 2005, the FAA
published in the Federal Register a
notice of proposed rulemaking to
modify the LAX Class B airspace area
(70 FE 15022). The FAA proposed this
action to improve several areas where
PO 00000
Frm 00012
Fmt 4700
Sfmt 4700
boundary locations and identification
could be enhanced, and modified
several areas to ensure the containment
of arrivals within the LAX Class B
airspace. Interested parties were invited
to participate in this rulemaking effort
by submitting written comments on the
proposal. In response to the notice, the
FAA received four written comments.
All comments received were considered
before making a determination on the
final rule. An analysis of the comments
received and the FAA’s responses are
summarized in the ‘‘Discussion of
Comments’’ section.
Discussion of Comments
The Aircraft Owners and Pilots
Association (AOPA) cited the work of
the Southern California Airspace User
Working Group (SCAUWG) and the
collaborative efforts of the FAA in
developing this rule. They pointed out
that the overall modifications will prove
beneficial to the general aviation
community and result in a reduction of
approximately 100 square miles of
existing Class B airspace.
The Airline Pilots Association,
International endorsed the proposal
stating ‘‘This is a significant
improvement to the current Class B
airspace.’’
The FAA agrees with these comments.
The modifications will improve the flow
of air traffic, enhance safety, and reduce
the potential for midair collision in the
LAX Class B airspace, while
accommodating the concerns of airspace
users.
One commenter stated it would be
helpful for General Aviation pilots if the
FAA reinstated (with multiple altitudes)
a shoreline transition, so that we don’t
have to lose Flight following to transit
LAX airspace, and then re-establish it
on the other side. The commenter
stated, ‘‘I think it would decrease the
workload for both pilots and controllers,
and increase safety.’’
The FAA agrees. In concert with the
SCAUWG, the Shoreline Route has been
redesigned to allow uninterrupted
transitions where pilots can retain
Flight Following at all times. This
change should become effective on or
before the revised LAX Class B airspace
becomes effective.
One commenter suggested the FAA
use approach and climb corridors, and
eliminate the need for taking 3000
square miles away from general aviation
to free an airport from traffic.
The FAA does not agree. If the FAA
adopted a rule in which only approach
and climb corridors were used in the
LAX Class B airspace, it would result in
a reduced air traffic control capability to
maintain an efficient flow of air traffic
E:\FR\FM\11AUR1.SGM
11AUR1
]]>Agencies
[Federal Register Volume 70, Number 154 (Thursday, August 11, 2005)]
[Rules and Regulations]
[Page 46754]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-15896]
[[Page 46754]]
-----------------------------------------------------------------------
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
14 CFR Part 39
[Docket No. FAA-2004-18538; Directorate Identifier 2004-NE-29-AD;
Amendment 39-13711; AD 2004-14-02]
RIN 2120-AA64
Airworthiness Directives; Rolls-Royce Corporation (formerly
Allison Engine Company, Allison Gas Turbine Division, and Detroit
Diesel Allison) Models 250-C28, -C28B, and -C28C Turboshaft Engines;
Correction
AGENCY: Federal Aviation Administration, DOT.
ACTION: Final rule; correction.
-----------------------------------------------------------------------
SUMMARY: This document makes a correction to Airworthiness Directive
(AD) 2004-14-02. That AD applies to Rolls-Royce Corporation (formerly
Allison Engine Company, Allison Gas Turbine Division, and Detroit
Diesel Allison) models 250-C28, -C28B, and -C28C turboshaft engines
with certain serial number (SN) third-stage turbine wheels, part number
(P/N) 6899383. We published AD 2004-14-02 in the Federal Register on
July 9, 2004 (69 FR 41389). The SUMMARY and the SUPPLEMENTAL
INFORMATION paragraphs each have a sentence that is not clear. This
document corrects these two sentences. In all other respects, the
original document remains the same.
DATES: Effective August 11, 2005.
FOR FURTHER INFORMATION CONTACT: John Tallarovic, Aerospace Engineer,
Chicago Aircraft Certification Office, FAA, 2300 East Devon Avenue, Des
Plaines, IL 60018-4696; telephone (847) 294-8180; fax (847) 294-7834.
SUPPLEMENTARY INFORMATION: A final rule; request for comments AD, FR
Doc. 04-15508, that applies to Rolls-Royce Corporation (formerly
Allison Engine Company, Allison Gas Turbine Division, and Detroit
Diesel Allison) models 250-C28, -C28B, and -C28C turboshaft engines
with certain SN third-stage turbine wheels, P/N 6899383, was published
in the Federal Register on July 9, 2004, (69 FR 41389). The following
corrections are needed:
0
On page 41390, in the first column, in the SUMMARY, in the twelfth
line, ``before reaching new reduced life limits'' is corrected to read
``before the new reduced life limits for these turbine wheels are
reached''.
0
On page 41390, in the first column, in the SUPPLEMENTARY INFORMATION,
in the twelfth line, ``manufactured and accepted with a blueprint
variance'' is corrected to read ``manufactured and inadvertently
accepted with a blueprint variance''.
Issued in Burlington, MA, on August 4, 2005.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. 05-15896 Filed 8-10-05; 8:45 am]
BILLING CODE 4910-13-P
