Policy for Repair and Alteration of Rotating Turbine Engine Life Limited Parts, 59801 [05-20457]
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Federal Register / Vol. 70, No. 197 / Thursday, October 13, 2005 / Notices
Alternative One—Sponsor’s Proposed
Action: Relocate Runway 11R/29L, 450
feet to the southwest, creating a
centerline separation of 1,156 feet
between the existing Runway 11L/29R
and the relocated Runway 11R/29L. The
relocated Runway 11R/29L will be
11,000 feet long by 150 feet wide. The
relocation of Runway 11R/29L will
include construction of a parallel and
connecting taxiway system, and
associated navigational aids.
Alternative Two—Alternative Airfield
Development at Tucson: Extending and
upgrading the current general aviation
Runway 11R/29L to an air carrier
runway, maintaining a 700-foot
centerline separation between the
current air carrier Runway 11L/29R and
the extended and upgraded runway
11R/29L, and
Alternative 3—Relocating and
upgrading the general aviation Runway
11R/29L, to an air carrier runway, 2,500
feet south of Runway 11L/29R and
converting the current runway 11R/29L
to a parallel taxiway that would serve
both runways, and
Alternative 4—Relocating and
upgrading the general aviation Runway
11R/29L to an air carrier runway, 1,156
feet south of Runway 11L/29R, and
converting the runway to a parallel
taxiway that would serve both runways.
This alternative incorporates a localizer
directional aide (LDA) approach.
These airfield development
alternatives identified under Alternative
2, 3 and four would likely include
several of the support features of
Alternative One, including taxiway
improvements and associated
navigational aids. The specific details of
the alternative airfield development at
Tucson International Airport will be
refined following the scoping process
during the preparation of the EIS.
Alternative Five—Use of Other
Existing Airports: The possible use of
other existing area airports including,
but not limited to, Ryan Airfield and
Marana Regional Airport will be
evaluated.
Alternative Six—Use of Other Modes
of Transportation: Use of intercity bus
line, rail, and automobile transportation
will be evaluated.
Alternative Seven—No Action
Alternative: Under this alternative, the
existing airport would remain
unchanged. Runway 11R/29L would
remain in its current configuration.
Comments and suggestions are invited
from Federal, State and local agencies,
and other interested parties to ensure
that the full range of issues related to
these proposed projects are addressed
and all significant issues are identified.
Written comments and suggestions may
VerDate Aug<31>2005
16:14 Oct 12, 2005
Jkt 208001
be mailed to the FAA informational
contact listed above and must be
received no later than 5:00 p.m. Pacific
Standard Time, December 15, 2005.
Scoping Meetings: The FAA will hold
one (1) public and one (1) governmental
agency scoping meeting to solicit input
from the public and various Federal,
State and local agencies having
jurisdiction or having specific expertise
with respect to any environmental
impacts associated with the proposed
projects. The public scoping meeting
will be held on Tuesday, November 15,
2005, in the Tucson Airport Authority
Boardroom at 7005 South Plumer
Avenue, Tucson, Arizona 85706. The
meeting will be held from 4 p.m. to 7
p.m. Mountain Standard Time (MST). A
scoping meeting will be held
specifically for governmental agencies
on the same day at the same location
from 10 a.m. to 12 p.m. MST.
Issued in Hawthorne, California on
Tuesday, October 4, 2005.
Mark A. McClardy,
Manager, Airports Division, Western-Pacific,
Region AWP–600.
[FR Doc. 05–20461 Filed 10–12–05; 8:45 am]
BILLING CODE 4910–13–M
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
[Proposed Policy Statement No. ANE–200X–
33.3–X]
Policy for Repair and Alteration of
Rotating Turbine Engine Life Limited
Parts
Federal Aviation
Administration, DOT.
ACTION: Notice of availability for
proposed policy statement; request for
comments.
AGENCY:
SUMMARY: The Federal Aviation
Administration (FAA) announces the
availability of proposed policy for the
repair and alteration of rotating turbine
engine-life limited parts (RTE–LLPs).
This proposed policy establishes that
the FAA will treat all repairs and
alterations of RTE–LLPs as major repairs
and major alterations. We are also
proposing that all RTE–LLP repair and
alteration data must include a
methodology to assess the life of the
repaired or altered part and the
continued operational safety of the
repaired product. This proposed policy
provides guidance for: (1) Technical
substantiation for repair or alteration of
RTE–LLPs; and (2) Aircraft Certification
Offices (ACOs) and Designated
Engineering Representatives to evaluate
and approve repair and alteration data.
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59801
Comments must be received by
November 14, 2005.
DATES:
Send all comments on the
proposed policy to the individual
identified under FOR FURTHER
INFORMATION CONTACT.
ADDRESSES:
FOR FURTHER INFORMATION CONTACT:
Karen M. Grant, FAA, Engine and
Propeller Standards Staff, ANE–110, 12
New England Executive Park,
Burlington, MA 01803; e-mail:
karen.m.grant@faa.gov; telephone (781)
238–7119; fax: (781) 238–7199.
SUPPLEMENTARY INFORMATION:
Comments Invited: The proposed
policy is available on the Internet at the
following address: https://www.faa.gov/
aircraft/draft_docs/. If you do not have
access to the Internet, you may request
a copy by contacting the individual
listed under FOR FURTHER INFORMATION
CONTACT. The FAA invites interested
parties to comment on the proposed
policy. Comments should identify the
subject of the proposed policy and be
submitted to the individual identified
under FOR FURTHER INFORMATION
CONTACT. The FAA will consider all
comments received by the closing date
before issuing the final policy.
We will file in the docket all
comments received, as well as a report
summarizing each substantive public
contact with FAA personnel concerning
this proposed policy. The docket is
available for public inspection before
and after the comment date. If you wish
to review the docket in person, go to the
above address between 9 a.m. and 5
p.m., Monday through Friday, except
Federal holidays.
Background: During the past year, we
reviewed the technical data for
numerous RTE–LLP repairs. We
observed deficiencies in the data for
many of these repairs. We also noted
that may repairs were improperly
assessed as minor and were not properly
coordinated with the appropriate ACOs.
This proposed policy would provide
guidance on the coordination and the
technical data needed for RTE–LLP
repairs and alterations.
(Authority: 49 U.S.C. 106(g), 40113, 44701–
44702, 44704).
Issued in Burlington, Massachusetts, on
October 3, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller
Directorate, Aircraft Certification Service.
[FR Doc. 05–20457 Filed 10–12–05; 8:45 am]
BILLING CODE 4910–13–M
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13OCN1
Agencies
[Federal Register Volume 70, Number 197 (Thursday, October 13, 2005)]
[Notices]
[Page 59801]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-20457]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
[Proposed Policy Statement No. ANE-200X-33.3-X]
Policy for Repair and Alteration of Rotating Turbine Engine Life
Limited Parts
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of availability for proposed policy statement; request
for comments.
-----------------------------------------------------------------------
SUMMARY: The Federal Aviation Administration (FAA) announces the
availability of proposed policy for the repair and alteration of
rotating turbine engine-life limited parts (RTE-LLPs). This proposed
policy establishes that the FAA will treat all repairs and alterations
of RTE-LLPs as major repairs and major alterations. We are also
proposing that all RTE-LLP repair and alteration data must include a
methodology to assess the life of the repaired or altered part and the
continued operational safety of the repaired product. This proposed
policy provides guidance for: (1) Technical substantiation for repair
or alteration of RTE-LLPs; and (2) Aircraft Certification Offices
(ACOs) and Designated Engineering Representatives to evaluate and
approve repair and alteration data.
DATES: Comments must be received by November 14, 2005.
ADDRESSES: Send all comments on the proposed policy to the individual
identified under FOR FURTHER INFORMATION CONTACT.
FOR FURTHER INFORMATION CONTACT: Karen M. Grant, FAA, Engine and
Propeller Standards Staff, ANE-110, 12 New England Executive Park,
Burlington, MA 01803; e-mail: karen.m.grant@faa.gov; telephone (781)
238-7119; fax: (781) 238-7199.
SUPPLEMENTARY INFORMATION:
Comments Invited: The proposed policy is available on the Internet
at the following address: https://www.faa.gov/aircraft/draft_docs/. If
you do not have access to the Internet, you may request a copy by
contacting the individual listed under FOR FURTHER INFORMATION CONTACT.
The FAA invites interested parties to comment on the proposed policy.
Comments should identify the subject of the proposed policy and be
submitted to the individual identified under FOR FURTHER INFORMATION
CONTACT. The FAA will consider all comments received by the closing
date before issuing the final policy.
We will file in the docket all comments received, as well as a
report summarizing each substantive public contact with FAA personnel
concerning this proposed policy. The docket is available for public
inspection before and after the comment date. If you wish to review the
docket in person, go to the above address between 9 a.m. and 5 p.m.,
Monday through Friday, except Federal holidays.
Background: During the past year, we reviewed the technical data
for numerous RTE-LLP repairs. We observed deficiencies in the data for
many of these repairs. We also noted that may repairs were improperly
assessed as minor and were not properly coordinated with the
appropriate ACOs. This proposed policy would provide guidance on the
coordination and the technical data needed for RTE-LLP repairs and
alterations.
(Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704).
Issued in Burlington, Massachusetts, on October 3, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 05-20457 Filed 10-12-05; 8:45 am]
BILLING CODE 4910-13-M