Advisory Circular 33.70-1, Guidance Material for Aircraft Engine Life-Limited Parts Requirements, 45515 [E9-21068]
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Federal Register / Vol. 74, No. 169 / Wednesday, September 2, 2009 / Notices
jlentini on DSKJ8SOYB1PROD with NOTICES
local match: Procurement of rails, ties,
and other specialized equipment; the
procurement of commodities; and
demolition.
FTA reminds project sponsors and the
public that local funds expended by the
project sponsor pursuant to and after the
date of the pre-award authority are
eligible for reimbursement or as credit
toward local match only if FTA later
makes a grant or grant amendment for
the project. Local funds expended by
the project sponsor prior to the date of
the pre-award authority are not eligible
for credit toward local match or
reimbursement.
The above changes to automatic preaward authority are expected to reduce
the need for LONPs. FTA will still
consider LONPs for activities not
covered by automatic pre-award
authority. As a change in administrative
practice, FTA will, following the
completion of the requirements under
NEPA, expedite the issuance of LONPs,
when appropriate, by no longer
performing a detailed review of the cost
and scope of the request in every
instance. Rather, a limited review will
be performed in those cases that are of
a more routine nature, especially those
involving an experienced sponsor.
This change has the following
ramifications. First, an LONP is no
longer an indication by FTA that the
project is a promising candidate for
either an FFGA or PCGA. Second, FTA
is transferring more risk to the project
sponsor. LONPs allow a project sponsor
to incur costs using non-Federal
resources, with the understanding that
the costs incurred subsequent to the
issuance of the LONP may be
reimbursable as eligible expenses or
eligible as credit toward the local match
only if FTA approves the project for
funding at a later date. Federal funding
is not implied or guaranteed by an
LONP. The reduced level of FTA
oversight should expedite the delivery
of New Starts and Small Starts projects,
but will also require increased diligence
on the part of project sponsors to ensure
that public funds are expended wisely.
Peter M. Rogoff,
Administrator, Federal Transit
Administration.
[FR Doc. E9–21173 Filed 9–1–09; 8:45 am]
BILLING CODE P
DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Advisory Circular 33.70–1, Guidance
Material for Aircraft Engine LifeLimited Parts Requirements
AGENCY: Federal Aviation
Administration (FAA), DOT.
16:56 Sep 01, 2009
Jkt 217001
This notice announces the
issuance of Advisory Circular (AC)
33.70–1, Guidance Material for Aircraft
Engine Life-limited Parts Requirements.
This AC provides definitions, guidance,
and acceptable methods that may be
used to demonstrate compliance with
the engine life-limited parts integrity
requirements of § 33.70 of Title 14 of the
Code of Federal Regulations. Section
33.70 contains requirements applicable
to the design and life management of
propulsion system life-limited parts
including high-energy rotating parts.
SUMMARY:
DATES: The Engine and Propeller
Directorate issued AC 33.70–1 on July
31, 2009.
FOR FURTHER INFORMATION CONTACT: The
Federal Aviation Administration, Attn:
Timoleon Mouzakis, Engine and
Propeller Standards Staff, ANE–111, 12
New England Executive Park,
Burlington, MA 01803–5299; telephone:
(781) 238–7114; fax: (781) 238–7199;
e-mail: timoleon.mouzakis@faa.gov.
We have filed in the docket all
substantive comments received, and a
report summarizing them. If you wish to
review the docket in person, you may go
to the above address between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. If you wish to contact
the above individual directly, you can
use the above telephone number or
e-mail address provided.
How to Obtain Copies: A paper copy
of AC 33.70–1 may be obtained by
writing to the U.S. Department of
Transportation, Subsequent Distribution
Office, DOT Warehouse, SVC–121.23,
Ardmore East Business Center, 3341Q
75th Ave., Landover, MD 20785,
telephone 301–322–5377, or by faxing
your request to the warehouse at 301–
386–5394. The AC will also be available
on the Internet at https://www.faa.gov/
regulations_policies (then click on
‘‘Advisory Circulars’’).
PO 00000
Frm 00104
Fmt 4703
Sfmt 4703
Issued in Burlington, Massachusetts, on
July 31, 2009.
Francis A. Favara,
Manager, Engine and Propeller Directorate,
Aircraft Certification Service.
[FR Doc. E9–21068 Filed 9–1–09; 8:45 am]
BILLING CODE 4910–13–M
DEPARTMENT OF TRANSPORTATION
Notice of issuance of advisory
circular.
ACTION:
Authority: 49 U.S.C. 106(g), 40113, 44701–
44702, 44704.
VerDate Nov<24>2008
45515
Federal Aviation Administration
Advisory Circular 33–8, Guidance for
Parts Manufacturer Approval of
Turbine Engine and Auxiliary Power
Unit Parts Under Test and
Computation
AGENCY: Federal Aviation
Administration (FAA), DOT.
ACTION: Notice of issuance of advisory
circular.
SUMMARY: This notice announces the
issuance of Advisory Circular (AC) 33–
8, Guidance for Parts Manufacturer
Approval of Turbine Engine and
Auxiliary Power Unit Parts under Test
and Computation. This AC provides
guidance for developing substantiation
data to support the design approval of
critical and complex turbine engine and
auxiliary power unit (APU) parts
produced under parts manufacturer
approval. This guidance is for the
comparative test and analysis method
used to show compliance to the
airworthiness requirements under test
and computation, per S21.303 of Title
14 of the Code of Federal Regulations
(14 CFR). This method supports
showing the engine or APU still
complies with 14 CFR part 33 and
Technical Standard Order (TSO) C77.
DATES: The Engine and Propeller
Directorate issued AC 33–8 on August
19, 2009.
FOR FURTHER INFORMATION CONTACT: The
Federal Aviation Administration, Attn:
Karen M. Grant, Engine and Propeller
Standards Staff, ANE–111, 12 New
England Executive Park, Burlington, MA
01803–5299; telephone: (781) 238–7119;
fax: (781) 238–7199; e-mail:
karen.m.grant@faa.gov.
We have filed in the docket all
substantive comments received, and a
report summarizing them. If you wish to
review the docket in person, you may go
to the above address between 9 a.m. and
5 p.m., Monday through Friday, except
Federal holidays. If you wish to contact
the above individual directly, you can
use the above telephone number or email address provided.
How to Obtain Copies: A paper copy
of AC 33–8 may be obtained by writing
to the U.S. Department of
E:\FR\FM\02SEN1.SGM
02SEN1
]]>Agencies
[Federal Register Volume 74, Number 169 (Wednesday, September 2, 2009)]
[Notices]
[Page 45515]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: E9-21068]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Advisory Circular 33.70-1, Guidance Material for Aircraft Engine
Life-Limited Parts Requirements
AGENCY: Federal Aviation Administration (FAA), DOT.
ACTION: Notice of issuance of advisory circular.
-----------------------------------------------------------------------
SUMMARY: This notice announces the issuance of Advisory Circular (AC)
33.70-1, Guidance Material for Aircraft Engine Life-limited Parts
Requirements. This AC provides definitions, guidance, and acceptable
methods that may be used to demonstrate compliance with the engine
life-limited parts integrity requirements of Sec. 33.70 of Title 14 of
the Code of Federal Regulations. Section 33.70 contains requirements
applicable to the design and life management of propulsion system life-
limited parts including high-energy rotating parts.
DATES: The Engine and Propeller Directorate issued AC 33.70-1 on July
31, 2009.
FOR FURTHER INFORMATION CONTACT: The Federal Aviation Administration,
Attn: Timoleon Mouzakis, Engine and Propeller Standards Staff, ANE-111,
12 New England Executive Park, Burlington, MA 01803-5299; telephone:
(781) 238-7114; fax: (781) 238-7199; e-mail: timoleon.mouzakis@faa.gov.
We have filed in the docket all substantive comments received, and
a report summarizing them. If you wish to review the docket in person,
you may go to the above address between 9 a.m. and 5 p.m., Monday
through Friday, except Federal holidays. If you wish to contact the
above individual directly, you can use the above telephone number or e-
mail address provided.
How to Obtain Copies: A paper copy of AC 33.70-1 may be obtained by
writing to the U.S. Department of Transportation, Subsequent
Distribution Office, DOT Warehouse, SVC-121.23, Ardmore East Business
Center, 3341Q 75th Ave., Landover, MD 20785, telephone 301-322-5377, or
by faxing your request to the warehouse at 301-386-5394. The AC will
also be available on the Internet at https://www.faa.gov/regulations_policies (then click on ``Advisory Circulars'').
Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704.
Issued in Burlington, Massachusetts, on July 31, 2009.
Francis A. Favara,
Manager, Engine and Propeller Directorate, Aircraft Certification
Service.
[FR Doc. E9-21068 Filed 9-1-09; 8:45 am]
BILLING CODE 4910-13-M
