Proposed Advisory Circular; Calibration Test, Endurance Test and Teardown Inspection for Turbine Engine Certification (Sections 33.85/87/93), 47272 [05-16021]

Download as PDF 47272 Federal Register / Vol. 70, No. 155 / Friday, August 12, 2005 / Notices administrative error, while, at the same time, providing interested parties with a suitable period of time to file comments, we find it appropriate to direct persons wishing to file objections to our tentative decision to so by August 15, 2005. FOR FURTHER INFORMATION CONTACT: Mr. Trace Atkinson, Air Carrier Fitness Division (X–56, Room 6401), U.S. Department of Transportation, 400 Seventh Street, SW., Washington, DC 20590, (202) 366–3176. Correction Dated: August 5, 2005. Karan K. Bhatia, Assistant Secretary for Aviation and International Affairs. [FR Doc. 05–16025 Filed 8–11–05; 8:45 am] BILLING CODE 4910–62–P DEPARTMENT OF TRANSPORTATION In the Federal Register of July 21, 2005, in FR Doc. 05–14379, on page 42135, in the third column, correct the ‘‘Dates’’ caption to read: DATES: Persons wishing to file objections should do so no later than August 15, 2005. Editorial Note: This document was inadvertently omitted from the issue of Wednesday, August 10, 2005. Dated: August 4, 2005. Karan K. Bhatia, Assistant Secretary, for Aviation and International Affairs. [FR Doc. 05–15917 Filed 8–9–05; 8:45 am] BILLING CODE 4910–62–M DEPARTMENT OF TRANSPORTATION Office of the Secretary Application of Eos Airlines, Inc. for Certificate Authority Department of Transportation. Notice of order to show cause (Order 2005–8–4) Dockets OST–2004– 19617. AGENCY: ACTION: SUMMARY: The Department of Transportation is directing all interested persons to show cause why it should not issue an order finding Eos Airlines, Inc., fit, willing, and able, and awarding it a certificate of public convenience and necessity to engage in foreign scheduled passenger air transportation of persons, property and mail. DATES: Persons wishing to file objections should do so no later than August 19, 2005. ADDRESSES: Objections and answers to objections should be filed in Dockets OST–2004–19617 and addressed to the Department of Transportation Dockets (SVC–124.1, Room PL–401), U.S. Department of Transportation, 400 Seventh Street, SW., Washington, DC 20590, and should be served upon the parties listed in Attachment A to the order. VerDate jul<14>2003 Mr. Trace Atkinson, Air Carrier Fitness Division (X–56, Room 6401), U.S. Department of Transportation, 400 Seventh Street, SW., Washington, DC 20590, (202) 366–3176. FOR FURTHER INFORMATION CONTACT: 17:14 Aug 11, 2005 Jkt 205001 Federal Aviation Administration Proposed Advisory Circular; Calibration Test, Endurance Test and Teardown Inspection for Turbine Engine Certification (Sections 33.85/87/ 93) Federal Aviation Administration, DOT. ACTION: Notice of availability of proposed advisory circular and request for comments. AGENCY: SUMMARY: This notice announces the availability and request for comments of draft Advisory Circular (AC), No. 33.87, Calibration Test, Endurance Test and Teardown Inspection for Turbine Engine Certification (§§ 33.85/87/93). DATES: Comments must be received on or before September 12, 2005. ADDRESSES: Send all comments on the proposed AC to the Federal Aviation Administration, Attn: Robert McCabe, Engine and Propeller Standards Staff, ANE–111, Engine and Propeller Directorate, Aircraft Certification Service, 12 New England Executive Park, Burlington, MA 01803–5299. FOR FURTHER INFORMATION CONTACT: Robert McCabe, Engine and Propeller Standards Staff, ANE–111, at the above address, telephone (781) 238–7138, fax (781) 238–7199. If you have access to the Internet, you may also obtain further information by writing to the following address: robert.mccabe@faa.gov. SUPPLEMENTARY INFORMATION: Comments Invited You may obtain a copy of the draft AC by contacting the person named under FOR FURTHER INFORMATION CONTACT, or if using the Internet, you may obtain a copy at either of the following addresses: https://www.airweb.faa.gov/ rgl or https://www.faa.gov/aircraft/ draft_doc/. Interested persons are invited to comment on the proposed AC and to submit written data, views, or arguments. Commenters must identify PO 00000 Frm 00105 Fmt 4703 Sfmt 4703 the subject of the AC, and submit comments to the address specified above. The Engine and Propeller Directorate, Aircraft Certification Service, will consider all responses received on or before the closing date for comments before it issues the final AC. We will also file in the docket all substantive comments received, and a report summarizing them. The docket is available for public inspection both before and after the comment date. If you wish to review the docket in person, you may go to the address above 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. Background This draft advisory circular (AC) would provide guidance and acceptable methods, but not the only methods, of compliance with the test requirements of § 33.85 (calibration test), § 33.87 (endurance test), and § 33.93 (teardown inspection) of Title 14 of the Code of Federal Regulations (14 CFR). This advisory circular would be published under the authority granted to the Administrator by 49 U.S.C. 106(g), 40113, 44701–44702, 44704, and would provide guidance for the requirements in 14 CFR part 33. Issued in Burlington, Massachusetts, on August 5, 2005. Francis A. Favara, Acting Manager, Engine and Propeller Directorate, Aircraft Certification Service. [FR Doc. 05–16021 Filed 8–11–05; 8:45 am] BILLING CODE 4910–13–M DEPARTMENT OF TRANSPORTATION Federal Aviation Administration Advisory Circular (AC) 45–2C, Identification and Regulation Marking Federal Aviation Administration (FAA), DOT. ACTION: Notice of availability. AGENCY: SUMMARY: This notice announces the availability of AC 45–2C, Identification and Registration Marking. AC 45–2C provides information and guidance concerning the requirements for identifying aircraft and related products with identification plates, and identifying aircraft with nationality and registration marks. The requirements are detailed in Title 14, Code of Federal Regulations (14 CFR), part 45, Identification and Registration Marking. E:\FR\FM\12AUN1.SGM 12AUN1

Agencies

[Federal Register Volume 70, Number 155 (Friday, August 12, 2005)]
[Notices]
[Page 47272]
From the Federal Register Online via the Government Printing Office [www.gpo.gov]
[FR Doc No: 05-16021]


-----------------------------------------------------------------------

DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


Proposed Advisory Circular; Calibration Test, Endurance Test and 
Teardown Inspection for Turbine Engine Certification (Sections 33.85/
87/93)

AGENCY: Federal Aviation Administration, DOT.

ACTION: Notice of availability of proposed advisory circular and 
request for comments.

-----------------------------------------------------------------------

SUMMARY: This notice announces the availability and request for 
comments of draft Advisory Circular (AC), No. 33.87, Calibration Test, 
Endurance Test and Teardown Inspection for Turbine Engine Certification 
(Sec. Sec.  33.85/87/93).

DATES: Comments must be received on or before September 12, 2005.

ADDRESSES: Send all comments on the proposed AC to the Federal Aviation 
Administration, Attn: Robert McCabe, Engine and Propeller Standards 
Staff, ANE-111, Engine and Propeller Directorate, Aircraft 
Certification Service, 12 New England Executive Park, Burlington, MA 
01803-5299.

FOR FURTHER INFORMATION CONTACT: Robert McCabe, Engine and Propeller 
Standards Staff, ANE-111, at the above address, telephone (781) 238-
7138, fax (781) 238-7199. If you have access to the Internet, you may 
also obtain further information by writing to the following address: 
robert.mccabe@faa.gov.

SUPPLEMENTARY INFORMATION:

Comments Invited

    You may obtain a copy of the draft AC by contacting the person 
named under FOR FURTHER INFORMATION CONTACT, or if using the Internet, 
you may obtain a copy at either of the following addresses: https://
www.airweb.faa.gov/rgl or https://www.faa.gov/aircraft/draft_doc/. 
Interested persons are invited to comment on the proposed AC and to 
submit written data, views, or arguments. Commenters must identify the 
subject of the AC, and submit comments to the address specified above. 
The Engine and Propeller Directorate, Aircraft Certification Service, 
will consider all responses received on or before the closing date for 
comments before it issues the final AC.
    We will also file in the docket all substantive comments received, 
and a report summarizing them. The docket is available for public 
inspection both before and after the comment date. If you wish to 
review the docket in person, you may go to the address above 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.

Background

    This draft advisory circular (AC) would provide guidance and 
acceptable methods, but not the only methods, of compliance with the 
test requirements of Sec.  33.85 (calibration test), Sec.  33.87 
(endurance test), and Sec.  33.93 (teardown inspection) of Title 14 of 
the Code of Federal Regulations (14 CFR).
    This advisory circular would be published under the authority 
granted to the Administrator by 49 U.S.C. 106(g), 40113, 44701-44702, 
44704, and would provide guidance for the requirements in 14 CFR part 
33.

    Issued in Burlington, Massachusetts, on August 5, 2005.
Francis A. Favara,
Acting Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 05-16021 Filed 8-11-05; 8:45 am]
BILLING CODE 4910-13-M

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