[Federal Register: July 23, 2002 (Volume 67, Number 141)]
[Notices]
[Page 48246]
From the Federal Register Online via GPO Access [wais.access.gpo.gov]
[DOCID:fr23jy02-810]
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DEPARTMENT OF TRANSPORTATION
Federal Aviation Administration
Proposed Advisory Circular; Turbine Engine Continued Rotation and
Rotor Locking
AGENCY: Federal Aviation Administration, DOT.
ACTION: Notice of availability of proposed advisory circular and
request for comments.
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SUMMARY: This notice announces the availability and request for
comments of draft Advisory Circular (AC), No. 33.74/92-1A, Turbine
Engine Continued Rotation and Rotor Locking.
DATES: Comments must be received on or before September 23, 2002.
ADDRESSES: Send all comments on the proposed AC to the Federal Aviation
Administration, Attn: Marc Bouthillier, Engine and Propeller Standards
Staff, ANE-110, Engine and Propeller Directorate, Aircraft
Certification Service, 12 New England Executive Park, Burlington, MA
01803-5299.
FOR FURTHER INFORMATION CONTACT: Marc Bouthillier, Engine and Propeller
Standards Staff, ANE-100, at the above address, telephone (781) 238-
7120, fax (781) 238-7199. If you have access to the Internet, you may
also obtain further information by writing to the following address:
``marc.bouthillier@faa.gov.''
SUPPLEMENTARY INFORMATION:
Comments Invited
A copy of the draft AC may be obtained by contacting the person
named under FOR FURTHER INFORMATION CONTACT, or Internet users may
obtain a copy at the following address: ``http://www.airweb.faa.gov/
rgl.'' Interested persons are invited to comment on the proposed AC,
and to submit such written data, views, or arguments as they desire.
Commenters must identify the subject of the AC, and submit comments to
the address specified above. All communications received on or before
the closing date for comments will be considered by the Engine and
Propeller Directorate, Aircraft Certification Service, before issuance
of the final AC.
Background
This draft advisory circular (AC) would provide guidance and
acceptable methods, but not the only methods that may be used to
demonstrate compliance with the continued rotation and rotor locking
requirements. This AC would combine Secs. 33.74 and 33.92.
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 June 28, 2002.
Francis Favara,
Assistant Manager, Engine and Propeller Directorate, Aircraft
Certification Service.
[FR Doc. 02-18473 Filed 7-22-02; 8:45 am]
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