[Federal Register Volume 67, Number 169 (Friday, August 30, 2002)]
[Notices]
[Page 55910]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-22120]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


Proposed Advisory Circular; Guidance Material for 14 CFR 33.19, 
Durability, for Reciprocating Engine Redesigned Parts

AGENCY: Federal Aviation Administration, DOT.

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

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SUMMARY: The Federal Aviation Administration (FAA) announces the 
availability of proposed Advisory Circular (AC) Number 33.19-1, 
Guidance Material For 14 CFR 33.19, Durability, For Reciprocating 
Engine Redesigned Parts.

DATES: Comments must be received on or before October 31, 2002.

ADDRESSES: Send all comments on the proposed AC to the Federal Aviation 
Administration, Attn: Mark Rumizen, Engine and Propeller Standards 
Staff, ANE-110, 12 New England Executive Park, Burlington, MA 01803-
5299.

FOR FURTHER INFORMATION CONTACT: Mark Rumizen, Engine and Propeller 
Standards Staff, ANE-110, at the above address; telephone: (781) 238-
7113; fax: (781) 238-7199; e-mail: [email protected].

SUPPLEMENTARY INFORMATION:

Comments Invited

    A copy of the subject AC may be obtained by contacting the person 
named under FOR FURTHER INFORMATION CONTACT or by downloading the 
proposed AC from the following Internet Web site: http://www.airweb.faa.gov/rgl. The FAA invites interested parties to comment 
on the proposed AC. Comments should identify the subject of the AC and 
be submitted to the individual identified under FOR FURTHER INFORMATION 
CONTACT. The FAA will consider all communications received by the 
closing date before issuing the final AC.

Background

    This AC provides guidance and acceptable methods, but not the only 
methods, that may be used to demonstrate that redesigned parts for 
reciprocating engines comply with the requirements of 14 CFR 33.19 or 
Sec. 13.104 of the Civil Air Regulations (CAR). This AC addresses type 
design changes, parts manufacturing approvals (PMA), and supplemental 
type certificates (STC) for critical, highly stressed, or complex parts 
in reciprocating engines.

    (Authority: 49 U.S.C. 106(g), 40113, 44701-44702, 44704.)

    Issued in Burlington, Massachusetts, on August 21, 2002.
Francis Favara,
Assistant Manager, Engine and Propeller Directorate, Aircraft 
Certification Service.
[FR Doc. 02-22120 Filed 8-29-02; 8:45 am]
BILLING CODE 4910-13-M