[Federal Register Volume 67, Number 132 (Wednesday, July 10, 2002)]
[Notices]
[Page 45780]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 02-17378]



[[Page 45780]]

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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration


Proposed Advisory Circular; Guidance Material for 14 CFR 33.28, 
Reciprocating Engines, Electrical and Electronic Engine Control Systems

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 33.28-2, 
Guidance Material For 14 CFR Sec. 33.28, Reciprocating Engines, 
Electrical And Electronic Engine Control Systems.

DATES: Comments must be received on or before September 18, 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

    Electrical and Electronic Engine Control (EEC) technology was 
initially applied to turbine engines designed for large transport 
aircraft applications. Therefore, the information and guidance for 
showing compliance with Sec. 33.28 provided by the FAA was oriented 
toward these applications. However, the increasing use of EEC systems 
in reciprocating piston engines has created a need for guidance 
specifically for reciprocating engines. This AC provides a means, but 
not the only means, of showing compliance with Sec. 33.28 that 
addresses these issues.


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

    Issued in Burlington, Massachusetts, on July 3, 2002.
Jay J. Pardee,
Manager, Engine and Propeller Directorate, Aircraft Certification 
Service.
[FR Doc. 02-17378 Filed 7-9-02; 8:45 am]
BILLING CODE 4910-13-M