[Federal Register Volume 69, Number 111 (Wednesday, June 9, 2004)]
[Notices]
[Page 32396]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 04-12974]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

[Summary Notice No. PE-2004-36]


Petitions for Exemption; Dispositions of Petitions Issued

AGENCY: Federal Aviation Administration (FAA), DOT.

ACTION: Notice of disposition of prior petition.

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SUMMARY: Pursuant to FAA's rulemaking provisions governing the 
application, processing, and disposition of petitions for exemption, 
part 11 of title 14, Code of Federal Regulations (14 CFR), this notice 
contains the disposition of certain petitions previously received. The 
purpose of this notice is to improve the public's awareness of, and 
participation in, this aspect of FAA's regulatory activities. Neither 
publication of this notice nor the inclusion or omission of information 
in the summary is intended to affect the legal status of any petition 
or its final disposition.

FOR FURTHER INFORMATION CONTACT: Susan Boylon (425-227-1152), Transport 
Airplane Directorate (ANM-113), Federal Aviation Administration, 1601 
Lind Ave., SW., Renton, WA 98055-4056; or John Linsenmeyer (202-267-
5174), Office of Rulemaking (ARM-207), Federal Aviation Administration, 
800 Independence Avenue, SW., Washington, DC 20591. This notice is 
published pursuant to 14 CFR 11.85 and 11.91.

    Issued in Washington, DC, on June 3, 2004.
Donald P. Byrne,
Assistant Chief Counsel for Regulations.

Disposition of Petitions

    Docket No.: FAA-2004-17909.
    Petitioner: The Boeing Company.
    Sections of 14 CFR Affected: 14 CFR 25.301, 25.303, 25.305, and 
25.901(c).
    Description of Relief Sought/Disposition: To permit type 
certification of the modification to the thrust reverser type design of 
Pratt & Whitney powered Boeing Model 777 airplanes, which is described 
in the background section of the exemption, without a complete showing 
of compliance. These requirements relate to the structural strength, 
deformation and failure of the thrust reverser inner wall panels during 
a rejected takeoff related thrust reverser deployment at high engine 
power.
    Time-Limited Partial Grant of Exemption, 05/26/2004, Exemption No. 
8329.
[FR Doc. 04-12974 Filed 6-8-04; 8:45 am]
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