[Federal Register Volume 70, Number 95 (Wednesday, May 18, 2005)]
[Notices]
[Pages 28595-28596]
From the Federal Register Online via the Government Publishing Office [www.gpo.gov]
[FR Doc No: 05-9825]


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DEPARTMENT OF TRANSPORTATION

Federal Aviation Administration

[Summary Notice No. PE-2005-28]


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: Kenna Sinclair (425) 227-1556), 
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-1), 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 May 11, 2005.
Anthony F. Fazio,
Director, Office of Rulemaking.

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: A seven-year extension of 
FAA Partial Time Limited Exemption Number 8329A for Boeing Model 777 
airplanes equipped with Pratt & Whitney or Rolls-Royce engines. This is

[[Page 28596]]

an exemption from the affected regulations as they relate to the 
structural strength, deformation, and failure of the thrust reverser 
inner wall panels under certain refused takeoff (RTO) conditions. 
Partial Grant of Exemption, 04/29/2005, Exemption No. 8329B.

[FR Doc. 05-9825 Filed 5-17-05; 8:45 am]
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